Beech Kit Catalog April 2009

Technical Manual Distribution Center(TMDC)

Kit Catalog

April 2009

Visit our web site at http://pubs.hawkerbeechcraft.com

For a list of up-to-date kits

Raytheon Aircraft Company, which has been renamed Hawker Beechcraft Corporation, is now owned by Hawker Beechcraft, Inc. Neither Hawker Beechcraft, Inc. nor Hawker Beechcraft Corporation are affiliated any longer with Raytheon Company. Any Raytheon marks contained in this document are owned by Raytheon Company and are employed pursuant to a limited license granted by Raytheon Company.

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KIT CATALOG - TABLE OF CONTENTS

Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberEXTERNAL POWER RECEPTACLE INSTALLATION - (100-3007-1 P) 1

E.L.T. SWITCH GUARD - (101-3062-1 S) 1

ELECTRICAL BONDING EQUIPMENT - (101-3227-1) 1



BATTERY & STARTER RELAY REPLACEMENT - (105-3002-0001) 2




LANDING GEAR RELAY REPLACEMENT INSTL-KIT - (105-3003-0001) 2

EXTERNAL POWER RELAY REPLACEMENT - (105-3004-0001) 3

HEATER RELAY REPLACEMENT - (105-3005-0001) 3

VOLTAGE REGULATOR AND OVERVOLTAGE RELAY REPLACEMENT - (23-3006-1 S) 3

GROUND STRAP INSTL(COMM KIT) - (23-3011-1 S) 3

PITOT TUBE INSTALLATION, HEATED - (23-4002- P) 3

WING SPAR REPAIR, OUTBOARD SECTION LH WING UPPER OR LOWER SPAR FLANGE - (23-4008-1 S) 4

WING SPAR REPAIR, OUTBOARD SECTION RH WING UPPER OR LOWER SPAR FLANGE - (23-4008-2 S) 4

WING SPAR REPAIR, OUTBOARD SECTION IN WEB AND FLANGE AREA OF SLICE LH WING - (23-4008-3 S) 4

WING SPAR REPAIR, OUTBOARD SECTION IN WEB AND FLANGE AREA OF SLICE RH WING - (23-4008-4 S) 4

DOOR - CABIN ENTRANCE ASSIST STEP REPLACEMENT - (23-4012-3 S) 5

AILERON PUSHROD, INSPECTION ACCESS - (23-4013-1 S) 5

SHOULDER HARNESS INSTALLATION PILOT AND COPILOT (BEIGE) - (23-5004-1 P) 5

SHOULDER HARNESS INSTALLATION PILOT AND COPILOT (BEIGE) - (23-5004-3 P) 6

SHOULDER HARNESS INSTALLATION (3RD AND 4TH SEATS) - (23-5010-1 P) 6

LANDING GEAR REMOVAL OF FREE PLAY IN MAIN LANDING GEAR - (23-8009-1 S) 6

SHIMMY DAMPER REPLACEMENT - SPARES - (23-8010-1 S) 6

NOSE GEAR DOWN LOCK SWITCH INSTALLATION - (23-8011-1) 7

WINTER BAFFLE - (23-9007-1 P) 7

FUEL SELECTOR VALVE, REPLACEMENT - (23-9019-1 S) 7

FUEL MIXTURE CONTROL ASSEMBLY - (23-9022-1 S) 7




FUEL MIXTURE CONTROL CABLE REPLACEMENT - (23-9024-1 S) 8



FUEL STRAINER - SPARES - (23-9026-1 S) 9

Page 1 of 2Printed on Tuesday, March 31, 2009


Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberHORIZON GYRO REPLACEMENT (DIRECTIONAL) - SPARES - (33-5007-1 S) 9

HORIZON GYRO REPLACEMENT (ARTIFICIAL) - SPARES - (33-5007-3 S) 10

STARTER RELAY - SPARES - (36-3008-1 S) 10

STARTER RELAY - SPARES - (36-3008-3 S) 10

FRESH AIR BLOWER REPLACEMENT - SPARES - (36-4009-1 S) 10

FUEL FILLER NECK RESTRICTOR - (36-5013-1 S) 11

STARTER ENERGIZE LIGHT INSTALLATION - (55-3022-1 S) 11

CLOCK INSTALLATION, INSTRUMENT PANEL, (14-VOLT) - SPARES - (55-3029-1 P) 11


EXTERIOR PLACARD - (76-2001-1 S) 11

ALTERNATOR DIODE INSTALLATION - (76-3001-1 S) 12

RUDDER TORQUE TUBE FASTENER - (76-4001-1 S) 12

NACELLE KEEL FLANGE, FORWARD - (76-4002-1 S) 12

NACELLE INSPECTION PANEL - (76-4003-1 S) 12

INSTRUMENT CLUSTER, ENGINE - SPARES - (76-5002-1 S) 12

INSTRUMENT CLUSTER, ENGINE - SPARES - (76-5002-3 S) 13

SPACER INSTL(COMM KIT) - (76-5005-1 S) 13


LANDING GEAR DOOR, MAIN - (76-8002-1 S) 13

KIT-S-NS GR DR LKG - (76-8003-1 S) 13

NOSE LANDING GEAR BUSHING AND HINGE PIN REPLACEMENT - (76-8004-1 S) 14

NOSE LANDING GEAR BUSHING REPLACEMENT - (76-8005-1 S) 14

SHOCK ABSORBER INSTALLATION - SPARES - (76-8006-1 S) 14


INTERIOR PLACARD - (77-2002-1 S) 14

LANDING LIGHT WIRE, IMPROVED CONNECTION - (77-3002-1 S) 15

ELEVATOR TRIM TAB CABLE AND DRUM REPLACEMENT - (77-4002-1 S) 15

TAIL SKID INSTL - (77-4004-1 P) 15

BALANCE WEIGHT, RUDDER REINFORCED ATTACHMENT - (77-4006-1 S) 15

RUDDER HINGE PIN BUSHING INSTALLATION - (77-4007-1 S) 15

LANDING GEAR ATTACHMENT POINT - (77-8001-1 S) 16

LANDING GEAR, ELLIPTICAL BUSHING RETAINER INSTALLATION - (77-8003-1 S) 16

ENGINE MOUNT, REPLACEMENT - (77-9001-1 S) 16


KIT CATALOG

100-3007-1 PEXTERNAL POWER RECEPTACLE INSTALLATION ATA :23, A23, A23A, B23, C23, 24, A24, A24R,B24R, C24RTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN EXTERNAL POWERRECEPTACLE (12-VOLT ONLY).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

101-3062-1 SE.L.T. SWITCH GUARD ATA :23, 24, 76, 77THIS KIT PROVIDES A SWITCH GUARD FOR THE ABOVE MODELS EQUIPPED WITH A TR70-13TRANSMITTER AND KIT 101-3039-1 S REMOTE SWITCH INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

101-3227-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN VHF FORMAT.

NOTENOTENOTENOTE:::: ALODINE600X60GR PROTECTIVE COATING REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3227-3ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN PAL FORMAT.



101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES FOR PROPER ELECTRICAL BONDING TO METALS ON ALL NON-COMPOSITERAYTHEON AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

105-3002-0001BATTERY & STARTER RELAY REPLACEMENT ATA : 24C23 M-2179 THRU M-2281; C24R; MC-674 THRU

MC-733THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITESTARTER RELAY, P/N SBC-9401-1 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

105-3002-0003BATTERY & STARTER RELAY REPLACEMENT ATA : 24C23 M-2282 THRU M-2367; C24R S/N: MC-734

THRU MC-781THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITESTARTER RELAY, P/N SBC-9401-1 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

105-3002-0005BATTERY & STARTER RELAY REPLACEMENT ATA : 2476 ME-183 THRU ME-353THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITESTARTER RELAY, P/N SBC-9401-1 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

105-3002-0007BATTERY & STARTER RELAY REPLACEMENT ATA : 2477 THIS KIT PROVIDES PARTS AND

INFORMATION TO INSTALLREPLACEMENTS FOR THE PRESTOLITEBATTERY & STARTER RELAYS, P/NSBC-9401-1, ON IN-SERVICE AIRCRAFT.

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITESTARTER RELAY, P/N SBC-9401-1 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

105-3003-0001LANDING GEAR RELAY REPLACEMENT INSTL-KIT ATA : 3276 ME-354 THRU ME-437C24R MC-734 THRU MC-781THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITELANDING GEAR RELAYS P/N SBC-9401-1, ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

105-3004-0001EXTERNAL POWER RELAY REPLACEMENT ATA : 2476 ME-183 THRU ME-437C23 M-2179 THRU M-2367; C24R S/N:C24R MC-674 THRU MC-781THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITE (EXTPOWER) RELAY P/N SBC-9401-1, ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

105-3005-0001HEATER RELAY REPLACEMENT ATA : 2176 ME-354 THRU ME-437THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE PRESTOLITEHEATER RELAY P/N SBC-9401-1, ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

23-3006-1 SVOLTAGE REGULATOR AND OVERVOLTAGE RELAY REPLACEMENT ATA : 2419, 19A, B19 MB-1 THRU MB-840A23, B23, C23 M-555 THRU M-1929A23-24, A24 MA-1 THRU MA-368A24R, B24R MC-2 THRU MC-487SI NO. 0874 OR SUBSEQUENTTHIS KIT PROVIDES A REPLACEMENT VOLTAGE REGULATOR AND OVERVOLTAGE RELAY FOR THEEXISTING PARTS WHICH ARE NO LONGER AVAILABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

23-3011-1 SGROUND STRAP INSTL(COMM KIT) ATA : 23WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

23-4002- PPITOT TUBE INSTALLATION, HEATED ATA : 2119, 23, A23, A23A, B23, A23-24, B24R & C23THRU M-1878 (EXCEPT 1971 MODELS),C24R THRU MC-536 (EXCEPT MC-533).THIS KIT PROVIDES A HEATED PITOT TUBE INSTALLATION FOR 12 VOLT ONLY AIRCRAFT:

NOTENOTENOTENOTE:::: MC-533 AND MC-537 AND AFTER ARE 24 VOLT AIRCRAFT.WT. CHANGE : WT: +1.2 LBS @ 108 ARMEST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

23-4008-1 SWING SPAR REPAIR, OUTBOARD SECTION LH WING UPPER OR LOWERSPAR FLANGE

ATA : 57

19 SERIES23 SERIES24 AND 24R SERIESTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A SPAR REPAIR TO THE OUTBOARDSECTION LEFT HAND WING. THIS REPAIR MAY BE MADE TO UPPER OR LOWER FLANGE OF SPAR INAREAS WHERE DAMAGE MAY HAVE OCCURRED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

23-4008-2 SWING SPAR REPAIR, OUTBOARD SECTION RH WING UPPER OR LOWERSPAR FLANGE

ATA : 57

19 SERIES23 SERIES24 AND 24R SERIESTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A SPAR REPAIR TO THE OUTBOARDSECTION RIGHT HAND WING. THIS REPAIR MAY BE MADE TO UPPER OR LOWER FLANGE OF SPAR INAREAS WHERE DAMAGE MAY HAVE OCCURRED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

23-4008-3 SWING SPAR REPAIR, OUTBOARD SECTION IN WEB AND FLANGE AREAOF SLICE LH WING

ATA : 57

19 SERIES23 SERIES24 AND 24R SERIESTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A SPAR REPAIR TO THE OUTBOARDSECTION IN WEB AND FLANGE AREA OF SPAR SPLICE LEFT HAND WING.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

23-4008-4 SWING SPAR REPAIR, OUTBOARD SECTION IN WEB AND FLANGE AREAOF SLICE RH WING

ATA : 57

19 SERIES23 SERIES24 AND 24R SERIESTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A SPAR REPAIR TO THE OUTBOARDSECTION IN WEB AND FLANGE AREA OF SPAR SPLICE LEFT HAND WING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

23-4012-3 SDOOR - CABIN ENTRANCE ASSIST STEP REPLACEMENT ATA : 53B24R (SIERRA 200) MC-155, MC-165 THRU MC-283SB NO. 2090, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY FOR REPLACEMENT OF ASSIST STEP ONAIRCRAFT THAT HAVE EXPERIENCED PREMATURE CABIN ASSIST STEP BREAKAGE WITH A STRONGERSTEP TO AID IN BOARDING.

NOTENOTENOTENOTE:::: THIS KIT FOR USE ON AIRCRAFT WITHOUT FIFTH AND SIXTH SEATS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

23-4013-1 SAILERON PUSHROD, INSPECTION ACCESS ATA : 2723, A23, A23A, B23, C23, C23 SUNDOWNER180

M-1 THRU M-2392

A23-19, 19A, M19A, B19, B19 SPORT 150 MB-1 THRU MB-905 EXCEPT MB-723 WHICHWAS CANCELLED AND REPLACED BYMB-623

A23-24, A24 MA-1 THRU MA-368A24R, B24R SIERRA 200, C24R SIERRA 200 MC-2 THRU MC-150, MC-152 THRU MC-795SB NO. 2198 OR SUBSEQUENTTHIS KIT CONTAINS PARTS AND INFORMATION FOR THE INSTALLATION OF AN ACCESS PLATE FOR THEINSPECTION AND/OR INSTALLATION OF THE AILERON PUSHROD.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

23-5004-1 PSHOULDER HARNESS INSTALLATION PILOT AND COPILOT (BEIGE) ATA : 25A24 MA-364 THRU MA-368A24R, B24R MC-2 THRU MC-385B19 MB-481 THRU MB-778C23 M-1285 THRU M-1714SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES ALL PARTS AND INFORMATION REQUIRED TO INSTALL NEW SEAT BELTS ANDSHOULDER HARNESS WITH INERTIA REELS FOR BOTH THE PILOT AND COPILOT SEATS.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 1 AND FIGURE 2, FOR ADDITIONAL INFORMATION.WT. CHANGE : N/AEST. MAN/HRS: : 17MEN : 1 (MAN)


KIT CATALOG

23-5004-3 PSHOULDER HARNESS INSTALLATION PILOT AND COPILOT (BEIGE) ATA : 25A23-19, 19A, 23, A23, A23A, B23, A23-24SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES ALL PARTS AND INFORMATION REQUIRED TO INSTALL NEW SEAT BELTS ANDSHOULDER HARNESS WITH INERTIA REELS FOR BOTH THE PILOT AND COPILOT SEATS.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 1 AND FIGURE 2, FOR ADDITIONAL INFORMATION.WT. CHANGE : WT: +5.9 LBS @ 122 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

23-5010-1 PSHOULDER HARNESS INSTALLATION (3RD AND 4TH SEATS) ATA : 2519, 19A, B19, 23, A23, A23A, B23, C23A24, A24R AND B24R MC-151 THRU MC-381, MC-383 THRU

MC-385SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES ALL PARTS AND INFORMATION REQUIRED TO INSTALL A NEW SHOULDER HARNESSCOMPLETE WITH INERTIA REELS ON THE SEATS INDICATED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 20MEN : 1 (MAN)

23-8009-1 SLANDING GEAR REMOVAL OF FREE PLAY IN MAIN LANDING GEAR ATA : 3223, A23, A23A, B23, C23 M-1 THRU M-2037A23-19, 19A, M19A, B19 MB-1 THRU MB-891A23-24 AND A24 MA-1 THRU MA-368"OPTIONAL" SB NO. 2014 OR SUBSEQUENTRAYTHEON AIRCRAFT CORPORATION RECOMMENDS THAT THE REPAIR SPECIFIED IN THIS KIT BEACCOMPLISHED AT ANY TIME FREE PLAY IS INDICATED AT THE BASE OF THE LANDING GEAR WELDASSEMBLY DURING NORMAL OPERATION OF THE AIRPLANE OR AT ANY ROUTINE INSPECTION INTERVAL.

NOTENOTENOTENOTE:::: EPON 828 VERSAMID 125 RESIN, DTA951 CATALYST, & MOLD RELEASE #225 PARTINGAGENT REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY, OR FROM RAPID. 1 EACH OF PART NUMBERSLISTED ABOVE.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)

23-8010-1 SSHIMMY DAMPER REPLACEMENT - SPARES ATA : 32A23-19, 19A, M19A, B19, A23A, B23, C23,A23-24, A24R, B24R, C24RTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A 169-380029-5 SHIMMY DAMPERASSEMBLY AS A SPARE REPLACEMENT FOR THE 169-380029 (BASIC) SHIMMY DAMPER.

NOTENOTENOTENOTE:::: REWORK THE ENGINE MOUNT IN THIS KIT FOR MODELS, A24R, B24R AND C24R AIRCRAFTONLY. FOR ALL OTHER MODELS NOTED, DISREGARD REWORK INFORMATION ANDINSTALL THE 169-380029-5 SHIMMY DAMPER AS A DIRECT REPLACEMENT PART.



KIT CATALOG

23-8011-1NOSE GEAR DOWN LOCK SWITCH INSTALLATION ATA : 32A24A MC-2 THRU MC-150B24R MC-152 THRU MC-448, MC-450, MC-451C24R MC-449, MC-452 THRU MC-795THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SWITCH ON THE NOSE GEAR DOWN LOCKHOOK.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEM, EPOXY PRIMER, "MILP23377 QT" OR "U1201 QT" OR "MIL-P-23377D", OR "MIL-P23377C QT" OR "GL" OR IT'S EQUIVALENT, IF NOT IN YOUR SHOPSTOCK, PROCURE LOCALLY.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

23-9007-1 PWINTER BAFFLE ATA : 71B19, C23THIS KIT PROVIDES REDUCTION OF ENGINE WEAR AND ALLOWS ENGINE WARM UP DURING COLDWEATHER OPERATIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)

23-9019-1 SFUEL SELECTOR VALVE, REPLACEMENT ATA : 7323, A23, A23A, B23, C23 M-2 THRU M-1516A23-19, 19A, M19A, B19 MB-1 THRU MB-654A23-24, A24 MA-1 THRU MA-368A24R, B24R MC-2 THRU MC-180SI NO. 0838-289 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE FUEL SELECTOR VALVE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

23-9022-1 SFUEL MIXTURE CONTROL ASSEMBLY ATA : 7619A, M19A, A23-19, 23, A23, A23A, B23THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH A SPARES REPLACEMENT FOR 169-380007-1MIXTURE CONTROL ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

23-9022-2 SFUEL MIXTURE CONTROL ASSEMBLY ATA : 76B23THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH A SPARES REPLACEMENT FOR 169-380007-3MIXTURE CONTROL ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

23-9022-3 SFUEL MIXTURE CONTROL ASSEMBLY ATA : 76A23 A23ATHIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH A SPARES REPLACEMENT FOR 169-380007-5MIXTURE CONTROL ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

23-9022-4 SFUEL MIXTURE CONTROL ASSEMBLY ATA : 76A23-24THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH A SPARES REPLACEMENT FOR 169-380007-7MIXTURE CONTROL ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

23-9024-1 SFUEL MIXTURE CONTROL CABLE REPLACEMENT ATA : 76B19 MB-558 THRU MB-634, MB-649, MB-655

THRU MB-905SI NO. 1123 OR SUBSEQUENTTHIS KIT PROVIDES A MORE DURABLE MIXTURE CONTROL CABLE ASSEMBLY TO REPLACE THE ORIGINALMIXTURE CONTROL CABLE WHICH IS NO LONGER AVAILABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

23-9024-3 SFUEL MIXTURE CONTROL CABLE REPLACEMENT ATA : 76B19 MB-635 THRU MB-648, MB-650 THRU

MB-654C23 M-1413, M-1414, M-1416 THRU M-1418,

M-1420 THRU M-1422, M-1424 THRU M-1438,M-1440, M-1446, M-1448 THRU M-2016,M-2018 THRU M-2143

SI NO. 1123 OR SUBSEQUENTTHIS KIT PROVIDES A MORE DURABLE MIXTURE CONTROL CABLE ASSEMBLY TO REPLACE THE ORIGINALMIXTURE CONTROL CABLE WHICH IS NO LONGER AVAILABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : N/A

23-9024-5 SFUEL MIXTURE CONTROL CABLE REPLACEMENT ATA : 76B24R, C24R MC-152 THRU MC-539, MC-541 THRU

MC-650SI NO. 1123 OR SUBSEQUENTTHIS KIT PROVIDES A MORE DURABLE MIXTURE CONTROL CABLE ASSEMBLY TO REPLACE THE ORIGINALMIXTURE CONTROL CABLE WHICH IS NO LONGER AVAILABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

23-9026-1 SFUEL STRAINER - SPARES ATA : 2823, A23, A23A, B23, C23 M-1 THRU M-1604, M-1606 THRU M-1819,

M-1821 THRU M-1836, M-1838 THRU M-1841,M-1843 THRU M-1844, M-1846 THRU M-1852,M-1855, M-1857 THRU M-1859, M-1863,M-1864, M-1867, M-1868

A23-19, 19A, M19A, B19 MB-1 THRU MB-812A23-24 MA-1 THRU MA-368A24R MC-2 THRU MC-310THIS KIT PROVIDES A SPARES REPLACEMENT FUEL STRAINER.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

33-5007-1 SHORIZON GYRO REPLACEMENT (DIRECTIONAL) - SPARES ATA : 31A23-19, 23, A23A, A23-24THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE DIRECTIONAL GYROS PARTNUMBER 35-380039-1 OR 50-380007-7.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)


KIT CATALOG

33-5007-3 SHORIZON GYRO REPLACEMENT (ARTIFICIAL) - SPARES ATA :A23-19, 23, A23A, A23-24THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE ARTIFICIAL HORIZON GYROPART NUMBER 35-380043-1 OR 50-380008-7.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

36-3008-1 SSTARTER RELAY - SPARES ATA :B19, C23, B24RTHIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACEMENT OF SAW4204, SAW9201, 1114213 OR1464, 12 VOLT STARTER RELAY ON INSERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-3008-3 SSTARTER RELAY - SPARES ATA :76 ME-1 THRU ME-182THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REPLACEMENT 12 VOLTSTARTER RELAY, FOR THE SAW4204, SAW9201 OR 1464, 12 VOLT STARTER RELAY THAT MAY BE ONYOUR AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-4009-1 SFRESH AIR BLOWER REPLACEMENT - SPARES ATA :19, 23, 24, 76 SERIESSB NO. 2380, REV. 2THIS KIT PROVIDES PARTS FOR REPLACEMENT OF THE FRESH AIR BLOWER ASSEMBLIES PART NUMBER58-380108-1 OR 169-380096-5 ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REPLACEMENT OF THE BLOWER WITH THIS KIT DOES NOT REQUIRE THE DETAIL PARTSWHICH ARE FURNISHED.



KIT CATALOG

36-5013-1 SFUEL FILLER NECK RESTRICTOR ATA :19 MB-1 THRU MB-90523 M-1 THRU M-239224 MC-2 THRU MC-795A23-24 MA-1 THRU MA-368SB NO. 2045, REV. 3, QUANTITY AS REQUIREDFOR AIRCRAFT OPTIONAL FUEL SYSTEMS KIT CONSIST OF 2 CAPS AND INSERTS, 1 TOOL AND KITDRAWING.

NOTENOTENOTENOTE:::: INSERTS ARE TOO BIG ON AIRCRAFT, NEED ALSO TO INSTALL ON AIRCRAFT (M-1 THRUM-554) SERVICE INSTRUCTION NO. 0801-287 REV. 1, FUEL CAP AND ADAPTER PN169-380024-601 (2 PER AIRCRAFT) AND "890B1/2QT" SEALER AS REQUIRED.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.5MEN : 1 (MAN)

55-3022-1 SSTARTER ENERGIZE LIGHT INSTALLATION ATA :76THIS KIT PROVIDES A WARNING LIGHT TO SHOW WHEN STARTER RELAY IS CLOSED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

55-3029-1 PCLOCK INSTALLATION, INSTRUMENT PANEL, (14-VOLT) - SPARES ATA :B19, C23, A24, A24R, B24R, 76, 77THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 50-380013-5 AND 58-380015-1 8-DAY CLOCKS OR58-380077-1 AND 58-380077-5 ELECTRIC CLOCKS WHEN USED IN A 14-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

55-3029-3 PCLOCK INSTALLATION, INSTRUMENT PANEL, (28-VOLT) - SPARES ATA :C24, C24RTHIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 50-380013-5 AND 58-380015-3 8-DAY CLOCKS OR58-380077-3 AND 58-380077-7 ELECTRIC CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24 TO 30MEN : 2 (MEN)

76-2001-1 SEXTERIOR PLACARD ATA :76THIS KIT INCLUDES INSTRUCTIONS AND A REPLACEMENT SET OF EASILY INSTALLED, PRESSURESENSITIVE STANDARD EXTERIOR PLACARDS.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

76-3001-1 SALTERNATOR DIODE INSTALLATION ATA :76 ME-1 THRU ME-342SI NO. 1232 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR INSTALLATION OF ALTERNATOR FIELDDIODE TO REDUCE POSSIBILITY OF ALTERNATOR FEED SHORT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

76-4001-1 SRUDDER TORQUE TUBE FASTENER ATA :76 ME-1 THRU ME-394SI NO. 1238 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL IMPROVED SECURITY OF THERUDDER TORQUE TUBE TO THE LOWER HINGE ADAPTER.

NOTENOTENOTENOTE:::: NAPTHA TT-N-95A PRIMER AND EA9309 ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


76-4002-1 SNACELLE KEEL FLANGE, FORWARD ATA :76"MANDATORY" SI NO. 2018 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REPLACEMENT KEEL FLANGESAND ENGINE MOUNT ATTACH BRACKETS.WT. CHANGE : WT: +1.67 LBS @ 94.05 ARM: MOMENT: 157.06 IN.-LBSEST. MAN/HRS: : 116MEN : 1 (MAN)

76-4003-1 SNACELLE INSPECTION PANEL ATA :76"MANDATORY" SB NO. 2018 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL INBOARD AND OUTBOARDINSPECTION PANELS ON BOTH LEFT AND RIGHT ENGINE NACELLES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

76-5002-1 SINSTRUMENT CLUSTER, ENGINE - SPARES ATA :76 REPLACEMENT FOR 105-389011-31)THESE KITS PROVIDE SPARES REPLACEMENT AS INDICATED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

76-5002-3 SINSTRUMENT CLUSTER, ENGINE - SPARES ATA :76 REPLACEMENT FOR 105-389011-5)THESE KITS PROVIDE SPARES REPLACEMENT AS INDICATED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

76-5005-1 SSPACER INSTL(COMM KIT) ATA : 23WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

76-5006-1 SFUEL FILLER NECK RESTRICTOR ATA :76 ME-1 THRU ME-437"MANDATORY" SB NO. 2045, REV. 3THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL FILLER AND REPLACETHE FUEL FILLER CAPS WITH NON-LIGHTNING TYPE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.5MEN : 1 (MAN)

76-8002-1 SLANDING GEAR DOOR, MAIN ATA :76 ME-1 THRU ME-347SI NO. 1166 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL IMPROVED MAIN LANDING GEARDOORS AND ATTACHING HARDWARE.

NOTENOTENOTENOTE:::: NAPTHA TT-N-95A PRIMER AND EA9309 ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


76-8003-1 SKIT-S-NS GR DR LKG ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

76-8004-1 SNOSE LANDING GEAR BUSHING AND HINGE PIN REPLACEMENT ATA :76 ME-1 THRU ME-418SI NO. 1209 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A BUSHING AND HINGE PIN INTHE NOSE LANDING GEAR.

NOTENOTENOTENOTE:::: KIT NO. 76-8004 INCLUDES KIT NO. 76-8003.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

76-8005-1 SNOSE LANDING GEAR BUSHING REPLACEMENT ATA :76 ME-1 THRU ME-437SB NO. 2009 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR INSPECTION AND INSTALLATION OF THENOSE LANDING GEAR BUSHINGS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

76-8006-1 SSHOCK ABSORBER INSTALLATION - SPARES ATA :76 ME-1 THRU ME-437THIS KIT PROVIDES PARTS FOR REPLACEMENT OF THE 105-384001-1 SHOCK ABSORBER ASSEMBLIES ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT REPLACES ONE MAIN GEAR SHOCK ABSORBER ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

77-2001-1 SEXTERIOR PLACARD ATA :77THIS KIT INCLUDES INSTRUCTIONS AND A REPLACEMENT SET OF EASILY INSTALLED, PRESSURESENSITIVE STANDARD EXTERIOR PLACARDS.WT. CHANGE : SEE KIT DRAWINGEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

77-2002-1 SINTERIOR PLACARD ATA :77THIS KIT INCLUDES INSTRUCTIONS AND A REPLACEMENT SET OF EASILY INSTALLED, PRESSURESENSITIVE STANDARD INTERIOR PLACARDS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

77-3002-1 SLANDING LIGHT WIRE, IMPROVED CONNECTION ATA :77 WA-1 THRU WA-312SI NO. 1246 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR AN IMPROVED CONNECTION FOR THELANDING LIGHT WIRE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

77-4002-1 SELEVATOR TRIM TAB CABLE AND DRUM REPLACEMENT ATA :77 WA-1 THRU WA-41SI NO. 1194 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE ORIGINAL PARTS WITH ACHAIN AND SPROCKET SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

77-4004-1 PTAIL SKID INSTL ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

77-4006-1 SBALANCE WEIGHT, RUDDER REINFORCED ATTACHMENT ATA :77 WA-1 THRU WA-312SI NO. 1256 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR REINFORCED ATTACHMENT OF THERUDDER BALANCE WEIGHT TO THE RUDDER LEADING EDGE SKIN.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

77-4007-1 SRUDDER HINGE PIN BUSHING INSTALLATION ATA :77 WA-1 THRU WA-312THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BUSHINGS AROUND THE 108-630010-1 UPPERRUDDER HINGE PIN AS AN ALTERNATE REPLACEMENT TO ACTUAL CHANGE OF THE 108-630010-1 PIN ONTO PREVENT RUDDER FLUTTER OR VIBRATIONS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: YOU WILL ALSO REQUIRE THE FOLLOWING ITEMS NOT FURNISHED WITH KIT TO MAKETHIS INSTALLATION: EA9309 QT OR EA9309 6 OZ ADHESIVE, EC3911 PT OR EC3911 QTAND 100 GRIT SANDPAPER. IF NOT IN YOUR SHOP STOCK, PROCURE LOCALLY.

NOTENOTENOTENOTE:::: AIRCRAFT MUST HAVE A SERVICEABLE 108-630010-1 RUDDER PIN TO USE THIS KIT. YOUNEED TO CONTACT PRODUCT SUPPORT. IF YOU CAN NOT OBTAIN OR ARE NOT SUREYOU HAVE A SERVICEABLE RUDDER PIN.



KIT CATALOG

77-8001-1 SLANDING GEAR ATTACHMENT POINT ATA :77 WA-1 THRU WA-312SI NO. 1218 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO IMPROVE THE STRUCTURAL INTEGRITYOF THE NOSE LANDING GEAR ATTACH POINT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

77-8003-1 SLANDING GEAR, ELLIPTICAL BUSHING RETAINER INSTALLATION ATA :77 WA-1 THRU WA-312SB NO. 2003 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A RETAINER FOR THEELLIPTICAL BUSHINGS ON THE MAIN LANDING GEAR STRUT ASSEMBLIES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 14MEN : 1 (MAN)

77-9001-1 SENGINE MOUNT, REPLACEMENT ATA :77 WA-1 THRU WA-312SI NO. 1233 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A NEW IMPROVEDREPLACEMENT ENGINE MOUNT ASSEMBLY, AND TO ENSURE CLEARANCE BETWEEN THE ENGINE MOUNTAND ENGINE CONTROL LINKAGE.WT. CHANGE : WT: +2.5 LBS @ 46.5 ARM 116.25 MOMENTEST. MAN/HRS: : 17MEN : 1 (MAN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberEXTERIOR MARKING "BEECHCRAFT" LOGO - (101-2003-1 S) 1

EMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH - (101-3039-1 S) 1

TIME INDICATOR INSTALLATION - (101-3066-3 P) 1


EMERGENCY LOCATOR TRANSMITTER - SPARES - (101-3127-1 S) 1

ANTENNA MARKER BEACON INSTALLATION - (101-3170-1 S) 2




HEATER PILOT INSTL(COMM KIT) - (33-2- P) 2



EXTERNAL POWER RECEPTACLE (28-VOLT) - (33-3008-1 P) 3

AIR CONDITIONING WIRING MODIFICATION - (33-3009-1 S) 3

AIR CONDITIONING WIRING MODIFICATION - (33-3009-3 S) 3

LATCH, SECONDARY DOOR INSTALLATION, BAGGAGE - (33-4001-1 S) 4

AERODYNAMIC COMPONENT INSTALLATION, SPIN CHARACTERISTICS - (33-4002-1 S) 4

AERODYNAMIC COMPONENT INSTALLATION, SPIN CHARACTERISTICS - (33-4002-3 S) 4

VORTEX GENERATOR, TEMPLATE ASSEMBLY - (33-4003-1 S) 4

STIFFENER INSTALLATION - (33-4006-1 S) 5

STIFFENER INSTALLATION - (33-4006-3) 5

ABSORBER, DYNAMIC NOSE AREA MODIFICATION - (33-4007-1) 5

GYRO, DIRECTIONAL - SPARES - (33-5007-1 S) 5

GYRO, HORIZON - SPARES - (33-5007-3 S) 5

RUDDER SPAR UPRSECT REPLACEMENT - (33-6000-1 S) 6

RUDDER STRUCTURAL MODIFICATIONS - (33-6001-1 S) 6

BRAKE, DUAL INSTALLATION - (33-8002-1 P) 6

DUAL BRAKE INSTL - (33-8002-3 P) 6

FUEL MIXTURE CONTROL ASSEMBLY, (REPLACES 33-380005-1 MIXTURE CONTROL) - (33-9003-1 S) 6


SHROUD INSTL (BREAKDOWN) - (33-910000-13) 7

BAFFLE ASSEM BD - (33-910010-77) 7

B.D. RIB ASSEM - (35-115130-655) 7


KIT-S-EXT PLAC*RA* - (35-2004-3 S) 7

KIT-S-EXT PLACARDS - (35-2004-5 S) 7




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberINTERIOR PLACARD - (35-2005-1 S) 8


OVERVOLTAGE RELAY - (35-3013-1 S) 8

LANDING GEAR RETRACT RELAY (WITHOUT MAGIC HAND INSTALLED) - (35-3015-1 S) 8

LANDING GEAR RETRACT RELAY (WITHOUT MAGIC HAND INSTALLED) - (35-3015-5 S) 9

LANDING GEAR RETRACT RELAY (WITH MAGIC HAND INSTALLED) - (35-3015-7 S) 9

IGNITION SWITCH - (35-3019-1 S) 9

FUEL TRANSMITTER REPLACEMENT - (35-3020-1 S) 10

LANDING GEAR WARNING HORN INSTALLATION - SPARES - (35-3023-1 S) 10

OUTBOARD WING SPAR (REWORK INFORMATION) - (35-4008-1 S) 10

NOSE LANDING GEAR DRAG LEG REPLACEMENT - (35-4012-1 S) 10

WINDOW 3RD TEAR DROP INSTALLATION (TINTED) - (35-4014-3 S) 11

STABILIZER REINFORCEMENT - (35-4016-3 S) 11

STABILIZER REINFORCEMENT - (35-4016-5 S) 11

V-TAIL STABILIZER REINFORCEMENT - (35-4016-7 S) 11

V-TAIL STABILIZER REINFORCEMENT - (35-4016-9 S) 12

INSPECTION MANUAL - (35-4017-1) 12

DOOR INSTL-NOSE WH B.D. - (35-410077-29) 12

EXTERNAL POWER RECEPTACLE (RH) (14-VOLT SYSTEM) - (35-5000-2 P) 12

EXTERNAL POWER RECEPTACLE (RH) (14-VOLT SYSTEM) - (35-5000-6 P) 12

STATICSDCH - (35-5010-1 P) 13

EMERGENCY STATIC AIR SOURCE - (35-5013-1 S) 13

SHOULDER HARNESS (BEIGE) - (35-5034-1 P) 13

SHOULDER HARNESS (BLACK) - (35-5034-3 P) 13

SHOULDER HARNESS (BEIGE) PILOT AND COPILOT - (35-5034-5 P) 14

SHOULDER HARNESS (BLACK) PILOT AND COPILOT - (35-5034-7 P) 14

DOOR HANDLE, INSIDE CABIN REPLACEMENT - SPARES - (35-5050-1 P) 15

KIT-S-NS GR RT PLG - (35-619- S) 15

NOSE LANDING GEAR RETRACT ROD PLUNGER - (35-8007-1 S) 15

NOSE LANDING GEAR GREASE SEAL INSTALLATION, WHEEL BEARING - (35-8008-1 S) 15

MAIN LANDING GEAR GREASE SEAL INSTALLATION, WHEEL BEARING - (35-8008-3 S) 16

LANDING GEAR STEERING ARM DUST BOOT INSTALLATION - SPARES - (35-8009-1 S) 16

LANDING GEAR RETRACT ROD DUST BOOT INSTALLATION - SPARES - (35-8009-3 S) 16

MAIN LANDING GEAR WHEEL BEARING REPLACEMENT - (35-8010-1 S) 17

MAIN WHEEL BEARING REPLACEMENT - (35-8010-3 S) 17

FUEL CELL INSTALLATION - (35-9009-1 S) 17




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFUEL CELL INSTALLATION - (35-9009-3 S) 18



ENGINE INSTRUMENT CLUSTER REPLACEMENT - (35-9014-1 S) 18





ENGINE INSTRUMENT CLUSTER INSTALLATION - (35-9014-9 S) 20

EXHAUST STACK INSTALLATION - SPARES - (35-9016-1 S) 20



FUEL BOOST PUMP INSTALLATION - (35-9017-1 P) 21

FUEL FLOW TRANSDUCER REPLACEMENT - (35-9018-1 S) 21


INTERIOR PLACARDS - (36-2003-1 S) 22


INSTRUMENT CLUSTER INSTALLATION, ROUND, LIGHTED (WITHOUT E.G.T.) - (36-3002-1 M) 22

ALTERNATOR, 100-AMP (24-VOLT) - (36-3004-1 P) 22

STANDBY GENERATOR (28-VOLT 6.5 AMP) - (36-3006-1 P) 23

STARTER RELAY INSTALLATION - SPARES - (36-3008-1 S) 23

STANDBY GENERATOR INSTALLATION (28-VOLT) - (36-3010-1 P) 23

STANDBY GENERATOR 28 VOLT - (36-3010-3 P) 24

AIR COND TIMEDELAY RELAY - (36-3011-1 S) 24

WARNING HORN, FULL FLAP - (36-3012-1 S) 24

LANDING GEAR WARNING LIGHT - (36-3013-1 S) 25

LANDING GEAR RETRACT PREVENTION, RELAY INSTALLATION, LOW THROTTLE - (36-3014-1 S) 25

AIR CONDITIONER TIME DELAY RELAY - (36-3015-1 S) 25

AIR PRESSURE SYSTEM REGULATOR RELOCATION - (36-3016-1 M) 26

LANDING GEAR WARNING LIGHT - (36-3016-3 M) 26

LANDING GEAR RETRACT PREVENTION RELAY INSTALLATION, LOW THROTTLE GEAR WARNING - (36-3017-1S)

26

TACHOMETER INDICATOR - SPARES - (36-3018-1 S) 26

AIR PLUMBING INSTRUMENT - (36-3019-1 S) 27

ELT REMOTE SWITCH INSTALLATION, COCKPIT AREA - (36-3020-1 S) 27

LANDING LIGHT RESISTOR INSTALLATION - (36-3021-1) 27

STATIC WICK B.D. - (36-360024-7) 27

B.D. STATIC WICK RUDDER - (36-360024-9) 28



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSPAR, FRONT CARRY THRU REINFORCEMENT - (36-4004-1 S) 28

FRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT - (36-4004-11 S) 28

SPAR CARRY THRU STRUCTURE REINFORCEMENT, FRONT - (36-4004-13 S) 28




FRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT - (36-4004-9 S) 30

CABIN DOOR OVER CENTER THIRD LATCH POINT INSTALLATION - (36-4007-1 S) 30


BLOWER, FRESH AIR INSTALLATION - SPARES - (36-4009-1 S) 31

FIFTH AND SIXTH SEAT ATTACHMENT - (36-4012-1) 31

SIXTH SEAT ATTACHMENT - (36-4012-11) 31




FIFTH SEAT ATTACHMENT - (36-4012-19) 33





FIFTH SIXTH SEAT ATTACHMENT - (36-4012-9) 34

CABIN DOOR SEAL - (36-4013-1) 35

OPENABLE WINDOW SEAL - (36-4014-1) 35

SEALS, UTILITY DOOR - (36-4015-1) 35

LANDING LIGHT ASSY IMPROVEMENT - (36-4016-0001) 36

FUEL SELECTOR VALVE, STOP INSTALLATION - (36-5006-1 S) 36

OXYGEN FILLER TUBE INSTALLATION - SPARES - (36-5007-1 S) 36

STANDBY AIR PRESSUSYSTEM (COMM KIT - (36-5009-3 P) 36

AIR CONDITIONER EXPANSION VALVE INSTALLATION - (36-5010-1 S) 37



MANIFOLD INSTALLATION - STANDBY AIR PRESSURE - (36-5014-1 P) 37

INFORMATION-STANDBY AIR PRESSURE SYSTEM INSTALLATION - (36-5015-1 P) 38

FIRE EXTINGUISHER REPLACEMENT - (36-5017-1 S) 38

AIR CONDITIONER INSTALLATION - (36-5019-1 P) 38

AIR CONDITIONER CONDENSER COIL REPLACEMENT - SPARES - (36-5022-1 S) 38

ELEVATOR TAB POSITION RETAINER - (36-5023-1 S) 39



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberAILERON CONTROL PUSH ROD - (36-5024-1 S) 39

FIRE EXTINGUISHER - SPARES - (36-5025-1) 39

COVER ASSEMBLY, RH CONTROL WHEEL - (36-5027-1) 39

G36/G58 MODEL NAME EMBLEM INSTL - (36-5040-0001) 40

SPEAKER - (36-530168-1) 40

BRAKE, COPILOT INSTALLATION - (36-8003- P) 40

NOSE LANDING GEAR, SHAFT, ROLLER ASSEMBLY, RETRACTION MECHANISM IMPROVEMENT - (36-8005-1) 40

PROP DEICE ELECTROTHERMAL - (36-9003-1 P) 41

PROP DEICE, ELECTRIC, MCCAULEY PROPELLER (28-VOLT) - (36-9003-3 P) 41

PROP DEICE, ELECTRIC, HARTZELL PROP (28-VOLT) - (36-9004-1 P) 41

OIL DRAIN INSTALLATION, TURBOCHARGER - (36-9006-1 S) 42

DRAIN VALVE INSTALLATION - SPARES - (36-9007-1 S) 42

MAGNETO INSTALLATION PRESSURIZED - (36-9011-1 S) 42

MAGNETO INSTALLATION PRESSURIZED - (36-9011-3 S) 42

PROP DE-ICE ELECTROTHERMAL - (36-9012-1 P) 43

PROP DE-ICE ELECTROTHERMAL - (36-9012-3 P) 43

ENGINE COOLING I0550 ENGINE - (36-9013-1 S) 43

AIRCRAFT CONVERSION FROM A36AT TO A36 - (36-9014-1 S) 43

ENGINE COOLING I0550 ENGINE - (36-9015-1 S) 44

OVERVOLTAGE RELAY INSTALLATION - (55-3017-1 S) 44

FUEL TRANSMITTER INSTALLATION - (55-3019-1 S) 44

FUEL QUANTITY CIRCUIT BOARD INSTALLATION - (55-3023-3 S) 44

PRINTED CIRCUIT BOARD INSTALLATION - (55-3025-1 S) 45

CLOCK INSTALLATION, CONTROL WHEEL (14-VOLT) - (55-3028-1 P) 45

CLOCK INSTALLATION, CONTROL WHEEL (28-VOLT) - (55-3028-3 P) 45

CLOCK INSTALLATION, INSTRUMENT PANEL - SPARES (14-VOLT) - (55-3029-1 P) 46

CLOCK INSTALLATION, INSTRUMENT PANEL - SPARES (28-VOLT) - (55-3029-3 P) 46

WINDSHIELD INSTALLATION - ONE PIECE - (55-4016- P) 46

SHOULDER HARNESS INSTALLATION (BEIGE) - (55-5012-1 P) 46

SHOULDER HARNESS INSTALLATION (BLACK) - (55-5012-3 P) 47

SHOULDER HARNESS INSTALLATION (BLACK) - (55-5012-5 P) 47


INSTRUMENT AIR PUMP INSTALLATION (FOR AIRPLANES EQUIPPED WITH 224CW OR 232CW PUMP) -(55-9012-1 S)

48

FUEL TRANSMITTER REPLACEMENT FOR INBOARD OR OUTBOARD, 39 OR 40 GALLON CAPACITY FUELCELLS, LH OR RH, WITH A.C. GAGES - (55-9018-1 S)

48

FUEL TRANSMITTER REPLACEMENT LH WITH A.C. GAGES - (55-9018-3 S) 48

FUEL TRANSMITTER REPLACEMENT RH 25-GALLON CAPACITY WITH A.C. GAGES - (55-9018-4 S) 49



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberANTENNA REPLACEMENT B-6 - (58-3003-1 S) 49

ANTENNA, VHF, COMM INSTALLATION - (58-3010-1 S) 49

SEAT TIE DOWN, AFT - (58-4003-1 S) 49

LOCK ASSEMBLY INSTALLATION, NOSE BAGGAGE DOOR, CABIN DOOR, UTILITY DOOR - (58-4011-3) 50




SHOULDER HARNESS INSTALLATION (5TH SEAT ONLY) - (58-5009-11 P) 51





LANDING GEAR SWITCH GUARD INSTALLATION - (58-8001-1 S) 52

BRUSH BLOCK ASSEMBLY, MODULAR - (90-3085-1 S) 52

WING ATTACH FITTING - (90-4111-1 S) 52


ACTUATOR ASSY, SEAL REPLACEMENT - (95-8100-0001) 53


KIT CATALOG

101-2003-1 SEXTERIOR MARKING "BEECHCRAFT" LOGO ATA :F33A, F33C, A36, B36TCTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE101-531347-1 PLACARD.

NOTENOTENOTENOTE:::: MASKS FURNISHED IN THIS KIT ARE DESIGNED FOR SINGLE COLOR LETTER PAINTING.NOTENOTENOTENOTE:::: PAINT IS NOT INCLUDED IN THE KIT. PROCURE LOCALLY BEECHCRAFT RED "P/N 2351".

WT. CHANGE : N/AEST. MAN/HRS: : 1 TO 2MEN : 1 (MAN)

101-3039-1 SEMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH ATA :SI NO. 1139, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REMOTE SWITCH FOR THE TR70-13 E.L.T.ON ALL INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : N/A

101-3066-3 PTIME INDICATOR INSTALLATION ATA :33, 35, 36THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ELAPSED TIME INDICATORACROSS ALL 28-VDC ELECTRIC EQUIPMENT REQUIRING INSPECTION EVERY 2,000 HOURS OR LESS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3066-5 PTIME INDICATOR INSTALLATION ATA :33, 35, 36THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ELAPSED TIME INDICATORACROSS ALL 28-VDC ELECTRIC EQUIPMENT REQUIRING INSPECTION EVERY 10,000 HOURS OR LESS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3127-1 SEMERGENCY LOCATOR TRANSMITTER - SPARES ATA :WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-3170-1 SANTENNA MARKER BEACON INSTALLATION ATA :F33A, F33C, G33, V35B, A36, A36TC, B36TC,THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION FOR SPARES REPLACEMENT OF100-384120 MARK BEACON ANTENNA WITH A 101-384179 MARKER BEACON ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10 TO 12MEN : 1 (MAN)

101-3227-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN VHF FORMAT.



101-3227-3ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN PAL FORMAT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES FOR PROPER ELECTRICAL BONDING TO METALS ON ALL NON-COMPOSITEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

33-2- PHEATER PILOT INSTL(COMM KIT) ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

33-2002-1 SEXTERIOR PLACARD ATA : 1133 THRU G33, C33A THRU F33A AND E33CTHRU F33CTHIS KIT INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVEEXTERIOR PLACARDS, INSTRUCTIONS AND A SPRAY CAN OF PROTECTIVE FINISH.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

33-2003-1 SINTERIOR PLACARD ATA : 1133 THRU G33,C33A THRU F33AE33C THRU F33CTHIS KIT INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVEINTERIOR PLACARDS AND INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

33-3008-1 PEXTERNAL POWER RECEPTACLE (28-VOLT) ATA : 24A36 E-1111, E-1241 AND AFTERA36TC AND B36TC EA- AND AFTER PERCHANGE ORDER F05716 TO KIT DRAWING.F33A CE-748, CE-772 AND AFTERF33C CJ-149 THRU CJ-155V35B D-10097, D-10120 AND AFTERADD THE CONVENIENCE OF AN EXTERNAL POWER RECEPTACLE TO YOUR AIRPLANE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

33-3009-1 SAIR CONDITIONING WIRING MODIFICATION ATA : 2433, 36 CE-290 THRU CE-1036, CJ-26 THRU CJ-179,

E-185 THRU E-2103, E-2105 THRU E-2110,EA-1 THRU EA-463

SB NO. 2282THIS KIT PROVIDES THE PARTS AND NECESSARY INFORMATION TO INSTALL ATIME DELAY RELAY IN THE AIR CONDITIONING ELECTRICAL CIRCUIT ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

33-3009-3 SAIR CONDITIONING WIRING MODIFICATION ATA : 24F33A, F33C, A36, A36TC, B36TC CE-290 THRU CE-1125, CJ-26 THRU CJ-179,

E-185 THRU E-2103, E-2105 THRU E-2110,EA-1 THRU EA-463

SB NO. 2282THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO MODIFY THE AIR CONDITIONINGELECTRICAL CIRCUIT WIRING ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 3MEN : 1 (MAN)


KIT CATALOG

33-4001-1 SLATCH, SECONDARY DOOR INSTALLATION, BAGGAGE ATA : 52F33A CE-809, CE-828 AND AFTERF33C CJ-149 AND AFTERV35B D-10196 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SECONDARY BAGGAGE DOOR LATCH ONAIRPLANES EQUIPPED WITH A UTILITY BAGGAGE DOOR.

ADD A SAFETY FEATURE TO YOUR PRESENT BAGGAGE DOOR RELEASE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

33-4002-1 SAERODYNAMIC COMPONENT INSTALLATION, SPIN CHARACTERISTICS ATA : 52F33C CJ-39, CJ-52 THRU CJ-155THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AERODYNAMIC COMPONENTS.KIT NO. 33-4003 (NOT INCLUDED IN KIT 33-4002) IS REQUIRED FOR CORRECT INSTALLATION OFCOMPONENTS THAT ARE A PART OF KIT 33-4003.

SEE 33-4002-3 S ON SSTX AND SERVICE INNOTENOTENOTENOTE:::: 33-4003-1 S KIT WILL BE REQUIRED TO PURCHASED ALSO TO ACCOMPLISH THIS KIT

INSTALLATION.WT. CHANGE : WT: + 2.0 LBS \@ + 139 ARM + 278 MOMENTEST. MAN/HRS: : 92MEN : 1 (MAN)

33-4002-3 SAERODYNAMIC COMPONENT INSTALLATION, SPIN CHARACTERISTICS ATA : 51E33C, F33C CJ-1 THRU CJ-51, EXCEPT CJ-39 (SEE -1 S

KIT)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AERODYNAMIC COMPONENTS.KIT P/N 33-4003-1 S (NOT INCLUDED IN 33-4002KITS) IS REQUIRED FOR CORRECT INSTALLATION OF COMPONENTS THAT ARE A PART OF KIT 33-4003.SEE SERVICE INSTRUCTION NO. 1249 FOWT. CHANGE : WT: + 6.7 LBS \@ + 106 ARM + 710 MOMENTEST. MAN/HRS: : 92MEN : 1 (MAN)

33-4003-1 SVORTEX GENERATOR, TEMPLATE ASSEMBLY ATA : 57E33C, F33C CJ-1 THRU CJ-155THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR ASSEMBLING THE VORTEX GENERATORTEMPLATE. KIT NO. 33-4002 (NOT INCLUDED IN KIT 33-4003) IS TO BE USED ONLY FOR INSTALLINGVORTEX GENERATORS THAT ARE A PART OF KIT 33-4002.

REQUIRED TO INSTALL 33-400WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

33-4006-1 SSTIFFENER INSTALLATION ATA : 53F33A CE-290 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" TO FABRICATE AND INSTALL ADDITIONAL STIFFENERS ON THEFIREWALL, NOSE WHEEL WELL, LOWER FUSELAGE SKIN AND ADD AN ADDITIONAL FASTENER TO THE LHFORWARD FLOORBOARD.WT. CHANGE : WEIGHT AND BALANCE CHANGE TO BE THE RESPONSIBILITY OF THE INSTALLER AND TO BE

DETERMINED AT INSTALLATION.EST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

33-4006-3STIFFENER INSTALLATION ATA : 53A36 E185 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" TO FABRICATE AND INSTALL ADDITIONAL STIFFENER ON THEFIREWALL, NOSE WHEEL WELL AND LOWERFUSELAGE SKIN ON INSERVICE AIRCRAFT.WT. CHANGE : WEIGHT AND BALANCE CHANGE TO BE THE RESPONSIBILITY OF THE INSTALLER AND TO BE

DETERMINED AT INSTALLATION.EST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

33-4007-1ABSORBER, DYNAMIC NOSE AREA MODIFICATION ATA : 71F33A CE-1671THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO IMPROVE THE VIBRATIONCHARACTERISTICS.WT. CHANGE : WT: 3.0 LBS; MOMENT: 100 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

33-5007-1 SGYRO, DIRECTIONAL - SPARES ATA : 31A33, B33, C33, C33A ALLN35, P35, S35, V35, V35TC ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE DIRECTIONAL GYRO P/N 35-380039-1 OR50-380007-7 ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

33-5007-3 SGYRO, HORIZON - SPARES ATA : 31A33, B33, C33, C33A ALLP35, S35, V35, V35TC ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE HORIZON GYRO P/N 35-380043-1 OR50-380008-7 ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

33-6000-1 SRUDDER SPAR UPRSECT REPLACEMENT ATA : 55WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

33-6001-1 SRUDDER STRUCTURAL MODIFICATIONS ATA : 5535-33, 35A33, 35B33, 35C33, E33, F33, G33 CD-1 THRU CD-130436, A36 E-1 THRU E-2518A36TC, B36TC EA-1 THRU EA-500E33C, F33C CJ-1 THRU CJ-179THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RUDDER SPAR AND HINGE BRACKETSON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 48 TO 60MEN : 2 (MEN)

33-8002-1 PBRAKE, DUAL INSTALLATION ATA : 32B33, G33 CD-736 THRU CD-1304C33A THRU F33A TO SERIAL CE-301E33C THRU F33C TO SERIAL CJ-26P35 THRU V35B TO SERIAL D-9125THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DUAL BRAKE SYSTEM.EQUIPPED WITH DUAL CONTROL PROVISIONS.WT. CHANGE : WT: + 4 LBS @ MOMENT + 216 IN.-LBSEST. MAN/HRS: : 30MEN : 1 (MAN)

33-8002-3 PDUAL BRAKE INSTL ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

33-9003-1 SFUEL MIXTURE CONTROL ASSEMBLY, (REPLACES 33-380005-1 MIXTURECONTROL)

ATA : 76

B33THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED MIXTURE CONTROL CABLE FOREASIER OPERATION AND LONGER SERVICE LIFE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

33-9003-3 SFUEL MIXTURE CONTROL ASSEMBLY ATA : 7633, A33THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE MIXTURE CONTROL ASSEMBLY, P/N WC154-5 AND WC 154-5-50.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

33-910000-13SHROUD INSTL (BREAKDOWN) ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

33-910010-77BAFFLE ASSEM BD ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-115130-655B.D. RIB ASSEM ATA : 57WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-2004-1 SEXTERIOR PLACARD ATA : 11K35 THRU V35B-TC D-5726 AND AFTERINCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVE EXTERIORPLACARDS, INSTRUCTIONS, AND A SPRAY CAN OFPROTECTIVE FINISH.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

35-2004-3 SKIT-S-EXT PLAC*RA* ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-2004-5 SKIT-S-EXT PLACARDS ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

35-2004-7 SEXTERIOR PLACARD ATA : 1135 THRU J35 D-1 THRU D-5725INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVE EXTERIORPLACARDS, INSTRUCTIONS, AND A SPRAY CAN OFPROTECTIVE FINISH.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

35-2005-1 SINTERIOR PLACARD ATA : 11K35 THRU V35B D-5726 AND AFTERTHIS KIT CONTAINS A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVEINTERIOR PLACARDS AND INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

35-2005-5 SINTERIOR PLACARD ATA : 1135 THRU J35 D-1 THRU D-5725INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVE INTERIORPLACARDS AND INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

35-3013-1 SOVERVOLTAGE RELAY ATA : 2433, 35, 36THIS KIT PROVIDES THE PARTS AND INFORMATION TO REPLACE THE RBM RELAY P/N 138-1WITH A NEWRELAY P/N 36-380032-1.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

35-3015-1 SLANDING GEAR RETRACT RELAY (WITHOUT MAGIC HAND INSTALLED) ATA : 24A36 E-710, E-763 THRU E-901, E-903 THRU E-926F33A CE-613 THRU CE-673F33C CJ-105 THRU CJ-128V35B D-9818 THRU D-9947SI NO. 0943 REV. 1, CLASS II(TO PREVENT VOLTAGE DROP) KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RELAY FORLANDING GEAR RETRACT THAT FACTORY INSTALLED DUAL SQUAT SWITCHES (WITHOUT THE MAGICHAND).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)


KIT CATALOG

35-3015-5 SLANDING GEAR RETRACT RELAY (WITHOUT MAGIC HAND INSTALLED) ATA : 24A36 E-606 THRU E-709, E-711 THRU E-762F33A CE-538 THRU CE-541, CE-543, CE-545,

CE-546, CE-548 THRU CE-612F33C CJ-62 THRU CJ-66, CJ-69 THRU CJ-74, CJ-77

THRU CJ-104V35B D-9691 THRU D-9817SIS NO. 0943, REV. 1, CLASS II(TO PREVENT VOLTAGE DROP) KIT PROVIDES PARTS AND INFORMATION TO INSTALL RELAY FORLANDING GEAR RETRACT THAT HAVE FACTORY INSTALLED DUAL SQUAT SWITCHES (WITHOUT MAGICHAND).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

35-3015-7 SLANDING GEAR RETRACT RELAY (WITH MAGIC HAND INSTALLED) ATA : 24A36 E-606 THRU E-709, E-711 THRU E-762F33A CE-538 THRU CE-541, CE-543, CE-545,

CE-546, CE-548 THRU CE-612F33C CJ-62 THRU CJ-66, CJ-69 THRU CJ-74, CJ-77

THRU CJ-104V35B D-9691 THRU D-9817SI NO. 0943 REV. 1, CLASS IITHE LANDING GEAR CONTROL CIRCUIT IS MODIFIED BY A RELAY TO REDUCE THE VOLTAGE DROP TOTHE LANDING GEAR RETRACT MOTOR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

35-3019-1 SIGNITION SWITCH ATA :THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE COMPONENTS OF THE MALLORY SWITCH P/N VB-6532. THIS KIT DOES NOT INCLUDE IGNITION LOCK CYLINDER WITH KEYS.

THIS KIT CONSIST OF A SWITCH AND CERAMIC SECTIONS TO MODIFY YOUR ORIGINAL IGNITION SWITCH.NOTENOTENOTENOTE:::: IF DESIRE IGNITION LOCK CYLINDER WITH 2 KEYS SEE P/N F-6600-CX2 AND YOUR 35

THRU G35 PARTS CATALOG. DEPENDING ON YOUR AIRCRAFT SERIAL NUMBER, YOU MAYREQUIRE P/N 35-590070 WITH 2 KEYS, 35-364055 CONNECTOR, OR 10-357200-1 SWITCHAND LOCK WITH 2 KEYS.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)


KIT CATALOG

35-3020-1 SFUEL TRANSMITTER REPLACEMENT ATA :36 E-1 THRU E-184B33, C33 AND E33 CD-626 THRU CD-1234C33A AND E33A CE-1 THRU CE-235, CE-249, CE-250, CE-256,

CE-260, CE-264 THRU CE-268, CE-270 THRUCE-289

P35, S35, V35, V35TC, V35A, V35A-TC D-7080 THRU D-9068SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT REPLACES THE ORIGINAL A.C. BRAND EQUIPMENT IN THE FUEL QUANTITY INDICATING SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-3023-1 SLANDING GEAR WARNING HORN INSTALLATION - SPARES ATA :35 THRU P35THIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 318, 319, 35-364134 AND 35-364134-652 LANDINGGEAR WARNING HORN INSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-4008-1 SOUTBOARD WING SPAR (REWORK INFORMATION) ATA :33 THRU G3335 THRU V35B36 THRU A36THIS KIT PROVIDES THE NECESSARY INFORMATION TO INSTALL A NEW COMMONALITY OUTBOARD WINGSPAR. SPAR ASSEMBLY AND INSTALLATION HARDWARE ARE NOT PART OF THIS KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-4012-1 SNOSE LANDING GEAR DRAG LEG REPLACEMENT ATA :36, A36 E-1 THRU E-1102A33 THRU G33C33A THRU F33A CE-1 THRU CE-731E33C, F33C CJ-1 THRU CJ-128N35 THRU V35B D-6562 THRU D-10048INSTALL THE IMPROVED NOSE GEAR BRACE TO IMPROVE STABILITY AND ADD EXTRA SAFETY FEATURESTO YOUR AIRPLANE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-4014-3 SWINDOW 3RD TEAR DROP INSTALLATION (TINTED) ATA :33, A33, B33 CD-1 THRU CD-81335 THRU M35 D-1 THRU D-6561THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO ADD A CUT BACK TEAR DROP THIRDWINDOW THAT ENHANCES THE STYLING OFYOUR AIRPLANE WHILE INCREASING VISIBILITY.

THIS KIT PROVIDES INFORMATION ON INSTALLATION IN AIRCRAFT WITH OR WITHOUT THE SMALLWT. CHANGE : WITH SMALL WINDOW: WT: 5 LBS @ 160 ARM

WITHOUT SMALL WINDOW: WT: 7 LBSEST. MAN/HRS: : 85MEN : 1 (MAN)

35-4016-3 SSTABILIZER REINFORCEMENT ATA :C35, D35, E35, F35, G35 D-2681 THRU D-4865, D-15002SB NO. 2188 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REINFORCE THE STABILIZERS ANDINSTALL A LOADING LIMITATION PLACARD AND REWORK TO REDUCE NOSE-DOWN ELEVATOR TRIM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-4016-5 SSTABILIZER REINFORCEMENT ATA :H35, J35, K35, M35 D-4866 THRU D-6561SB NO. 2188 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REINFORCE THE STABILIZERS ANDINSTALL A LOADING LIMITATION PLACARD AND REWORK TO REDUCE NOSE-DOWN ELEVATOR TRIM.WT. CHANGE : N/AEST. MAN/HRS: : 1MEN : N/A

35-4016-7 SV-TAIL STABILIZER REINFORCEMENT ATA :N35, P35, S35, S35TC, V35, V35-TC, V35A,V35A-TC, V35B, V35-TC

D-6562 THRU D-1040

SB NO. 2188 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REINFORCE THE STABILIZERS ANDINSTALL A LOADING LIMITATION PLACARD AND REWORK TO REDUCE NOSE-DOWN ELEVATOR TRIM.WT. CHANGE : N/AEST. MAN/HRS: : 16MEN : N/A


KIT CATALOG

35-4016-9 SV-TAIL STABILIZER REINFORCEMENT ATA :C35, D35, E35, F35, G35 D-2681 THRU D-4865, D-15002SB NO. 2188 OR SUBSEQUENTTHIS KIT IS REQUIRED ON A LIMITED NUMBER OF AIRPLANES WHICH ARE EQUIPPED WITH ANADDITIONAL STABILIZER ACCESS PLATE. THE ADDITIONAL PLATE IS LOCATED BETWEEN THE FORWARDAND REAR STABILIZER SPARS. EXAMINE INDIVIDIUAL AIRPLANES AND CONFIRM THE NEED FOR THISWT. CHANGE : N/AEST. MAN/HRS: : 2MEN : N/A

35-4017-1INSPECTION MANUAL ATA :SBS NO. 2188 AND KITS 35-4016-3 S, 35-4016-5 S, 35-4016-7 S OR 35-4016-9 SNO PARTS REQUIRED BY LATEST FAA AD NO. 94-20-04 ON V-TAIL BONANZA INSPECTION. THIS 32 PAGEMANUAL SUPPLIES "INFORMATION ONLY" ON EMPENNAGE AND AFT FUSELAGE INSPECTION,INSTRUCTION.

NOTENOTENOTENOTE:::: 35-4017-1 IS FURNISHED AS PART OF 35-4016-3 S, 35-4016-5 S AND 35-4016-7 S KITS BUTNOT WITH 35-4016-9 S KIT.

WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-410077-29DOOR INSTL-NOSE WH B.D. ATA : 52WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-5000-2 PEXTERNAL POWER RECEPTACLE (RH) (14-VOLT SYSTEM) ATA :33 CD-1 THRU CD-73635 D-1117 THRU D-7309THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION TO MAKE AN EXTERNAL POWERRECEPTACLE INSTALLATION ON INSERVICE AIRCRAFT.WT. CHANGE : WT: + 2 LBS @ + 41 ARMEST. MAN/HRS: : 5MEN : 1 (MAN)

35-5000-6 PEXTERNAL POWER RECEPTACLE (RH) (14-VOLT SYSTEM) ATA :33 CE-1 THRU CE-26936, A36F33C CJ-26 AND AFTERV35 D-7977 THRU D-9537ADD A THREE PRONG RECEPTACLE FOR UTILIZATION OF ANY STANDARD EXTERNAL POWER SOURCE.WT. CHANGE : WT: + 2 LBS @ + 41 ARMEST. MAN/HRS: : 5MEN : 1 (MAN)


KIT CATALOG

35-5010-1 PSTATICSDCH ATA : 23WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-5013-1 SEMERGENCY STATIC AIR SOURCE ATA :33 THRU E33C35 THRU V35B (EXCEPT EXTENDEDBAGGAGE)36, A36THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION REQUIRED TO INSTALL AN EMERGENCYSTATIC AIR SOURCE.

NOTENOTENOTENOTE:::: NO FLIGHT MANUAL ORDER NEW, P/N: 35-324428-13.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

35-5034-1 PSHOULDER HARNESS (BEIGE) ATA : 2535 THRU H35, J35, K35, M35 D-1 THRU D-656135-33 CD-1 THRU CD-224, CD-233, CD-234,

CD-236, CD-241, CD-246 THRU CD-250SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES ON PILOT ANDCOPILOT SEATS ON INSERVICE AIRCRAFT. BELTS AND HARNESSES ARE BEIGE.WT. CHANGE : WT: + 4 LBS @ + 97 ARMEST. MAN/HRS: : 24MEN : 1 (MAN)

35-5034-3 PSHOULDER HARNESS (BLACK) ATA :33 THRU B33 CD-1 THRU CD-224, CD-233, CD-234,

CD-236, CD-0241, CD-246 THRU CD-25035 D-1 THRU D-6561SI NO. 1020 AND SB NO. 2031, REV. 2 OR SUBSEQUENTSHOULDER HARNESS KITS ARE COMPLETE WITH PARTS AND INFORMATION AND INERTIA REEL. KIT FITSPILOT AND COPILOT SEATS.

NOTENOTENOTENOTE:::: "M"S.B.#2031 REV 2WT. CHANGE : WT: + 4 LBS @ + 97 ARMEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

35-5034-5 PSHOULDER HARNESS (BEIGE) PILOT AND COPILOT ATA :33, A33, B33, C35 CD-225 THRU CD-232, CD-235, CD-237

THRU CD-245, CD-251 THRU CD-1027C33A CE-1 THRU CE-26N35, P35, S35 D-6562 THRU D-7976SI NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A PILOT AND COPILOT HARNESSASSEMBLY ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "M"S.B.#2031 REV 2WT. CHANGE : WT: + 4 LBS @ + 97 ARMEST. MAN/HRS: : 24MEN : 1 (MAN)

35-5034-7 PSHOULDER HARNESS (BLACK) PILOT AND COPILOT ATA : 2533, A33, B33, C35 CD-225 THRU CD-232, CD-235, CD-237

THRU CD-245, CD-251 THRU CD-1027C33A CE-1 THRU CE-26N35, P35, S35 D-6562 THRU D-7976SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A PILOT AND COPILOT HARNESSASSEMBLY ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: S.B.#2031 REV 28 X 8 X 24

WT. CHANGE : WT: 4 LBS @ 97EST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

35-5050-1 PDOOR HANDLE, INSIDE CABIN REPLACEMENT - SPARES ATA :35-B33 CD-569 THRU CD-81335-C33, 35-C33A, E33, E33A, E33C ALL36, A36TC ALLA36 E-185 THRU E-2579B36TC EA-2 THRU EA-512C35 THRU S35, V35, V35-TC ALLF33 ALLF33A CE-180 THRU CE-1537F33C CJ-126 THRU CJ-179V35A, V35A-TC ALLV35B, V35B-TC ALL"OPTIONAL" SB NO. 2363THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH THE SPARES REPLACEMENT FOR THE INSIDECABIN DOOR HANDLES P/N 35-400436, 95-380010, AND 36-380099-1 ON INSERVICE AIRCRAFT.

FOR AFT UTILITY DOOR HANDLE, USE P/N 2316 OR C100160.NOTENOTENOTENOTE:::: "O"S.B.#2363

EFFECTS 14222 AIRCRAFT, 1 PER AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

35-619- SKIT-S-NS GR RT PLG ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-8007-1 SNOSE LANDING GEAR RETRACT ROD PLUNGER ATA :35 THRU G35SI NO. 1149 OR SUBSEQUENTTHIS KIT PROVIDES AN IMPROVED NOSE GEAR RETRACT ROD PLUNGER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-8008-1 SNOSE LANDING GEAR GREASE SEAL INSTALLATION, WHEEL BEARING ATA :F33A, F33C, V35B, 36, A36, A36TCTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL NOSE WHEEL BEARING THIN LIPGREASE SEALS AS A SPARE REPLACEMENTFOR FELT OR THICK LIP SEALS INSTALLED IN BEECH P/N 36-8002-1 OR CLEVELAND P/N 40-77D AND40-87A WHEEL ASSEMBLIES.

NOTENOTENOTENOTE:::: 1 KIT PER AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-8008-3 SMAIN LANDING GEAR GREASE SEAL INSTALLATION, WHEEL BEARING ATA :F33A, F33C, V35B, 36, A36, A36TCTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL MAIN WHEEL BEARING THIN LIPGREASE SEALS AS A SPARE REPLACEMENTFOR FELT SEALS ON RAYTHEON P/N 36-8001-25 OR CLEVELAND P/N 40-83A WHEEL ASSEMBLY.

NOTENOTENOTENOTE:::: 1 KIT PER AIRCRAFT. TAKES CARE OF 2 WHEELS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-8009-1 SLANDING GEAR STEERING ARM DUST BOOT INSTALLATION - SPARES ATA :33 CD-1 THRU CD-130435 D-1 THRU D-1040736 E-1 THRU E-2073A36TC EA-1 THRU EA-342C33A, E33A, F33A CE-1 THRU CE-1016E33C, F33C CJ-1 THRU CJ-155THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A P/N 36-820026-1 STEERING ARMDUST BOOT AS A SPARE REPLACEMENT FOR P/N 35-825171-9 AND 35-825171-11 BOOTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-8009-3 SLANDING GEAR RETRACT ROD DUST BOOT INSTALLATION - SPARES ATA :33 CD-1 THRU CD-130435 D-1 THRU D-1040736 E-1 THRU E-2073A36TC EA-1 THRU EA-342C33A, E33A, F33A CD-1 THRU CE-1016E33C, F33C CJ-1 THRU CJ-155THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A P/N 36-820023-1 RETRACT RODDUST BOOT AS A SPARE REPLACEMENT FOR THE P/N 35-825076-5, 002-820014-7 AND -11 BOOTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-8010-1 SMAIN LANDING GEAR WHEEL BEARING REPLACEMENT ATA :35B33, P35, S35THIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACEMENT OF 13685X1 CONE AND 13621X1 CUPP/N OF TYSON BEARING COMPANY.KIT PROVIDES (2) BEARINGS AND SEALS AND (2) CUPS FOR REPLACEMENT ON ONE MAIN WHEELASSEMBLY ONLY.

NOTENOTENOTENOTE:::: PENDING "M" S.B. OR COMMTOTAL AIRCRAFT 1698MODELS D95A, 33B33, P35 & S351 KIT PER MAIN WHEEL

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : N/A

35-8010-3 SMAIN WHEEL BEARING REPLACEMENT ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

35-9009-1 SFUEL CELL INSTALLATION ATA :K35, M35, N35, P35, S35, V35, V35A, V35B,36, A36, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, F33, F33A, G33SI NO. 0459-281THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A LH 40 GAL LEADING EDGEFUEL CEL (35-80135-1 OR -5) AND VELCRO PILE ON FUEL CELL LINES ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SI #0459-281WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 2 (MEN)

35-9009-2 SFUEL CELL INSTALLATION ATA :N35, P35, S35, V35, V35A, V35B, 36, A36,35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33,E33A, F33, F33A, G33SI NO. 0459-281THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A RH 40 GAL LEADING EDGEFUEL CELL (35-380135-2 OR -6) AND VELCRO PILE ON FUEL CELL LINERS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: S.I. #0459-281WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 2 (MEN)


KIT CATALOG

35-9009-3 SFUEL CELL INSTALLATION ATA :K35, M35, N35, P35, S35, V35, V35A, V35B,36, A36, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, F33, F33A, G33SI NO. 0459-281THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A LH 25 GAL LEADING EDGEFUEL CELL (96-380046-7 OR -9) AND VELCRO PILE ON FUEL CELL LINERS ON INSERVICE AIRCRAFT ONTHE FRONT SPAR CARRY-THROUGH STRUCTURE.

NOTENOTENOTENOTE:::: SI#0459-281WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 2 (MEN)

35-9009-4 SFUEL CELL INSTALLATION ATA :K35, M35, N35, P35, S35, V35, V35A, V35B,36, A36, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, F33, F33A, G33THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A RH 25 GAL LEADING EDGEFUEL CELL (96-380046-8 OR -10) AND VELCRO PILE ON FUEL CELL LINERS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

35-9009-5 SFUEL CELL INSTALLATION ATA :K35, M35, N35, P35, S35, V35, V35A, V35B,36, A36, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, F33, F33A, G33THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL VELCRO PILE ON LEADING EDGEFUEL CELL LINERS TO ACCOMODATE 35-80135OR 36-380046 FUEL CELLS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

35-9014-1 SENGINE INSTRUMENT CLUSTER REPLACEMENT ATA : 3635 THRU G35 D-1 THRU D-4865SI NO. 0920 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE INSTRUMENT CLUSTERS (FROMAC GAGES TO ROCHESTER GAGES). THE KITMUST BE USED ON INITIAL INSTALLATION. INDIVIDUAL REPLACEMENT IS NOT POSSIBLE UNTIL AFTERTHE APPLICABLE KIT IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : 1 (MAN)


KIT CATALOG

35-9014-13 SENGINE INSTRUMENT CLUSTER REPLACEMENT ATA : 36P35 D-6842 THRU D-7139, D-7141 THRU D-7309

WITH OPTIONAL 39 GAL. FUEL TANKSSI NO. 0920 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE INSTRUMENT CLUSTERS (FROMAC GAGES TO ROCHESTER GAGES). THE KITMUST BE USED ON INITIAL INSTALLATION. INDIVIDUAL REPLACEMENT IS NOT POSSIBLE UNTIL AFTERTHE APPLICABLE KIT IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : 1 (MAN)

35-9014-19 SENGINE INSTRUMENT CLUSTER REPLACEMENT ATA : 3636 E-1 THRU E-184 WITH STANDARD FUEL

TANKSC33A, E33A CE-1 THRU CE-289 WITH STANDARD FUEL

TANKSE33C CJ-1 THRU CJ-25 WITH STANDARD FUEL

TANKSS35, V35, V35A D-7140, D-7310 THRU D-9068 WITH

STANDARD FUEL TANKSSI NO. 0920 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE INSTRUMENT CLUSTERS (FROMAC GAGES TO ROCHESTER GAGES). THE KIT MUST BE USED ON INITIAL INSTALLATION. INDIVIDUALREPLACEMENT IS NOT POSSIBLE UNTIL AFTER THE APPLICABLE KIT IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : 1 (MAN)

35-9014-21 SENGINE INSTRUMENT CLUSTER REPLACEMENT ATA : 36C33A, E33A AND F33C CE-1 THRU CE-289, CJ-1S35, V35, V35A D-7140, D-7310 THRU D-9068 (WITH

OPTIONAL 40 GAL. FUEL SYSTEM)SI NO. 0920 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE INSTRUMENT CLUSTERS. THEKIT MUST BE USED ON ALL INITIAL INSTALLATIONS. INDIVIDUAL REPLACEMENT IS NOT POSSIBLE UNTILAFTER THE APPLICABLE KIT IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : 1 (MAN)


KIT CATALOG

35-9014-3 SENGINE INSTRUMENT CLUSTER REPLACEMENT ATA : 36H35 D-4866 THRU D-5330, EXCEPT D-5062SI NO. 0920 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE INSTRUMENT CLUSTERS (FROMAC GAGES TO ROCHESTER GAGES). THE KIT MUST BE USED ON INITIAL INSTALLATION. INDIVIDUALREPLACEMENT IS NOT POSSIBLE UNTIL AFTER THE APPLICABLE KIT IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : N/A

35-9014-9 SENGINE INSTRUMENT CLUSTER INSTALLATION ATA : 36N35 D-6562 THRU D-6841 (WITH OPTIONAL 39

GALLON FUEL SYSTEM)SI NO. 0920 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE INSTRUMENT CLUSTERS. THEKIT MUST BE USED ON ALL INITIAL INSTALLATIONS.INDIVIDUAL REPLACEMENT IS NOT POSSIBLE UNTIL AFTER THE APPLICABLE KIT IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : 1 (MAN)

35-9016-1 SEXHAUST STACK INSTALLATION - SPARES ATA :33, 35, 36THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A SPARE LEFT HAND EXHAUSTSTACK AS A REPLACEMENT FOR THE P/N35-950005-1 STACK ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30MEN : N/A

35-9016-3 SEXHAUST STACK INSTALLATION - SPARES ATA :33, 35, 36THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A SPARE RIGHT HAND EXHAUSTSTACK AS A REPLACEMENT FOR THE P/N35-950005-3 STACK ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-9016-5 SEXHAUST STACK INSTALLATION - SPARES ATA :35THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A SPARE RIGHT HAND EXHAUSTSTACK WITH PROVISIONS FOR EGT PROBE ASA SPARE REPLACEMENT FOR THE P/N 35-950005-29 STACK ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-9017-1 PFUEL BOOST PUMP INSTALLATION ATA :J35, K35, M35, N35, P35 D-5062, D-5331 THRU D-7139, D-7141 THRU

D-7309THIS KIT IS THE SPARES REPLACEMENT FOR 4032A FUEL BOOST PUMP.WT. CHANGE : SEE KIT DRAWINGEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-9018-1 SFUEL FLOW TRANSDUCER REPLACEMENT ATA :A36 E-185 THRU E-2790F33A CE-290 THRU CE-1730F33C CJ-26 THRU CJ-127V35B D-9069, D-9071 THRU D-9087, D-9089 THRU

D-9106, D-9108 THRU D-9130, D-9132 THRUD-9153, D-9155 THRU D-9179, D-9181 THRUD-10403

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ENGINE FUEL FLOWTRANSDUCER AND A LONGER HOSE ASSEMBLY AS SPARES FOR 102-389012-5, 102-389012-11 AND102-389034-1 TRANSDUCERS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

36-2002-1 SEXTERIOR PLACARD ATA :36 E-1 THRU E-104A36 E-185 AND AFTERA36TC EA-1 THRU EA-241, EA-243 THRU EA-272B36TC EA-242 EA-273 AND AFTERTHIS KIT INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVEEXTERIOR PLACARDS.

NOTENOTENOTENOTE:::: B36TC 36-920046-5 (W-C) OR -7 (B-C) FUEL PLACARD 54GAL/51 USABLE NOT PART OF THISKIT MUST ORDER DESIRED PLACARD AS A SEPARATE ITEM.

NOTENOTENOTENOTE:::: SPRAY CAN OF CLEAR PROTECTIVE FINISH PAINT WAS REMOVED FROM KIT TO REMOVEKIT FROM RESTRICTED ARTICLE KITS, IMPROVED DELIVERY AND LOWER SHIPPING COSTTO CUSTOMER. SPRAY PAINT IS A LOCAL HARDWARE STORE ITEM.



KIT CATALOG

36-2003-1 SINTERIOR PLACARDS ATA :36 AND A36 E-1 THRU E-282 WITHOUT INTERNALLY

LIGHTED PANELSINCLUDES A STANDARD REPLACEMENT SET FOR EASILY INSTALLED, PRESSURE SENSITIVE INTERIORPLACARDS AND INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

36-2003-3 SINTERIOR PLACARDS ATA :A36 E-283 AND AFTER WITHOUT INTERNALLY

LIGHTED PANELSINCLUDES A STANDARD REPLACEMENT SET FOR EASILY INSTALLED, PRESSURE SENSITIVE INTERIORPLACARDS AND INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

36-3002-1 MINSTRUMENT CLUSTER INSTALLATION, ROUND, LIGHTED (WITHOUTE.G.T.)

ATA :

F33A, V35B, A36THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE VERTICAL SCALE ENGINEINSTRUMENTATION WITH THE ROUND TYPE ENGINE INSTRUMENTATION (WITH LIGHTS) ON INSERVICEAIRCRAFT. IF AIRPLANE HAS A E.G.T., KIT NO. 36-3002-3 M IS REQUIRED IN CONJUNCTION WITH THISWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 30 TO 40MEN : 1 (MAN)

36-3004-1 PALTERNATOR, 100-AMP (24-VOLT) ATA :A36 E-1111, E-1241 AND AFTERA36TC EA-1 AND AFTERF33A CE-748, CE-772 AND AFTERF33C CJ-149 AND AFTERV35B D-10097, D-10120 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 100-AMP, 24-VOLT ALTERNATOR.WT. CHANGE : F33A, F33C = WT: + 6.0 LBS @ 11.0 ARM; 66.0 MOMENT

A36, A36TC = WT: + 6.0 LBS @ 11.0 ARM; 66.0 MOMENTV35B = WT: + 6.0 LBS @ 11.0 ARM; 66.0 MOMENT

EST. MAN/HRS: : 24 TO 30MEN : 1 (MAN)


KIT CATALOG

36-3006-1 PSTANDBY GENERATOR (28-VOLT 6.5 AMP) ATA :A36 E-1241 THRU E-2064A36TC, B36TC EA-1 THRU EA-388, EXCEPT EA-320F33A CE-772 AND AFTERF33C CJ-149 AND AFTERV35B D-10120 THRU D-10413THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH A STANDBY GENERATOR FOR INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: FMS 33-590009-25 WILL BE REQUIRED TO COMPLETE INSTALLATION OF THIS KIT. PLEASEORDER SEPARATELY TO ENSURE YOU HAVE THE CURRENT REVISION.

NOTENOTENOTENOTE:::: FOR LATER SERIAL NUMBERS ON A36 AND B36TC, SEE 36-3010-1 P OR 36-3010-3 P.WT. CHANGE : F33A, F33C AND V35B = WT: 11 LBS @ 35

A36, A36TC AND B36TC = WT: 11 LBS @ 45EST. MAN/HRS: : 35 TO 40MEN : 1 (MAN)

36-3008-1 SSTARTER RELAY INSTALLATION - SPARES ATA :33 THRU E33C35 THRU V35B36, A36THIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACEMENT OF SAW4204, SAW9201, 1114213 OR1464, 12 VOLT STARTER RELAY ON INSERVICE AIRCRAFT.


36-3010-1 PSTANDBY GENERATOR INSTALLATION (28-VOLT) ATA :B36TC EA-440 AND AFTERTHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A STANDBY GENERATOR ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT 36-590006-21 WILL BE REQUIRED FOR USAGEWITH THIS KIT INSTALLATION, YOU WILL NEED TO ORDER SEPARATELY WHENORDERING KIT TO GET CURRENT SUPPLEMENT.

NOTENOTENOTENOTE:::: FOR EARLIER MODEL A36 AND B36TC AIRCRAFT SEE 36-3010-3 P KIT. FOR MODELS F33A,F33C, V35B, A36, A36TC AND B36TC WITH 24 VOLT SYSTEM SEE 36-3006-1 P KIT.

WT. CHANGE : WT: 11.0 LBS; ARM: 35 IN.; MOMENT: 385 IN.-LBSEST. MAN/HRS: : 35 TO 40MEN : 1 (MAN)


KIT CATALOG

36-3010-3 PSTANDBY GENERATOR 28 VOLT ATA :A36 E-2104, E-2111 AND AFTERB36TC EA-320, EA-389 THRU EA-439THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A STANDBY GENERATOR ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR MODEL B36TC SERIAL NUMBER, EA-440 AND AFTER SEE 36-3010-1 P KIT. FOREARLIER MODELS F33A, F33C, V35B, A36, A36TC AND B36TC WITH 24 VOLT SYSTEMS, SEEKIT 36-3006-1 P.

NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT 36-590006-21 WILL BE REQUIRED.WT. CHANGE : WT: 11.0 LBS; ARM: 35 IN.; MOMENT: 385 IN.-LBSEST. MAN/HRS: : 35 TO 40MEN : 1 (MAN)

36-3011-1 SAIR COND TIMEDELAY RELAY ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

36-3012-1 SWARNING HORN, FULL FLAP ATA :A36 E-1371 THRU E-2467 EXCEPT E-2458A36TC, B36TC EA-242, EA-273 THRU EA-487F33A CE-816 THRU CE-1306 EXCEPT CE-1301F33C CJ-149 THRU CJ-179V35B D-10179 THRU D-10403SB NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW FLAP DOWN LIMIT SWITCH THAT WILLACTIVATE THE GEAR UP ON.

NOTENOTENOTENOTE:::: 36-590002-47 REQUIRED FOR USE WITH THIS KIT IS NOT FURNISHED AS PART OF THISKIT.



KIT CATALOG

36-3013-1 SLANDING GEAR WARNING LIGHT ATA :A36 E-1111, E-1241 THRU E-2110 EXCEPT

E-1946 AND E-2104A36TC EA-1 THRU EA-272 EXCEPT EA-242B36TC EA-242, EA-273 THRU EA-388 EXCEPT

EA-320F33A CE-748, CE-772 THRU CE-1306 EXCEPT

CE-1301F33C CJ-149 THRU CJ-179V35B D-10120 THRU D-10403SB NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A "GEAR-UP" LANDING GEAR WARNINGANNUNCIATOR LIGHT. THE LIGHT IS TO FLASH WHEN THE LANDING GEAR WARNING HORN SOUNDS.

NOTENOTENOTENOTE:::: WILL REQUIRE 36-590002-49 F.M.S. WHICH IS NOT FURNISHED WITH THIS KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

36-3014-1 SLANDING GEAR RETRACT PREVENTION, RELAY INSTALLATION, LOWTHROTTLE

ATA :

A36 E-1946, E-2104, E-2111 THRU E-2467EXCEPT E-2458

B36TC EA-320, EA-389 THRU EA-487SB NO. 2366 AND SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SWITCH AND A LATCHING RELAY THAT WILLPREVENT THE LANDING GEAR FROM RETRACTING WHEN THE MANIFOLD PRESSURE IS BELOW 17-INCHES OF HG.

NOTENOTENOTENOTE:::: WILL REQUIRE 58-590000-53 F.M.S. WHICH IS NOT FURNISHED WITH THIS KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

36-3015-1 SAIR CONDITIONER TIME DELAY RELAY ATA :(SUPERSEDES 36-3011-1 S KIT.)THIS KIT PROVIDES SPARES PARTS AND INFORMATION TO ALLOW USE OF 76400-200Y RELAY IN PLACEOF TNR 11720 OR TNR/D 11720 S RELAY ON IN SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

36-3016-1 MAIR PRESSURE SYSTEM REGULATOR RELOCATION ATA :A36 E-2217 THRU E-2531 EXCEPT E-2524F33A CE-1056 THRU CE-1456 EXCEPT CE-1440F33A, A36, B36TCF33C CJ-156 THRU CJ-179WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

36-3016-3 MLANDING GEAR WARNING LIGHT ATA :A36 E-1946, E-2104, E-2111 THRU E-2467,

EXCEPT E-2458B36TC EA-320, EA-389 THRU EA-487SB NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A "GEAR-UP" LANDING GEAR WARNINGANNUNCIATOR LIGHT. THE LIGHT IS TO FLASH WHEN THE LANDING GEAR WARNING HORN SOUNDS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

36-3017-1 SLANDING GEAR RETRACT PREVENTION RELAY INSTALLATION, LOWTHROTTLE GEAR WARNING

ATA :

A36 E-1519 THRU E-2110, EXCEPT E-1946 ANDE-2104

F33A CE-862 THRU CE-1306, EXCEPT CE-1301F33C CJ-150 THRU CJ-179V35B D-10249 THRU D-10403SI NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SWITCH AND A LATCHING RELAY THAT WILLPREVENT THE LANDING GEAR FROM RETRACTING WHEN THE THROTTLE IS POSITIONED FOR AMANIFOLD PRESSURE OF 17-INCHES OF HG OR BELOW AND REPLACES THE EXISTING GEAR WARNINGWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

36-3018-1 STACHOMETER INDICATOR - SPARES ATA :A36, B36TCTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 102-380011-23 TACHOMETER ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

36-3019-1 SAIR PLUMBING INSTRUMENT ATA :A36 E1946, E2104, E2111 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO DIRECT STANDBY INSTRUMENT AIR TO NO MORE THANTWO AIR DRIVEN INSTRUMENTS WHEN AIRCRAFTIS EQUIPPED WITH THREE AIR DRIVEN INSTRUMENTS AND THE LARGE CAPACITY ENGINE DRIVE AIRPUMP ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AF3306-2 SCRIM CLOTH AND EA9309 ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY


36-3020-1 SELT REMOTE SWITCH INSTALLATION, COCKPIT AREA ATA :A36 E-2679, E-2682, E-2687, E-2689, E-2721,

E-2724, E-2726, E-2729, E-2732, E-2734,E-2742, E-2745, E-2748,E-2750, E-2751, E-2753, E-2754, E-2757,E-2758,E-2760, E-2826, E-2827

THIS KIT FURNISHES PARTS AND INFORMATION NECESSARY TO INSTALL A REMOTE SWITCH FOR THEARTEX ELT 110-4 EMERGENCY LOCATORTRANSMITTER, IN THE COCKPIT OF THE INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 7 TO 10MEN : 1 (MAN)

36-3021-1LANDING LIGHT RESISTOR INSTALLATION ATA :A36 E-1111, E-1241 AND AFTERA36TC EA-1 THRU EA-241

EA-243 THRU EA-272B36TC EA-242, EA-273 AND AFTERF33A CE-748, CE-772 AND AFTERF33C CJ-149 AND AFTERV35B D-10097, D-10120 AND AFTER"OPTIONAL" SB NO. 2614, SEPTEMBER 1996THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A VOLTAGE DROPPINGRESISTOR TO INCREASE THE LANDING LIGHT LIFE FOR INSERVICE 24 VDC AIRCRAFT EQUIPPED WITH GENO. 4596 LAMP LANDING LIGHT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

36-360024-7STATIC WICK B.D. ATA : 23WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

36-360024-9B.D. STATIC WICK RUDDER ATA : 23WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

36-4004-1 SSPAR, FRONT CARRY THRU REINFORCEMENT ATA :35-33, 35A33, 35B33, 35C33, E33, F33, G33 CD-1 THRU CD-130435C33A, E33A, F33 CE-1 THRU CE-40036 AND A36 E-1 THRU E-379 EXCEPT E-356E33C, F33C CJ-1 THRU CJ-30H35, J35, K35, M35, N35, P35, S35, V35,V35A AND V35B

D-4868 THRU D-9414 EXCEPT D-9379

"MANDATORY" SB NO. 2360THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ONFORWARD FRAME ONLY ON FRONT SPAR CARRY THROUGH STRUCTURE.

KIT SIZE: 1 CARTON, 3 LBS., 14 X 12 X 14NOTENOTENOTENOTE:::: KIT S

WT. CHANGE : DEPENDS ON REPAIRS REQUIREDEST. MAN/HRS: : 60 TO 120MEN : 1 (MAN)

36-4004-11 SFRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT ATA :B36TC EA-242, EA-273 AND AFTER"MANDATORY" SB NO. 2360THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ONFORWARD FRAME ONLY ON FRONT SPAR CARRY THROUGHSTRUCTURE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

36-4004-13 SSPAR CARRY THRU STRUCTURE REINFORCEMENT, FRONT ATA :35-33, 35A33, 35B33, 35C33, E33, F33, G33 CD-1 THRU CD-130435-C33A, E33A, F33A CE-1 THRU CE-400E33C, F33C CJ-1 THRU CJ-30H35, J35, K35, M35, N35, P35, S35, V35,V35A, V35B

D-4866 THRU D-9414, EXCEPT D-9375

SB NO. 2360THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ONREAR FRAME ONLY ON FRONT SPAR CARRY THROUGH STRUCTURE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)


KIT CATALOG

36-4004-3 SSPAR CARRY THRU STRUCTURE REINFORCEMENT, FRONT ATA :36, A36 E-1 THRU E-379, EXCEPT E-356THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ONREAR FRAME ON THE FRONT SPAR CARRY-THROUGHSTRUCTURE.



36-4004-5 SSPAR CARRY THRU STRUCTURE REINFORCEMENT, FRONT ATA :A36 E-356, E-380 THRU E-2397A36TC EA-1 THRU EA-241

EA-243 THRU EA-272F33A CE-401 THRU CE-1192F33C CJ-31 THRU CJ-179V35B D-9379, D-9415 THRU D-10403"MANDATORY" SB NO. 2360THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ONFORWARD FRAME ONLY ON FRONT SPAR CARRY THROUGH STRUCTURE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 40MEN : 1 (MAN)

36-4004-7 SSPAR CARRY THRU STRUCTURE REINFORCEMENT, FRONT ATA :A36 E-356, E-380 THRU E-2397A36TC EA-1 THRU EA-241

EA-243 THRU EA-272F33A CE-401 THRU CE-1193F33C CJ-31 THRU CJ-179V35B D-9379, D-9415 THRU D-10403"MANDATORY" SB NO. 2360THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT ON REARFRAME ONLY ON FRONT SPAR CARRY THROUGH STRUCTURE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 40MEN : 1 (MAN)


KIT CATALOG

36-4004-9 SFRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT ATA :B36TC EA-242, EA-273 AND AFTER"MANDATORY" SB NO. 2360THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ONFORWARD FRAME ONLY ON FRONT SPAR CARRYTHROUGHSTRUCTURE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

36-4007-1 SCABIN DOOR OVER CENTER THIRD LATCH POINT INSTALLATION ATA :A36 E-477 THRU E-2727 EXCEPT E-2711A36TC EA-1 THRU EA-272 EXCEPT EA-242B36TC EA-242, EA-273 THRU EA-536F33A CE-465 THRU CE-1679 EXCEPT CE-1671V35B D-9538 THRU D-10403"MANDATORY" SB NO. 2457, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING THIRD LATCH POINTMECHANISM WITH A THIRD LATCH POINT MECHANISM THAT GOES OVER CENTER WHEN THE DOORLATCH ASSEMBLY IS LATCHED AND REPLACES THE DOOR LATCH MECHANISM STOP.

NOTENOTENOTENOTE:::: IT MAY BE NECESSARY TO MODIFY THE ARM-REST TO INSTALL THIS KIT AS THEBELLCRANK MAY STRIKE THE ARM-REST ON SOME AIRCRAFT. (TIME TO MAKE ANYMODIFICATIONS TO THE ARM-REST NOT INCLUDED IN ESTIMATED MAN-HOURS).


36-4008-1 SCABIN DOOR OVER CENTER THIRD LATCH POINT INSTALLATION ATA :36 E-4 THRU E-184A36 E-185 THRU E-476E33 CD-1171 THRU CD-1234E33A CE-218 THRU CE-289F33 CD-1235 THRU CD-1254F33A CE-290 THRU CE-464G33 CD-1255 THRU CD-1304V35AV35B D-9069 THRU D-9537"MANDATORY" SB NO. 2457, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE EXISTING THIRD LATCHPOINT MECHANISM WITH A THIRD LATCH POINT MECHANISM THAT GOES OVER CENTER WHEN THEDOOR LATCH ASSEMBLY IS LATCHED AND REPLACED, IF REQUIRED, THE DOOR LATCH MECHANISMSTOP

NOTENOTENOTENOTE:::: IT MAY BE NECESSARY TO MODIFY THE ARMREST TO PREVENT BELLCRANK STRIKINGARMREST ON SOME AIRCRAFT (EXTRA TIME ITEM).



KIT CATALOG

36-4009-1 SBLOWER, FRESH AIR INSTALLATION - SPARES ATA :F33A, F33C, A36, A36TC, B36TC"MANDATORY" SB NO. 2380, REV. 2THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FRESH AIR BLOWER ASSEMBLY AS ASPARES REPLACEMENT FOR THE 58-380108-1 OR 169-380096-5 FRESH AIR BLOWER ASSEMBLY ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KITS IS ONLY FOR REF MODELS WITH 28 VOLT SYSTEMS. THE OLD BLOWER P/N'S58-380108-1 OR 169-380096-5 WERE ONLY INSTALLED ON 28 VOLT AIRCRAFT ONREFERENCED MODELS.


36-4012-1FIFTH AND SIXTH SEAT ATTACHMENT ATA : 5336 E-1 THRU E-145"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "AF3306-2" SCRIM CLOTH AND "EA9309" ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


36-4012-11SIXTH SEAT ATTACHMENT ATA : 5336 E-1 THRU E-145A36 E-185 THRU E-571"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE SIXTHSEAT ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AF3306-2 SCRIM CLOTH AND EA9309 ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

36-4012-13FIFTH AND SIXTH SEAT ATTACHMENT ATA : 53A36 E-221 THRU E-571"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS (CLUB SEATING) ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: ?AF3306-2? SCRIM CLOTH AND ?EA9309? ADHESIVE REQUIRED BUT NOT FURNISHEDWITH KIT. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


36-4012-15FIFTH AND SIXTH SEAT ATTACHMENT ATA : 53A36 E-572 THRU E-1370A56TC TG-84 THRU TG-94"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS ON INSERVICE AIRCRAFT.



36-4012-17FIFTH AND SIXTH SEAT ATTACHMENT ATA : 53A36 E-572 THRU E-3193A36TC EA-1 THRU EA-241, EA-243 THRU EA-272A56TC TG-84 THRU TG-94B36TC EA-242, EA-273 THRU EA-620"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS ON INSERVICE AIRCRAFT.




KIT CATALOG

36-4012-19FIFTH SEAT ATTACHMENT ATA : 53A36 E-572 THRU E-3193A36TC EA-1 THRU EA-241, EA-243 THRU EA-272B36TC EA-242, EA-273 THRU EA-620"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHSEAT ON INSERVICE AIRCRAFT.



36-4012-21SIXTH SEAT ATTACHMENT ATA : 53A36 E-572 THRU E-3193A36TC EA-1 THRU EA-241, EA-243 THRU EA-272A56TC TG-84 THRU TG-94B36TC EA-242, EA-273 THRU EA-620"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE SIXTHSEAT ON INSERVICE AIRCRAFT.



36-4012-3FIFTH SEAT ATTACHMENT ATA : 5336 E-1 THRU E-145"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AF3306-2 SCRIM CLOTH AND EA9309 ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

36-4012-5SIXTH SEAT ATTACHMENT ATA : 5336 E-1 THRU E-145"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEAT ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ?AF3306-2? SCRIM CLOTH AND ?EA9309? ADHESIVE REQUIRED BUT NOT FURNISHEDWITH KIT. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY


36-4012-7FIFTH AND SIXTH SEAT ATTACHMENT ATA : 5336 E-146 THRU E-184A36 E-185 THRU E-571"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS ON INSERVICE AIRCRAFT.



36-4012-9FIFTH SIXTH SEAT ATTACHMENT ATA : 5336 E-146 THRUE-184A36 E-185 THRU E-571"MANDATORY" SB NO. 53-3159THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHSEAT ON INSERVICE AIRCRAFT.




KIT CATALOG

36-4013-1CABIN DOOR SEAL ATA :A36 E-754 THRU E-3217A36TC EA-1 THRU EA-241, EA-243 THRU EA-272B36TC EA-242, EA-273 THRU EA-628F33A CE-633 THRU CE-1791V35B D-9819, D-9865 THORUGH D-10403THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEALS ON THE CABIN DOOR.

NOTENOTENOTENOTE:::: S2260 OR 1200 PRIMER AND A400 ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


36-4014-1OPENABLE WINDOW SEAL ATA :A36 E-1212 THRU E-3217A36TC EA-1 THRU EA-241, EA-243 THRU EA-272B36TC EA-242, EA-273 THRU EA-628F33A CE-762 THRU CE-1791F33C CJ-141 THRU CJ-179V35B D-10091, D-10099, D-10101 THRU D-10403THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW SEAL FOR THE OPENABLE WINDOW.


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5 HRSMEN : 1 (MAN)

36-4015-1SEALS, UTILITY DOOR ATA :A36 E-1 THRU E-3217B36TC EA-242, EA-273 THRU EA-628THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEALS ON THE CABIN DOOR.




KIT CATALOG

36-4016-0001LANDING LIGHT ASSY IMPROVEMENT ATA :35-B33, 35-C33, E33, F33, G33 CD-626 THRU CD-130435-C33A, E33A, F33A CE-1 THRU CE-179136, A36 E-1 THRU E-3455A36TC, B36TC EA-1 THRU EA-696E33C, F33C CJ-1 THRU CJ-179N35, P35, S35, V35, V35TC, V35A, V35A-TC,V35B, V35B-TC

D-6562 THRU D-10403

THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE LANDING LIGHT ASSEMBLY TO INCREASELIGHT LIFE ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EC1300L" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY AUTHORIZED COMPANY OUTLET.


36-5006-1 SFUEL SELECTOR VALVE, STOP INSTALLATION ATA :36, A36 E-1 AND AFTERA36TC, B36TC EA-1 AND AFTERB33 THRU G33 CD-388 THRU CD-1304C33A THRU F33A CE-1 AND AFTERE33C, F33C CJ-1 AND AFTERP35 THRU V35B-TC D-6874 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR THE INSTALLATION OF A FUELSELECTOR VALVE STOP.

NOTENOTENOTENOTE:::: THIS KIT IS NOT APPLICABLE FOR AIRPLANES EQUIPPED WITH BRITAIN WING TIP TANKFUEL SYSTEM.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-5007-1 SOXYGEN FILLER TUBE INSTALLATION - SPARES ATA :A36, A36TC, B36TCTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A P/N 36-560013-5 OXYGENFILLER TUBE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-5009-3 PSTANDBY AIR PRESSUSYSTEM (COMM KIT ATA : 36WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

36-5010-1 SAIR CONDITIONER EXPANSION VALVE INSTALLATION ATA :A36 E-715, E-732 THRU E-2110 EXCEPT E-2104F33A CE-602 THRU CE-1036V35B D-9789, D-9806 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LARGER CAPACITY EXPANSION VALVE ONINSERVICE AIRCRAFT EQUIPPED WITH FACTORY INSTALLED OPTIONAL AIR CONDITIONING SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

36-5012-1 SFUEL FILLER NECK RESTRICTOR ATA :B36TC EA-242, EA-273 THRU EA-477SB NO. 2045, REV. 3, OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LIGHTNING RESISTANT FUEL CAPS ANDINSERTS. KIT CONSIST OF 2 CAPS AND INSERTS, 1TOOL, AND KIT DRAWING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5MEN : 1 (MAN)

36-5013-1 SFUEL FILLER NECK RESTRICTOR ATA :35 D-6746 THRU D-1040336, A36 E-1 THRU E-2216A36TC EA-1 THRU EA-272, EXCEPT EA-242B33 THRU G33 CD-388 THRU CD-1304C33A, F33A CE-1 THRU CE-1055E33C, F33C CJ-1 THRU CJ-155SB NO. 2045, REV. 3, QUANTITY AS REQUIRED FOR AIRCRAFT, OPTIONAL FUEL SYSTEMS. KIT CONSISTSOF 2 CAPS AND INSERTS, 1 TOOL AND KIT DRAWINGTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NON-LIGHTNING RESISTANT FUEL CAPS ANDINSERTS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.5MEN : 1 (MAN)

36-5014-1 PMANIFOLD INSTALLATION - STANDBY AIR PRESSURE ATA :SB NO. 2133 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO DIVERT STANDBY INSTRUMENT AIR FROM EXTRA AIR-DRIVEN GYROS (MORE THAN 2) AND FROM THE WEATHER SCOUT RADAR INSTALLATION (IF INSTALLED)WHEN 36-5009-1 OR -3 STANDBY INSTRUMENT AIR SYSTEM IS OPERATING.

NOTENOTENOTENOTE:::: THIS KIT IS TO BE INSTALLED IN CONJUNCTION WITH KITS 36-5009-1 OR -3, ONLY WHENTHE AIRCRAFT IS EQUIPPED WITH MORE THAN TWO AIR-DRIVEN GYROS OR WEATHERSCOUT RADAR.

WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

36-5015-1 PINFORMATION-STANDBY AIR PRESSURE SYSTEM INSTALLATION ATA :"OPTIONAL" SB NO. 2133 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO DIVERT STANDBY INSTRUMENT AIR FROM OPTIONALEQUIPMENT TO THE STANDARD EQUIPMENT WHEN KIT 36-5011-1 P AND 3 P STANDBY AIR PRESSURESYSTEM IS INSTALLED.

NOTENOTENOTENOTE:::: THIS KIT IS TO BE INSTALLED IN CONJUNCTION WITH KIT 36-5011-1 P OR -3 P, ONLYWHEN THE AIRCRAFT IS EQUIPPED WITH MORE THAN 2 ITEMS THAT REQUIRE AIRPRESSURE NORMALLY SUPPLIED BY THE ENGINE DRIVEN AIR PUMP.


36-5017-1 SFIRE EXTINGUISHER REPLACEMENT ATA :35B33, 35C33, 35C33A, E33, E33A, E33C,F33, F33A, F33C, S35, V35 (D7977 THRUD10403) V35B (SEE 36-5025-3 KIT).36, A36, A36TC, B36TC (SEE 36-5025-1 KIT).THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A 344T FIRE EXTINGUISHER ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

36-5019-1 PAIR CONDITIONER INSTALLATION ATA :A36 E-1946, E-2104, E-2111 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN AIR CONDITIONING SYSTEM.


WT. CHANGE : WT: 70 TO 80 LBSEST. MAN/HRS: : 246 TO 280MEN : 1 (MAN)

36-5022-1 SAIR CONDITIONER CONDENSER COIL REPLACEMENT - SPARES ATA :36, A36 E-1 THRU E-2835B36TC EA-242, EA-273 THRU EA-566.F33A CE-290 THRU CE-1751V35B D-9069 THRU D-10403THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE 102-384016-5 AIR CONDITIONINGCONDENSER FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AS REQUIRED MIL-A-1154B CEMENT P/N: "EC1403" WILL BE REQUIRED TO INSTALL, BUTNOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.



KIT CATALOG

36-5023-1 SELEVATOR TAB POSITION RETAINER ATA :58 TH-1389, TH-1396 AND AFTERA36 E-1946, E-2104, E-2111 AND AFTERB36TC EA-320, EA-389 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RETAIN THE ELEVATOR TABS AT THEPOSITION SELECTED ON AIRCRAFT NOT EQUIPPED WITH AN AUTOPILOT OR ELECTRIC TRIM TO IMPROVETRIM POSITION FOR TAKE-OFF ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

36-5024-1 SAILERON CONTROL PUSH ROD ATA :B36TC EA-371, EA-500THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION FOR INSTALLATION OF A PUSH ROD.

NOTENOTENOTENOTE:::: THIS KIT IS USED IN CONJUNCTION WITH 36-5015-1 P WHEN OPTIONAL EQUIPMENT ISINSTALLED (MORE THAN TWO GYROS).


36-5025-1FIRE EXTINGUISHER - SPARES ATA :36, A36, A36TC, B36TC EA-371, EA-500THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A ?352TS? FIRE EXTINGUISHER ON AIRCRAFTTHAT WERE PREVIOUSLY EQUIPPED WITH THE?FR-2 1/2? FIRE EXTINGUISHER (P/N GENERAL FIRE EXTINGUISHER CORP) OR MODEL ?2-10? FIREEXTINGUISHER (P/N: GRAVINER INC) OR

NOTENOTENOTENOTE:::: FOR OTHER LIGHT SINGLE AND TWIN PISTON AIRCRAFT SEE KIT: 36-5025-3.WT. CHANGE : WT: 5 LBS - WEIGHT OF FULL WEIGHT OF FIRE EXTINGUISHER BEING REPLACED;

ARM: 118; MOMENT: TBDEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

36-5027-1COVER ASSEMBLY, RH CONTROL WHEEL ATA :V35B, F33A, F33C, A36, A36TC, B36TCTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 36-530171-23 COVER ASSEMBLY ONINSERVICE AIRCRAFT THAT PREVIOUSLY HAD50-534846-11 PLATE INSTALLED ON THE RH CONTROL WHEEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

36-5040-0001G36/G58 MODEL NAME EMBLEM INSTL ATA :BONANZA G36 E-3630, E-3636 THRU E-3668, E-3671 &

E-3674THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A MODEL NAME EMBLEM FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "9372DK" FOAM ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. A PRODUCT OF 3MBONDING SYSTEMS IN ST. PAUL, MINN. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.


36-530168-1SPEAKER ATA : 23WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

36-8003- PBRAKE, COPILOT INSTALLATION ATA :36 THRU B36TCTHIS KIT PROVIDES THE CONVENIENCE OF COPILOT BRAKES BY ADDITION OF PEDALS, PLUMBING,MASTER CYLINDERS AND VALVES IN THE BRAKESYSTEM.WT. CHANGE : WT: + 4 LBS @ + 44 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

36-8005-1NOSE LANDING GEAR, SHAFT, ROLLER ASSEMBLY, RETRACTIONMECHANISM IMPROVEMENT

ATA :

A36 E-395, E-425 AND AFTERA36TC EA-1 THRU EA-272, EXCEPT EA-242B36TC EA-242, EA-273 AND AFTERF33A CE-418, CE-436 AND AFTERF33C CJ-40 AND AFTERV35B D-9439, D-9469 THRU D-10403"OPTIONAL" SB NO. 2601, JANUARY , 1995THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE THE SERVICE LIFE OF THE NOSE GEARRETRACT MECHANISM ON THE INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 5MEN : 1 (MAN)


KIT CATALOG

36-9003-1 PPROP DEICE ELECTROTHERMAL ATA :A36 E-1111, E-1241 THRU E-1931A36TC, B36TC EA-1 THRU EA-309F33A CE-748, CE-772 AND AFTERF33C CJ-149 AND AFTERV35B D-10097, D-10120 AND AFTERTHIS KIT PROVIDES THE PARTS AND NECESSARY INFORMATION TO INSTALL PROP DEICE BOOTS ON AMCCAULEY (2) BLADED PROPELLER ON AIRCRAFT EQUIPPED WITH A 100 AMP ALTERNATOR ORCONCURRENTLY WITH THE INSTALLATION OF KIT 36-3004-1 P, ALTERNATOR 100 AMP TCM.WT. CHANGE : N/AEST. MAN/HRS: : 26 TO 30MEN : 1 (MAN)

36-9003-3 PPROP DEICE, ELECTRIC, MCCAULEY PROPELLER (28-VOLT) ATA :A36 E-1111, E-1241 THRU E-1931A36TC EA-1 THRU EA-309F33A CE-748, CE-772 THRU CE-977F33C CJ-149 AND AFTERV35B D-10097, D-10120 THRU D-10303(AIRCRAFT MUST HAVE 100-AMP ALTERNATOR OR KIT 36-3004-1 P 100-AMP ALTERNATOR INSTALLEDPRIOR TO, OR AT TIME OF INSTALLATION)

THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROP DEICE CAPABILITY TO AIRCRAFT WITH AMCCAULEY THREE-BLADE PROPELLER.

NOTENOTENOTENOTE:::: FOR E-2111 AND AFTER SEE KIT 36-9012-1 P. FOR E-389 AND AFTER SEE KIT 36-9012-1 P.WT. CHANGE : 33, 35 WT: + 7.0 LBS @ + 22.0 ARM

36 WT: + 7.0 LBS @ + 12.0 ARMEST. MAN/HRS: : 24 TO 30MEN : 1 (MAN)

36-9004-1 PPROP DEICE, ELECTRIC, HARTZELL PROP (28-VOLT) ATA :A36 E-1111, E-1241 THRU E-1931A36TC, B36TC EA-1 THRU EA-309F33A CE-748, CE-772 THRU CE-977V35B D-10097, D-10120 THRU D-10382AIRCRAFT MUST HAVE 100-AMP ALTERNATOR OR KIT 36-3004-1 P 100-AMP ALTERNATOR INSTALLEDPRIOR TO, OR AT TIME OF INSTALLATION.

THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROP DEICE CAPABILITY TO MODELS WITH ATHREE-BLADE HARTZELL PROP INSTALLED.WT. CHANGE : 33, 35 WT: + 7.0 LBS @ 22.0 ARM; 154 MOMENT

36 = WT: + 7.0 LBS @ 12.0 ARM 84; MOMENTEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

36-9006-1 SOIL DRAIN INSTALLATION, TURBOCHARGER ATA :A36TC, B36TC EA-1 THRU EA-296SI NO. 1191 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED TURBOCHARGER OIL DRAINSYSTEM.WT. CHANGE : WT: - 3.5 LBS @ 15.2 ARM; -53 MOMENTEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-9007-1 SDRAIN VALVE INSTALLATION - SPARES ATA :B36TCSI NO. 1247 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT OF DRAIN VALVE ANDADAPTER PLATE ON THE F391-187-D DRAIN VALVE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-9011-1 SMAGNETO INSTALLATION PRESSURIZED ATA :A36TC, B36TC EA-159 THRU EA-439PENDING SB NO. 2613THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL SLICK PRESSURIZED MAGNETOSON TS10-520-U OR -UB ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : N/A

36-9011-3 SMAGNETO INSTALLATION PRESSURIZED ATA :A36TC EA-1 THRU EA-158SB NO. 2205 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL SLICK PRESSURIZED MAGNETOSON TS10-520-U OR -UB ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

36-9012-1 PPROP DE-ICE ELECTROTHERMAL ATA :A36 E-2104, E-2111 AND AFTERB36TC EA-389 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PROP DEICE BOOTS ON A MCCAULEY (3)BLADED PROPELLER ON AIRCRAFT EQUIPPED WITH A 100 AMP ALTERNATOR OR CONCURRENTLY WITHTHE INSTALLATION OF KIT 36-3004-1 P, 100 AMP ALTERNATOR OR CONCURRENTLY WITH THE INS

NOTENOTENOTENOTE:::: CURRENT A36 PILOTS OPERATING HANDBOOK E1946, E2104, E2111 AND AFTER P/N:36-590002-37 THRU REV: -37A7 COVERS MCCAULEY PROP DEICE OPERATIONS.

NOTENOTENOTENOTE:::: FOR EARLIER MODELS SEE KITS 36-9003-1 P, -3 P AND 36-9004-1 P.WT. CHANGE : WT: + 6 LBS ARM: N/A: MOMENT: + 120 IN.-LBSEST. MAN/HRS: : 24 TO 30MEN : 1 (MAN)

36-9012-3 PPROP DE-ICE ELECTROTHERMAL ATA :F33A CE-1024 AND AFTERBEECHCRAFT SERVICE LETTER 35 NO. 48, A35 NO. 30, B35 NO. 15, C35 NO. 15, D35 NO. 8 AND E35 NO. 9THIS KIT FURNISHES PARTS AND INFORMATION NECESSARY TO PROVIDE AN EXTRA MARGIN OF SAFETYBY INCREASING THE GEAR DOWN SPEED TO 160 MPH (IAS) BY MAKING MODIFICATIONS TO THE LANDINGGEAR DOOR ON INSERVICE AIRCRAFT.

THIS KIT PROVIDES THE PARTS AND INFORMATINOTENOTENOTENOTE:::: FOR EARLIER MODELS SEE KITS 36-9003-3 P AND 36-9004-1 P.

WT. CHANGE : WT: + 6 LBS; ARM: N/A; MOMENT: + 120 IN.-LBSEST. MAN/HRS: : 4MEN : 1 (MAN)

36-9013-1 SENGINE COOLING I0550 ENGINE ATA :A36 E-1946, E-2104, E-2111 THRU E-2760"OPTIONAL" SB NO. 2480THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE AND MODIFY ENGINE BAFFLES, MOVECYLINDER HEAD TEMPERATURE PROBE AND MAKE FUEL SYSTEM ADJUSTMENTS FOR IMPROVEDENGINE COOLING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

36-9014-1 SAIRCRAFT CONVERSION FROM A36AT TO A36 ATA :A36AT E-2712, E-2715THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO CONVERT A MODEL A36AT (MODEL A36MODIFIED FOR REDUCED EXTERNAL NOISE) INTO A STANDARD MODEL A36 WITH ENGINE COOLINGINSTALLATION.WT. CHANGE : WT: - 7 LBS; MOMENT: -57 IN.-LBSEST. MAN/HRS: : 20 - 24MEN : 1 (MAN)


KIT CATALOG

36-9015-1 SENGINE COOLING I0550 ENGINE ATA :A36 E-1946, E-2104, E-2111 THRU E-2760"OPTIONAL" SB NO. 2480, REV. ITHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE AND MODIFY ENGINE BAFFLES, MOVECYLINDER HEAD TEMPERATURE PROBE AND MAKE FUEL SYSTEM ADJUSTMENTS FOR IMPROVEDENGINE COOLING ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ANY CLEAR RTV SEALER AND "ALODINE 1200" CORROSION PROOFING WILL BEREQUIRED FOR USAGE WITH THIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOUCAN PROCURE LOCALLY.


55-3017-1 SOVERVOLTAGE RELAY INSTALLATION ATA :C33 (WITH 24-VOLT SYSTEM)THIS KIT REPLACES P/N 138-2 RELAY WITH P/N 100-364313-1 FOR SPARES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3019-1 SFUEL TRANSMITTER INSTALLATION ATA :33, 35, 36THIS KIT PROVIDES PARTS AND WIRING INFORMATION TO INSTALL OR PROVIDE AS SPARES P/N95-380012-13 TRANSMITTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3023-3 SFUEL QUANTITY CIRCUIT BOARD INSTALLATION ATA :A36 E-505 THRU E-1835A36TC EA-1 THRU EA-212F33A CE-480 THRU CE-946F33C CJ-52 THRU CJ-155V35B D-9569 THRU D-10369THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN IMPROVED FUEL QUANTITYPRINTED CIRCUIT BOARD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-3025-1 SPRINTED CIRCUIT BOARD INSTALLATION ATA :36, A36 E-124 THRU E-2049A36TC, B36TC EA-1 THRU EA-299, EA-301 THRU EA-323E33A, F33A CE-249 THRU CE-1029E33C, F33C CJ-14 THRU CJ-155V35A, V35A-TC, V35B, V35B-TC D-8883 THRU D-10403SB NO. 2016 OR SUBSEQUENTTHIS KIT PROVIDES IMPROVED CIRCUIT PROTECTION BY REPLACING THE ALTERNATOR AUXILIARYTERMINAL WIRE IN LINE FUSE WITH A PC BOARD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

55-3028-1 PCLOCK INSTALLATION, CONTROL WHEEL (14-VOLT) ATA :35-C33, 35-C33AA36E33, E33A, E33CF33, F33A, F33CG33V35, V35A, V35BVF35A-TC, V35B-TCTHIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-1, 50-534622-13, 50-534622-17,50-384210-1 OR 50-384211-1 8-DAY CLOCKS WHEN USED IN A 14-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

55-3028-3 PCLOCK INSTALLATION, CONTROL WHEEL (28-VOLT) ATA :A36, A36-TC, B36-TCF33A, F33CV35BTHIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-3, 50-534622-13, 50-534622-17,50-534622-21, 50-384209-1, 50-384210-1 OR 50-384211-1, 8-DAY CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)


KIT CATALOG

55-3029-1 PCLOCK INSTALLATION, INSTRUMENT PANEL - SPARES (14-VOLT) ATA :A36E33, E33AF33, F33A, F33CG33V35A, V35BTHIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 50-380013-5 AND 58-380015-1 8-DAY CLOCKS OR58-380077-1 AND 58-38007-5 ELECTRIC CLOCKS WHEN USED IN A 14-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

55-3029-3 PCLOCK INSTALLATION, INSTRUMENT PANEL - SPARES (28-VOLT) ATA :A36, A36-TC, B36-TCF33A, F33CV35BTHIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 50-380013-5 AND 58-380015-3 8-DAY CLOCKS OR58-380077-3 AND 58-380077-7 ELECTRIC CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

55-4016- PWINDSHIELD INSTALLATION - ONE PIECE ATA : 5633 THRU C33A CD-1 THRU CD-1118, CE-1 THRU CE-17935 THRU N35 D-1 THRU D-6841, IF KIT 35-393 IS

INSTALLED ON THE AIRCRAFTP35 THRU S35 D-6842 THRU D-7976THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A ONE PIECE WINDSHIELD. (SEE BROCHUREFIGURES 6 THROUGH 9).WT. CHANGE : WT: 4 LBS @ 68 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

55-5012-1 PSHOULDER HARNESS INSTALLATION (BEIGE) ATA : 2536, A36 E-1 THRU E-283F33 CD-1235 THRU CD-1256F33A CE-290 THRU CE-350V35 D-8599 THRU D-9287SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE BROCHURE FIGURES 10 AND 11)ADD THE COMFORT AND SAFETY OF SEAT BELTS AND HARNESSES INCLUDING INERTIA REELS FORBOTH PILOT AND COPILOT.WT. CHANGE : 33 AND 35 WT: + 4 LBS @ + 97 ARM; 388 MOMENT

36 WT: 4 LBS @ + 87 ARM; 348 MOMENTEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

55-5012-3 PSHOULDER HARNESS INSTALLATION (BLACK) ATA : 2536, A36 E-1 THRU E-28F33 CD-1235 THRU CD-1256F33A CE-290 THRU CE-350V35 D-8599 THRU D-9287SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE BROCHURE FIGURES 10 AND 11)ADD THE COMFORT AND SAFETY OF SEAT BELTS AND HARNESSES INCLUDING INERTIA REELS FORBOTH PILOT AND COPILOT.WT. CHANGE : 33 AND 35 WT: 4 LBS @ + 97 ARM; 388 MOMENT


55-5012-5 PSHOULDER HARNESS INSTALLATION (BLACK) ATA : 25C33, E33 CD-1028 THRU CD-1234C33A, E33A CE-27 THRU CE-289V35 D-7976 THRU D-8598SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE BROCHURE FIGURES 10 AND 11)ADD THE COMFORT AND SAFETY OF SEAT BELTS AND HARNESSES INCLUDING INERTIA REELS FORBOTH PILOT AND COPILOT.WT. CHANGE : 33 AND 35 WT: 4 LBS @ + 97 ARM; 388 MOMENT


55-5012-7 PSHOULDER HARNESS INSTALLATION (BEIGE) ATA : 25C33, E33 CD-1028 THRU CD-1234C33A, E33A CE-27 THRU CE-289V35 D-7976 THRU D-8598SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE BROCHURE FIGURES 10 AND 11)ADD THE COMFORT AND SAFETY OF SEAT BELTS AND HARNESSES INCLUDING INERTIA REELS FORBOTH PILOT AND COPILOT.WT. CHANGE : 33 AND 35 WT: 4 LBS @ + 97 ARM; 388 MOMENT



KIT CATALOG

55-9012-1 SINSTRUMENT AIR PUMP INSTALLATION (FOR AIRPLANES EQUIPPEDWITH 224CW OR 232CW PUMP)

ATA :

36, A36 E-1 THRU E-183, E-185 THRU E-196, E-198THRU E-202

C33A, E33A, F33A CE-135 THRU CE-235, CE-249, CE-250,CE-256, CE-260, CE-264 THRU CE-268,CE-270 THRU CE-297

E33, F33 CD-1119 THRU CD-1243E33C, F33C CJ-1 THRU CJ-27S35 THRU V35B-TC D-7920 THRU D-7925, D-7927, D-7929 THRU

D-7931, D-8381 THRU D-9060, D-9062 THRUD-9099, D-9101 THRU D-9104, D-9106 THRUD-9114

SI NO. 0933 OR SUBSEQUENTTHIS KIT PROVIDES A REPLACEMENT INSTRUMENT AIR PUMP.WT. CHANGE : 33 AND 35 WT: -2 LBS @ 41 INS. ARM; -82 IN.-LBS MOMENT

36 AND A36 WT: 2 LBS @ 31 INS. ARM; - 62 IN.-LBS MOMENTEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9018-1 SFUEL TRANSMITTER REPLACEMENT FOR INBOARD OR OUTBOARD, 39OR 40 GALLON CAPACITY FUEL CELLS, LH OR RH, WITH A.C. GAGES

ATA :

SI NO. 925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES REPLACEMENT OF FUEL QUANTITY TRANSMITTERS. THE ORIGINAL A.C. BRANDEQUIPMENT IS NO LONGER AVAILABLE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9018-3 SFUEL TRANSMITTER REPLACEMENT LH WITH A.C. GAGES ATA :SI NO. 925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES REPLACEMENT OF FUEL QUANTITY TRANSMITTERS. THE ORIGINAL A.C. BRANDEQUIPMENT IS NO LONGER AVAILABLE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-9018-4 SFUEL TRANSMITTER REPLACEMENT RH 25-GALLON CAPACITY WITHA.C. GAGES

ATA :

33 CD-626 THRU CD-123435 D-7080 THRU D-906936 E-1 THRU E-184 (WITH A.C. GAGES)C33A, E33A, F33A CE-1 AND AFTERSI NO. 925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES REPLACEMENT OF FUEL QUANTITY TRANSMITTERS. THE ORIGINAL A.C. BRANDEQUIPMENT IS NO LONGER AVAILABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-3003-1 SANTENNA REPLACEMENT B-6 ATA :A36, V356BF33A, F33C, G33THIS KIT PROVIDES A REPLACEMENT FOR THE B-6 (35-5006-1) ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-3010-1 SANTENNA, VHF, COMM INSTALLATION ATA :F33A, V35B, A36THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARE VHF COMM ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-4003-1 SSEAT TIE DOWN, AFT ATA :36, A36S35 THRU V35 D-7310 THRU D-9537THIS KIT PROVIDES PARTS AND INFORMATION TO ADD A REVISED TIE DOWN FOR THE AFT (5TH AND 6TH)SEATS. USED IN CONJUNCTION WITH KIT 58-5009-5 P, -9 P AND -11 P.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-4011-3LOCK ASSEMBLY INSTALLATION, NOSE BAGGAGE DOOR, CABIN DOOR,UTILITY DOOR

ATA : 52

A36 E-609 THRU E2727 EXCEPT E-2711A36 E-2711, E-2728 THRU E-3217A36TC EA-1 THRU EA-272, EXCEPT EA-242B36TC ES-537 THRU EA-628B36TC EA-273 THRU EA-536 IF KIT 36-4007-1 HAS

BEEN INSTALLED"OPTIONAL" SB NO. 52-3324THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED DOOR LOCK ASSEMBLIES FOR THECABIN DOOR AND THE UTILITY DOOR FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AF3306-2 SCRIM CLOTH, ALODINDE 1200S ALODINE, EA9309 ADHESIVE REQUIRED BUTNOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


58-5005-1 PSHOULDER HARNESS INSTALLATION (BEIGE) ATA :A36 E-284 THRU E-312F33A CE-351 THRU CE-357G33 CD-1257 THRU CD-1268V35B D-9308 THRU D-9861SI NO. 1020 AND SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESS, COMPLETE WITHINERTIA REELS, FOR THE PILOT AND COPILOT SEATS.

NOTENOTENOTENOTE:::: THIS KIT CAN BE USED ON LATER MODELS, BUT THEY SHOULD OF HAD FACTORYINSTALLATION ON AIRCRAFT.

WT. CHANGE : WT: + 4 LBS @ 97 ARMEST. MAN/HRS: : 24MEN : 1 (MAN)

58-5005-3 PSHOULDER HARNESS INSTALLATION (BEIGE) ATA :A36 E-284 THRU E-312F33A CE-351 THRU CE-357G33 CD-1257 THRU CD-1268V35B D-9288 THRU D-9307SI NO. 1020 AND SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE COMFORT AND SAFETY OF SEAT BELTS AND SHOULDER HARNESSES COMPLETE WITH INERTIAREELS, FOR BOTH PILOT AND COPILOT.WT. CHANGE : WT: + 4 LBS @ + 97 ARMEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

58-5009-1 PSHOULDER HARNESS INSTALLATION (3RD AND 4TH SEATS) ATA :33 CD-1 THRU CD-130435 D-1 THRU D-9861C33A CE-1 THRU CE-633E33C,F33C CJ-1 THRU CJ-128SI NO. 1020 AND SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE SAFETY AND CONVENIENCE OF SHOULDER HARNESSES TO PASSENGER SEATS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5009-11 PSHOULDER HARNESS INSTALLATION (5TH SEAT ONLY) ATA :36, A36 E-1 THRU E-824SI NO. 1020 AND SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE SAFETY AND CONVENIENCE OF SHOULDER HARNESSES TO PASSENGER SEATS.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)

58-5009-3 PSHOULDER HARNESS INSTALLATION (3RD AND 4TH SEATS) ATA :36, A36 E-1 THRU E-824SI NO. 1020 AND SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE SAFETY AND CONVENIENCE OF SHOULDER HARNESSES TO PASSENGER SEATS.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)

58-5009-5 PSHOULDER HARNESS INSTALLATION (5TH SEAT ONLY) ATA : 25SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE SAFETY AND CONVENIENCE OF SHOULDER HARNESSES TO PASSENGER SEATS.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)

58-5009-7 PSHOULDER HARNESS INSTALLATION (6TH SEAT ONLY) ATA : 25F33A CE-316 AND AFTERS35 D-7140, D-7310 THRU D-9861SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE SAFETY AND CONVENIENCE OF SHOULDER HARNESSES TO PASSENGER SEATS.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

58-5009-9 PSHOULDER HARNESS INSTALLATION (6TH SEAT ONLY) ATA : 25SB NO. 2031, REV. 2 OR SUBSEQUENTADD THE SAFETY AND CONVENIENCE OF SHOULDER HARNESSES TO PASSENGER SEATS.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)

58-8001-1 SLANDING GEAR SWITCH GUARD INSTALLATION ATA :35 D-6842 THRU D-1039636, A36 E-1 THRU E-2033A36TC EA-1 THRU EA-272B33 THRU G33 CD-388 THRU CD-1304C33A THRU F33A CE-1 THRU CE-999E33C, F33C CJ-1 THRU CJ-155SI NO. 1215 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A LANDING GEAR SWITCHGUARD. THIS KIT IS NOT APPLICABLE FOR AIRPLANES EQUIPPED WITH OPTIONAL LANDING GEARSAFETY SYSTEM INSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

90-3085-1 SBRUSH BLOCK ASSEMBLY, MODULAR ATA :33, 35, 36SI NO. 1075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT FOR 4E1387-3, -5 AND -6BRUSH BLOCK ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

90-4111-1 SWING ATTACH FITTING ATA :50 THRU J50THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER FORWARD LH WING 50-120073-7ATTACH FITTING, CENTER FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

90-4111-2 SWING ATTACH FITTING ATA :50 THRU J50THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER FORWARD RH WING 50-120073-8ATTACH FITTING, CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 2 (MEN)

95-8100-0001ACTUATOR ASSY, SEAL REPLACEMENT ATA :33, 35 &THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE SEALANT OR GASKETS WITH NEW GASKETSIN THE 95-810017 LANDING GEAR ACTUATOR (ALL DASH NUMBERS), TO REDUCE LEAKSWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberMARKER BEACON ANTENNA INSTALLATION - (100-3016-3 S) 1

EXTERIOR PLACARD, "BEECHCRAFT" - (101-2003-1 S) 1


SWITCH GUARD INSTALLATION, E.L.T. - (101-3062-1 S) 1







BRAKE SHUTTLE VALVE, DUAL BRAKES - SPARES - (101-8008-1 S) 3

WING ICE LIGHT INSTALLATION - (102-3003-1 P) 3

FILTER INSTALLATION NOISE SUPPRESSION EMI, FUEL BOOST PUMP - (102-3006-1 S) 4

WINDSHIELD HEATED - (102-3010-1 S) 4

DOOR SEAL, INSTALLATION - SPARES - (102-4007-1 S) 4

WINDOW, MID-CABIN, TINTED AMBER - SPARES - (102-4008-1 S) 5

WINDOW, MID-CABIN, (RH) TINTED AMBER - SPARES - (102-4008-2 S) 5

WINDOW, MID-CABIN, BRONZE TINTED - SPARES - (102-4008-3 S) 5

WINDOW, MID-CABIN, BRONZE TINTED - SPARES - (102-4008-4 S) 5




DEICE MODIFICATION, WINDSHIELD - (102-5004-1 S) 6

DEICE MODIFICATION, STALL WARNING DETECTOR - (102-5004-11 S) 7

WINDSHIELD HEATED - (102-5004-5 S) 7

ANTI-ICING/DEICING MODIFICATION INSTL - (102-5004-9) 7

ICING-FLIGHT REQUIREMENTS - (102-5006- P) 7

SURFACE DEICE INSTALLATION - (102-5007-1 P) 7

BRACKET INSTALLATION, 5TH AND 6TH SEATS - (102-5014-1 S) 8

CLAMP ASSEM,TRUSSTUBE - (102-9001-1 S) 8

SYNCHROPHASER INSTALLATION, ENGINE - (102-9004-1 S) 8

EXHAUST PIPE SHIELD ASSEMBLY - SPARES - (102-9007-1 S) 8

EXHAUST CLAMP INSTALLATION - (102-9008-1 S) 8

SYNCHROPHASER CONTROL BOX, TYPE II - (102-9009-1 S) 9

ENGINE AIR OIL SEPARATOR INSTALLATION - (102-9010-1 S) 9

PRESSURIZED MAGNETO INSTALLATION - (102-9012-1 S) 9

DOOR, BAGGAGE SECONDARY LATCH INSTALLATION - (33-4001-1 S) 10



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFUEL RESERVOIR FOAM INSTALLATION - (33-4005-1 S) 10

FUEL RESERVOIR FOAM INSERT INSTALLATION - (33-4005-2 S) 10



TELESCOPING TUBE, WING HINGE PIN TOOL - (35-0588-1) 11

LANDING GEAR DRAG LEG, NOSE GEAR COMMONALITY - SPARES - (35-4012-1 S) 11

WINDOW 3RD TEAR DROP (TINTED) - (35-4014-3 S) 12

FUEL FILLER NECK RESTRICTORS, NON-INDEXING - (35-5048-1 S) 12

DOOR HANDLE, INSIDE CABIN REPLACEMENT - SPARES - (35-5050-1 P) 12

WHEEL BEARING GREASE SEAL - SPARES - (35-8008-1 S) 13







FUEL CELL ATTACHMENT FASTENER - (35-9009-5 S) 15

FUEL FLOW TRANSDUCER - (35-9018-3 S) 15

WARNING HORN, FULL FLAP - (36-3012-1 S) 15

LANDING GEAR WARNING LIGHT - (36-3013-1 S) 16

LANDING GEAR RETRACT PREVENTION RELAY INSTALLATION LOW THROTTLE - (36-3014-3 S) 16

TACHOMETER INDICATOR - SPARES - (36-3018-3 S) 16

DOOR - CABIN CENTER 3RD LATCH POINT - (36-4007-1 S) 16


BLOWER, FRESH AIR REPLACEMENT - SPARES - (36-4009-1 S) 17

CABIN DOOR SEAL - (36-4013-1) 17

OPENABLE WINDOW SEAL - (36-4014-1) 18

SEALS, UTILITY DOOR - (36-4015-1) 18



FIRE EXTINGUISHER REPLACEMENT REPLACEMENT KITS LISTED BELOW ONLY FOR REFERENCE MODELS.SPARES SEE KIT CATALOG FOR AIRCRAFT MODELS AND SERIAL NUMBERS EXCEPT FOR AIRCRAFT LISTED.- (36-5017-1 S)

19

FIRE EXTINGUISHER (*RESTRICTED ARTICLE* IS FIRE BOTTLE) - SPARES - (36-5025-1) 19


G36/G58 MODEL NAME EMBLEM INSTL - (36-5040-0003) 20

ROLLER ASSEMBLY, RETRACTION MECHANISM, NOSE LANDING GEAR SHAFT - (36-8005-3) 20




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberINTERIOR PLACARD - (55-2002-1 S) 21



OVERVOLTAGE RELAY REPLACEMENT - (55-3017-1 S) 21

FUEL TRANSMITTER - SPARES - (55-3019-1 S) 22

FUEL QUANTITY INDICATING SYSTEM - (55-3021-1 S) 22

FUEL QUANTITY SYSTEM - (55-3021-2 S) 22

LIGHT INSTALLATION, STARTER ENERGIZED - (55-3022-1 S) 22

FUEL QUANTITY PRINTED CIRCUIT BOARD, IMPROVED - (55-3023-1 S) 23

DUAL VOLTAGE REGULATOR INSTL - (55-3024-1) 23

KIT-S-DUAL VT REG - (55-3024-1 S) 23

PRINTED CIRCUIT BOARD INSTALLATION - (55-3025-3 S) 23

ALTERNATOR FIELD FUSE INSTALLATION - (55-3026-1 S) 23

CLOCK INSTALLATION CONTROL WHEEL (28-VOLT) - (55-3028-3 P) 24


FLASHER INSTALLATION - (55-3030-1 S) 24

MODERNIZATION-GROS WT 5100#-MODEL 95 - (55-4014- P) 24

WINDSHIELD INSTALLATION - ONE PIECE - (55-4016- P) 24

ELEVATOR TRIM TAB ACTUATOR LINKAGE, IMPROVED - (55-4020-1 S) 25

RUDDER PEDAL BELL CRANK BRACKET REPLACEMENT, IMPROVED - (55-4029-1 S) 25

RUDDER PEDAL BELL CRANK BRACKET REPLACEMENT, IMPROVED - (55-4029-3 S) 25

FUSELAGE BULKHEAD REINFORCEMENT, STABILIZER ATTACHMENT - (55-4030-1 S) 26



NOSE BAGGAGE DOOR SECONDARY LATCH - (55-4031-1 S) 26

AIR CONDITIONER RECEIVER DRYER INSTALLATION - (55-4034-1 S) 27

AIR CONDITIONER RECEIVER DRYER INSTALLATION - (55-4034-3 S) 27

SHOULDER HARNESS INSTALLATION (BEIGE ONLY) - (55-5012-1 P) 27

SHOULDER HARNESS INSTALLATION (BLACK ONLY) - (55-5012-3 P) 27

SHOULDER HARNESS INSTALLATION (BLACK ONLY) - (55-5012-5 P) 28

SHOULDER HARNESS INSTALLATION (BEIGE ONLY) - (55-5012-7 P) 28

HEATER PRESSURE DIFFERENTIAL SWITCH RELOCATION - (55-5014-1 S) 28

WHEEL AND BRAKE INSTALLATION (SINGLE CONTROL ONLY) - (55-8002- P) 28

WHEEL AND BRAKE INSTALLATION (SINGLE CONTROL ONLY) - (55-8002-3 P) 29

BRAKE INSTALLATION, DUAL CONTROL - (55-8005- P) 29

FUEL BOOST PUMP INSTALLATION (1/2 INCH FUEL LINE) - (55-9011-1 S) 29

FUEL BOOST PUMP INSTALLATION ( 3/8 INCH FUEL LINE) - (55-9011-3 S) 29



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCOWL FLAP, MANUAL INSTALLATION - (55-9013-1 S) 30

COWL FLAP, MANUAL INSTALLATION - (55-9013-3 S) 30

FUEL TRANSMITTER INSTALLATION, AC GAGE - (55-9018-1 S) 30




FUEL TRANSMITTER INSTALLATION, AC GAGE - (55-9018-6) 31

RH FUEL TRANS W/EX GAGE 31GAL AUX - (55-9018-6 S) 31

FUEL TRANSMITTER INSTALLATION, ROCHESTER GAGE - (55-9019-1 S) 32





COWL FLAP ACTUATOR - SPARES - (55-9020-1 S) 33

FUEL BOOST PUMP - SPARES - (55-9021-1 S) 33

PROPELLER DEICE, 2-BLADE HARTZELL - (55-9022-1 P) 34




PROPELLER DEICE, 3-BLADE MCCAULEY - (55-9023-1 P) 35



FUEL VENT, FLUSH - (55-9024-1 S) 35

ENGINE MOUNT - SPARES - (55-9025-1 S) 35



ANTENNA, B-6 - SPARES - (58-3003-1 S) 36

TAXI LIGHT INSTALLATION, NOSE GEAR - (58-3004-1 P) 36

TAXI LIGHT INSTALLATION, NOSE GEAR - (58-3004-3 P) 37

ALTERNATOR INSTALLATION, 100-AMPERE - (58-3005-1 P) 37




ALTERNATOR INSTALLATION, 100-AMPERE - (58-3007-3) 38

STALL WARNING LIFT DETECTOR, HEATED - (58-3009-1 P) 38

ANTENNA, VHF COMM - (58-3010-1 S) 38

TURN AND SLIP INDICATOR - SPARES - (58-3011-1 S) 39



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberHEATED WINDSHIELD INSTALLATION - SPARES - (58-3012-1 S) 39

WINDSHIELD, HEATED PATCH SEALING - (58-3013-1 S) 39

KIT-GARMIN 530/SHADIN 200+/MD41-1469INFO - (58-3014-1) 39

KIT -GLIDESLOPE ANTENNACHANGE-INFO ONLY - (58-3016-1) 39

AIR CONDITIONING TIME DELAY RELAY - (58-3018-0001) 40

SPAR INSTALLATION, OUTBOARD WING FORWARD - (58-4002-1 S) 40

SEATING STRUCTURE TIE-DOWN, AFT - (58-4003-1 S) 40

DEICE SYSTEM, OUTBOARD WING, PNEUMATIC - (58-4007-1 P) 41




DEICE SYSTEM, INBOARD WING, PNEUMATIC - (58-4007-9 P) 42

SPAR FRONT CARRY-THRU REINFORCEMENT - (58-4008-1 S) 42

FRONT SPAR CARRY-THRU STRUCTURE REINFORCEMENT - (58-4008-11 S) 43

FRONT SPAR CARRY-THRU REINFORCEMENT - (58-4008-3 S) 43




LOCK ASSY INSTL, NOSE BAGGAGE DOOR - (58-4011-1) 44

HEATED WINDSHIELD INSTL - (58-4013-0001) 45

DOORS - PROVISIONS FOR FLIGHT WITH UTILITY DOORS REMOVED - (58-5002- S) 45

BEIGE HARNESSES FOR PILOT & CO-PILOT - (58-5005-1 P) 45

SHOULDER HARNESS INSTALLATION (BEIGE ONLY) SEE PAGE 3-43 AND 3-44 - (58-5005-3 P) 46

STATIC AIR VALVE, ALTERNATE - (58-5006-1 S) 46

HARNESS RESTRAINT, SHOULDER - (58-5009-1 P) 46






GROSS WEIGHT MODIFICATION - (58-5010-1 S) 48

OXYGEN REGULATOR AND BOTTLE - SPARES - (58-5011-3 S) 48

ICING FLIGHT REQUIREMENT LIST - (58-5012-1 P) 49







Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberICING FLIGHT APPROVAL PLACARD INSTALLATION - (58-5013-1 P) 50

ICING FLIGHT APPROVAL PLACARD INSTALLATION - (58-5013-3 P) 50

FIRESLEEVE INSTALLATION - INSTRUMENT AIR - (58-5014-1 S) 50

FIRESLEEVE INSTALLATION - INSTRUMENT AIR - (58-5014-7 S) 50

ENGINE CONTROLS SUPPORT ANGLE BRACKETS - (58-5016-1 S) 51

KIT"M"SPEC INTERIOR - (58-5019-1) 51

LANDING GEAR SWITCH GUARD - (58-8001-3 S) 51

TORQUE KNEE COMPONENTS, (MAIN LANDING GEAR) - (58-8003-1 S) 51

TORQUE KNEE COMPONENTS, (NOSE LANDING GEAR) - (58-8003-3 S) 52




EXHAUST CLAMP - SPARES - (58-9005-1 S) 53

FUEL PUMP REFERENCE LINE CHANGE - (58-9006-1 S) 53

ENGINE MOUNT REINFORCEMENT - (58-9007-1 S) 53

ENGINE MOUNT ASSEMBLY - (58-9008-1 S) 53

HOOK INSTL, ENGINE CONTROL CABLE - (58-9010-0001) 53

EXTENDED RANGE FUEL TANK IMPROVEMENT - (58-9011-0001) 54

FUEL CELL, LH BAFFLED - SPARES - (60-9002-1 S) 54

FUEL CELL, RH BAFFLED - SPARES - (60-9002-2 S) 54

FUEL BOOST PUMP, REPLACEMENT - (60-9005-1 S) 55




IGNITION VIBRATOR - SPARES - (90-3093-1 S) 56

IGNITION UNIT - SPARES - (90-3093-3 S) 56

OUTFLOW AND SAFETY VALVE GASKET - SPARES - (90-5058-1 S) 56

FUEL CELL, 13-GALLON LEADING EDGE - (90-9056-3 S) 56

FUEL CELL, 13-GALLON LEADING EDGE - (90-9056-4 S) 57



BATTERY - SPARES - (95-3001-1 S) 57

FLAP RUBBER BUMPER, ADDITION - (95-4001- S) 58

HARNESS INSTALLATION, SHOULDER - (95-5002-1 P) 58

HARNESS INSTALLATION, SHOULDER - (95-5002-5 P) 58

ACTUATOR ASSY, SEAL REPLACEMENT - (95-8100-0001) 58

ANNUNCIATOR LIGHT, FUEL TANK SELECTOR - (95-9002-1 S) 58



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberANNUNCIATOR LIGHT, FUEL TANK SELECTOR - (95-9002-3 S) 59

ANNUNCIATOR LIGHT AUXILIARY FUEL TANK SELECTOR - (96-9001-1 S) 59


KIT CATALOG

100-3016-3 SMARKER BEACON ANTENNA INSTALLATION ATA :B55, E55, 58, 58TCTHIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL REPLACEMENT LH MARKER BEACON.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

101-2003-1 SEXTERIOR PLACARD, "BEECHCRAFT" ATA :58 TH-1505 AND AFTER58P TJ-498 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE101-531347-1 PLACARD. PAINT IS NOT INCLUDED IN THE KIT. PURCHASE |P`BEECHCRAFT RED|P` PARTNUMBER 2351.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3039-1 SEMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH ATA :58 TH-188, TH-190 THRU TH-113258P TJ-3 THRU TJ-27158TC TK-1 THRU TK-121B55 TC-1418 THRU TC-2320E55 TE-850 THRU TE-1177THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REMOTE SWITCH FOR THE TR70-13 E.L.T.(E.L.T. AND BATTERY PACK ARE NOT INCLUDED).WT. CHANGE : N/AEST. MAN/HRS: : 2.5MEN : 1 (MAN)

101-3062-1 SSWITCH GUARD INSTALLATION, E.L.T. ATA :58 TH-188, TH-190 THRU TH-113258P TJ-3 THRU TJ-27158TC TK-1 THRU TK-121B55 TC-1418 THRU TC-2320E55 TE-850 THRU TE-1177THIS KIT PROVIDES A SWITCH GUARD FOR AIRPLANES EQUIPPED WITH A TR70-13 E.L.T. AND REMOTESWITCH KIT 101-3039-1 S INSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-3066-3 PTIME INDICATOR INSTALLATION ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-245656TC, A56TC TG-2 THRU TG-9458 TH-1 AND AFTER58P TJ-3 AND AFTER58TC TK-1 THRU TK-15195, B95, D95A, E95 TD-2 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELAPSED TIME INDICATOR FOR ALL 28-VDC ELECTRICAL EQUIPMENT REQUIRING AN INSPECTION AT INTERVALS UP TO 2,000 HOURS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3066-5 PTIME INDICATOR INSTALLATION ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-245656TC, A56TC TG-2 THRU TG-9458 TH-1 AND AFTER58P TJ-3 AND AFTER58TC TK-1 THRU TK-15195, B95, D95A, E95 TD-2 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELAPSED TIME INDICATOR FOR ALL 28-VDC ELECTRIC EQUIPMENT REQUIRING AN INSPECTION AT INTERVALS UP TO 10,000 HOURS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3170-1 SANTENNA MARKER BEACON INSTALLATION ATA :95B95, E55, 58, 58TC, 58PTHIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION FOR SPARES REPLACEMENT OF100-384120 MARKER BEACON ANTENNA WITH A 101-384179 MARKER BEACON ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10 TO 12MEN : 1 (MAN)

101-3227-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN VHS FORMAT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG



101-8008-1 SBRAKE SHUTTLE VALVE, DUAL BRAKES - SPARES ATA :55, A55 ,B55 TC-1 THRU TC-349, TC-351 THRU TC-212056TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-90258P TJ-3 THRU TJ-14258TC TK-1 THRU TK-6795, D95, D95A, E95 TD-2 THRU TD-721C55, D55 AND E55 TC-350, TE-1 THRU TE-1124SI NO. 1056 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED BRAKE SHUTTLE VALVES AS ASPARES REPLACEMENT.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

102-3003-1 PWING ICE LIGHT INSTALLATION ATA :58 TH-1 AND AFTER58P TJ-3 AND AFTER58TC TK-1 THRU TK-151D55, E55 TE-452 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WING ICE LIGHT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

102-3006-1 SFILTER INSTALLATION NOISE SUPPRESSION EMI, FUEL BOOST PUMP ATA :56TC,A56TC TG-1 THRU TG-9458P TJ-2 THRU TJ-22458TC TK-1 THRU TK-102THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN IMPROVED EMI FILTER ATFUEL BOOST PUMP FOR REDUCTION OF RADIO NOISE ON INSERVICE AIRCRAFT WITH A 60-361016-1FILTER PER INSTALLATION OF 60-9005-1 S KIT.

NOTENOTENOTENOTE:::: *AIRCRAFT SERIAL NUMBER: P-1 THRU P-281 AND TG-1 THRU TG-94 WITH 60-9005-1S KITINSTALLED.


102-3010-1 SWINDSHIELD HEATED ATA :58P TJ-48, TJ-57 THRU TJ-497THIS KIT HAS A TINTED HEATED WINDSHIELD. THIS KIT PROVIDES PARTS AND INFORMATION TOREPLACE 102-364044-55 HEATER WINDSHIELD ASSEMBLY OR 102-384017-1 HEATER ASSEMBLY OR MAYBE USED TO INSTALL 102-364044-85 HEATED WINDSHIELD ASSEMBLY ON AIRCRAFT WHICH PREVI

NOTENOTENOTENOTE:::: FOR TJ AND TK AIRCRAFT WITHOUT ONE AND DESIRING TO INSTALL A HEATEDWINDSHIELD SEE 102-3008-1, -3 OR -5 S KITS AND FOR OTHER BARONS SEE 58-3012-1 S.

NOTENOTENOTENOTE:::: WINDSHIELD SEALING COMPONENTS ARE PART OF THIS KIT, BUT YOU WILL HAVE TOORDER SEALANTS PART NUMBER PR1221B1/2 QT AND PR1425B2 AND ADHESIVE PARTNUMBER XMH8680 SEPARATELY. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


102-4007-1 SDOOR SEAL, INSTALLATION - SPARES ATA :58P TJ-2 THRU TJ-220THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN IMPROVED INFLATABLEDOOR SEAL FOR THE RH FORWARD CABIN DOOR ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: WILL REQUIRE "MEK" CLEANER AND "RTV732" CLEAR SEALANT TO MAKE THIS KITINSTALLATION. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

102-4008-1 SWINDOW, MID-CABIN, TINTED AMBER - SPARES ATA :58P TJ-48, TJ-57 THRU TJ-386THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE LH MID-CABIN SIDE WINDOW.

THIS KIT CONSIST OF AN UNDRILLED WINDOW ASSEMBLY LH, 3 DRILL JIGS, STRAP, SPACER, HILOKS,WASHERS AND KIT DRAWING. NO SEALER IS PROVIDED WITH THE KI

NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED, PROSEAL PART NUMBER: "890B4" OR "PR1440B-4" OR "MC236B4 QT" CEMENT. PER PROCESS LAB, PR142B2 IS SUITABLE ALTERNATEFOR 890B4 FOR THIS TYPE INSTALLATION.

WT. CHANGE : N/AEST. MAN/HRS: : 24 TO 30MEN : N/A

102-4008-2 SWINDOW, MID-CABIN, (RH) TINTED AMBER - SPARES ATA :58P TJ-48, TJ-57 THRU TJ-386THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE RH MID-CABIN SIDE WINDOW.

NOTENOTENOTENOTE:::: KIT SAME AS -1 S KIT EXCEPT, UNDRILLED WINDOW ASSEMBLY IS (RH).NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED, PROSEAL PART NUMBER: "890B4" OR "PR1440

B-4" OR "MC236B4 QT" CEMENT, PER PROCESS LAB, "PR1425B2" CEMENT CAN BE USEDAS ALTERNATE FOR THIS TYPE INSTALLATION. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


102-4008-3 SWINDOW, MID-CABIN, BRONZE TINTED - SPARES ATA :58P TJ-3 THRU TJ-47,TJ-49 THRU TJ-56THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BRONZE TINTED SPARES REPLACEMENTFOR THE LH MID CABIN SIDE WINDOW.

NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED, PROSEAL PART NUMBER:"890B4" OR "PR1440B-4" OR "MC236B4 QT" CEMENT. PER PROCESS LAB, "PR1425B2" SEALER IS SUITABLEALTERNATE FOR "890B4" PROSEAL FOR THIS TYPE OF INSTALLATION.


102-4008-4 SWINDOW, MID-CABIN, BRONZE TINTED - SPARES ATA :58P TJ-3 THRU TJ-47,TJ-49 THRU TJ-56THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES BRONZE TINTED REPLACEMENTWINDOW FOR THE RH MID-CABIN SIDE WINDOW.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, PROSEAL PART NUMBER: "890B4" OR"PR1440B4 OR "MC236B4 QT" CEMENT. PER PROCESS LAB, "PR1425B2" IS SUITABLEALTERNATE FOR "890B4" PROSEAL FOR THIS TYPE OF INSTALLATION.



KIT CATALOG

102-4009-1FIFTH SEAT ATTACHMENT ATA : 5358P TJ-3 THRU TJ-497SB NO. 53-3159 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHAND SIXTH SEATS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SCRIM CLOTH AND EA9309NA ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


102-4009-3FIFTH AND SIXTH SEAT ATTACHMENT ATA : 5358P TJ-3 THRU TJ-497SB NO. 53-3159 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHSEAT ON INSERVICE AIRCRAFT.



102-4009-5SIXTH SEAT ATTACHMENT ATA : 5358P TJ-3 THRU TJ-497SB NO. 53-3159 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEAT ATTACHMENTS FOR THE FIFTHSEAT ON INSERVICE AIRCRAFT.



102-5004-1 SDEICE MODIFICATION, WINDSHIELD ATA :58P TJ-1 THRU TJ-47, TJ-49 THRU TJ-56THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATED WINDSHIELD. (KIT INCLUDESWINDSHIELD).WT. CHANGE : WT: 2.1 LBS @ 37.1 ARMEST. MAN/HRS: : 48MEN : 1 (MAN)


KIT CATALOG

102-5004-11 SDEICE MODIFICATION, STALL WARNING DETECTOR ATA :58P TJ-3 AND AFTER58TC TK-1 THRU TK-151THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATED STALL WARNING DETECTOR.WT. CHANGE : WT: 0.8 LBS @ 58.8 ARMEST. MAN/HRS: : 6MEN : 1 (MAN)

102-5004-5 SWINDSHIELD HEATED ATA :58 TH-1 AND AFTER58TC TK-1 THRU TK-151D55, E55 TE-452 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATED WINDSHIELD. (KIT INCLUDESWINDSHIELD)

NOTENOTENOTENOTE:::: LAYOUT 102-050000 DELETES REQUIREMENT FOR 102-364044-41 COVER IN KIT.NOTENOTENOTENOTE:::: AIRCRAFT MUST HAVE INSTALLED 100 AMP ALTERNATORS TO USE THIS KIT, AS THERE

IS NO BEECH KIT TO INSTALL THE 100 AMP ALTERNATOR ON ANY 58TC AND SOME OFTHE OTHER MODELS SERIAL NUMBERS.

WT. CHANGE : WT: 1.8 LBS @ 37.8 ARMEST. MAN/HRS: : 48MEN : 1 (MAN)

102-5004-9ANTI-ICING/DEICING MODIFICATION INSTL ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

102-5006- PICING-FLIGHT REQUIREMENTS ATA : 3058P, 58PA, 58TC, 58TCATHIS DRAWING PROVIDES A LIST OF ITEMS REQUIRED FOR INSTALLATION TO APPROVE FLIGHT IN ICINGCONDITIONS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

102-5007-1 PSURFACE DEICE INSTALLATION ATA :58P TJ-3 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SURFACE DEICE SYSTEM. (THIS KIT DOESNOT INCLUDE BOOTS.)

NOTENOTENOTENOTE:::: KIT 102-5004-11 S MUST BE INSTALLED IN CONJUNCTION WITH THIS KIT.WT. CHANGE : WT: 22.8 LBS @ 139 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

102-5014-1 SBRACKET INSTALLATION, 5TH AND 6TH SEATS ATA :58P TJ-1 THRU TJ-435, TJ-437 THRU TJ-443SB NO. 2022 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED 5TH AND 6TH SEAT ATTACHBRACKETS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

102-9001-1 SCLAMP ASSEM,TRUSSTUBE ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

102-9004-1 SSYNCHROPHASER INSTALLATION, ENGINE ATA :58P TJ-1 THRU TJ-31658TC TK-1 THRU TK-133THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE SYNCHROPHASER ON AIRPLANESEQUIPPED WITH A PROPELLER SYNCHRONIZER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

102-9007-1 SEXHAUST PIPE SHIELD ASSEMBLY - SPARES ATA :58P TJ-3 THRU TJ-34258TC TK-1 THRU TK-135THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE102-910048-11 SHIELD ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

102-9008-1 SEXHAUST CLAMP INSTALLATION ATA :58P TJ-3 THRU TJ-40958TC TK-1 THRU TK-149SI NO. 1206 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED COUPLING AND ADD ASECONDARY RETAINING CLAMP AND BRACKET ON THE EXHAUST PIPE.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

102-9009-1 SSYNCHROPHASER CONTROL BOX, TYPE II ATA :

58P TJ-134 THRU TJ-49158TC TK-134 THRU TK-151"OPTIONAL" SB NO. 2115S I# 32-90-8931THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED TYPE II SYNCHROPHASERCONTROL BOX ON AIRPLANES WHICH HAVE A TYPE II SYNCHROPHASER SYSTEM CURRENTLYINSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

102-9010-1 SENGINE AIR OIL SEPARATOR INSTALLATION ATA :58P TJ-3 THRU TJ-49758TC TK-1 THRU TK-151SB NO. 2099 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ENGINE AIR OIL SEPARATORS TO REDUCETHE POSSIBILITY OF OIL BEING VENTED OVERBOARD THROUGH THE ENGINE CRANKCASE VENT.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : 1 (MAN)

102-9012-1 SPRESSURIZED MAGNETO INSTALLATION ATA :58P, 58PA TJ-2 THRU TJ-49758TC, 58TCA TK-1 THRU TK-151"OPTIONAL" SB NO. 2205, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL "CONTINENTAL MOTORS KIT EQ6583"CONSISTING OF SLICK PRESSURIZED MAGNETOS FOR ENGINES TSI0-520-L OR TSI0-520-LB OR TSIO-520-WB ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE 102-9012-1 INSTALLATION SHOWN ON LEFT ENGINE IS TO BE THE SAME FOR THERIGHT ENGINE. IT TAKES (1) KIT PER AIRCRAFT.

WT. CHANGE : WT: -2 LBS; ARM: 31 IN.; MOMENT: -62 IN.-LBSEST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

33-4001-1 SDOOR, BAGGAGE SECONDARY LATCH INSTALLATION ATA : 5255, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-219656TC AND A56TC TG-2 THRU TG-9495, B95, D95A, E95 TD-2 THRU TD-721B55 TC-2197 AND AFTERC55, D55, E55 TC-350, TE-1 THRU TE-1148E55 TE-1149 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SECONDARY BAGGAGE DOOR LATCH ONAIRPLANES EQUIPPED WITH A UTILITY BAGGAGE DOOR.WT. CHANGE : N/AEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

33-4005-1 SFUEL RESERVOIR FOAM INSTALLATION ATA : 2858 TH-385 THRU TH-765, TH-767 THRU TH-772B55 TC-1608 THRU TC-1969, TC-1971 THRU

TC-2002E55 TE-938, TE-943 THRU TE-1080, TE-1082,

TE-1083SB NO. 2109 OR SUBSEQUENTTHE FOLLOWING AIRPLANES WHICH HAVE INSTALLED FUEL CELL RESERVOIR KIT NO. 35-9012 S (LH ANDRH) OR 35-9012-1 S (LH).THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE FOAM INSERT IN THE LH FUEL CELLRESERVOIR ASSEMBLY.55, A55, B55TC-1 THRU TC-349,TWT. CHANGE : N/AEST. MAN/HRS: : 8MEN : N/A

33-4005-2 SFUEL RESERVOIR FOAM INSERT INSTALLATION ATA : 2858 TH-385 THRU TH-765, TH-767 THRU TH-772B55 TC-1608 THRU TC-1969, TC-1971 THRU

TC-2002E55 TE-938, TE-943 THRU TE-1080, TE-1082,

TE-1083SB NO. 2109 OR SUBSEQUENTTHE FOLLOWING AIRPLANES WHICH HAVE INSTALLED FUEL CELL RESERVOIR KIT NO. 35-9012 S (LH ANDRH) OR 35-9012 S (RH).THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE FOAM INSERT IN THE RH FUEL CELLRESERVOIR ASSEMBLY.55, A55, B55TC-1 THRU TC-349,TCWT. CHANGE : N/AEST. MAN/HRS: : 8MEN : N/A


KIT CATALOG

33-5007-1 SGYRO, DIRECTIONAL - SPARES ATA : 31A55, B55 TC-191 THRU TC-349, TC-351 THRU TC-1156C55 TC-350, TE-1 THRU TE-451D95A TD-534 THRU TD-707THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE DIRECTIONAL GYRO 35-380039-1.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

33-5007-3 SGYRO, HORIZON - SPARES ATA :A55, B55 TC-191 THRU TC-349, TC-351 THRU TC-1156C55 TC-350, TE-1 THRU TE-451D95A TD-534 THRU TD-707THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ARTIFICIAL HORIZON GYRO 35-380043-1.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-0588-1TELESCOPING TUBE, WING HINGE PIN TOOL ATA :95-55, 58, 95THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO AID WITH THE INSTALLATION OF THEHINGE PINS USED TO ATTACH THE WING L.E. TO THE FRONT SPAR TO THE BOX SECTION..WT. CHANGE : N/A (INSTALLATION AID)EST. MAN/HRS: : 2MEN : 1 (MAN)

35-4012-1 SLANDING GEAR DRAG LEG, NOSE GEAR COMMONALITY - SPARES ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-209156TC TG-2 THRU TG-9458 TH-1 THRU TH-83158P TJ-1 THRU TJ-12758TC TK-1 THRU TK-6095, B95, D95A, E95 TD-2 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-1113THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 95-824018, 95-824018-1, AND 95-824018-3DRAG LEG ASSEMBLY WITH A COMMONALITY DRAG LEG.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-4014-3 SWINDOW 3RD TEAR DROP (TINTED) ATA :95 THRU B95 TD-1 THRU TD-452THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO ADD A CUT BACK TEAR DROP THIRDWINDOW THAT ENHANCES THE STYLING OF YOUR AIRPLANE WHILE INCREASING VISIBILITY.THIS KIT PROVIDES INFORMATION ON INSTALLATION ON AIRCRAFT WITH OR WITHOUT THE SMALL THIRWT. CHANGE : WITH SMALL WINDOW: WT: 5 LBS @ 160 ARM

WITHOUT SMALL WINDOW: WT: 7 LBSEST. MAN/HRS: : 85MEN : 1 (MAN)

35-5048-1 SFUEL FILLER NECK RESTRICTORS, NON-INDEXING ATA :55 TC-1 THRU TC-7495, B95, B95A TD-1 THRU TD-454SB NO. 2045, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FUEL FILLER NECK RESTRICTORS.WT. CHANGE : N/AEST. MAN/HRS: : 0.5MEN : 1 (MAN)

35-5050-1 PDOOR HANDLE, INSIDE CABIN REPLACEMENT - SPARES ATA :58 TH-1 THRU TH-160995-B55, 95-B55A, 95-B55B ALL95-C55, 95-C55A, D55, D55A ALLD95A, E95, 95-55, 95-A55 ALLE55, E55A, 56TC, A56TC ALL"OPTIONAL" SB NO. 2363THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH THE SPARES REPLACEMENT FOR THE INSIDECABIN DOOR HANDLES PART NUMBER 35-400436, 95-380010, AND 36-380099-1 ON INSERVICE AIRCRAFT.

FOR AFT UTILITY DOOR HANDLE, USE PART NUMBER 2316 OR C100160.NOTENOTENOTENOTE:::: "O"S.B.#2363

EFFECTS 14222 AIRCRAFT, 1 PER AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

35-8008-1 SWHEEL BEARING GREASE SEAL - SPARES ATA :58 TH-1 THRU TH-132458P TJ-3 THRU TJ-41158TC TK-1 THRU TK-148B55 TC-1 THRU TC-349, TC-351 THRU TC-2433C55, D55, E55 TC-350, TE-1 THRU TE-1199THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NOSE WHEEL BEARING THIN LIP GREASESEALS AS A SPARES REPLACEMENT FOR FELT OR THICK LIP SEALS INSTALLED IN BEECHCRAFT36-8002-1 OR CLEVELAND 40-77D AND 40-87A WHEEL ASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-8008-5 SWHEEL BEARING GREASE SEAL - SPARES ATA :58 TH-1 THRU TH-1259B55 TC-663, TC-979, TC-984 THRU TC-2387C55, D55, E55 TC-350, TE-1 THRU TE-1190THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL MAIN WHEEL BEARING THIN LIP SEALS AS ASPARES REPLACEMENT FOR FELT SEALS IN CLEVELAND 40-98 WHEELS WITH STANDARD BRAKES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

35-8008-7 SWHEEL BEARING GREASE SEAL - SPARES ATA :58 TH-873 THRU TH-1233B55 TC-2092 THRU TC-2375E55 TE-1114 THRU TE-1148THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL MAIN WHEEL BEARING THIN LIP GREASESEALS AS A SPARES REPLACEMENT FOR FELT SEALS ON CLEVELAND 40-128 WHEELS WITH HEAVY DUTYBRAKES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-9009-1 SFUEL CELL INSTALLATION ATA :55 TC-1 THRU TC-349, TC-351 THRU TC-160795, B95, D95A, E95 TD-2 THRU TD-721B95A, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55A, E55A, 58, 58AC55, D55, E55 TC-350, TE-1 THRU TE-937, TE-939 THRU

TE-942SI NO. 0459-281, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH 40 GALLON LEADING EDGE FUEL CELL(35-380135-9 OR -11) AND VELCRO PILE ON THE FUEL CELL LINERS.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)


TE-942SI NO. 0459-281, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RH 40-GALLON LEADING EDGE FUEL CELL(35-380135-10 OR -12) AND VELCRO PILE ON THE FUEL CELL LINERS.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)


TE-942SI NO. 0459-281, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH 25-GALLON LEADING EDGE FUEL CELL(96-380046-7 OR -9) AND VELCRO PILE ON THE FUEL CELL LINERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG


TE-942THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RH 25-GALLON LEADING EDGE FUEL CELL(96-380046-8 OR -10) AND VELCRO PILE ON THE FUEL CELL LINERS.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)

35-9009-5 SFUEL CELL ATTACHMENT FASTENER ATA :55 TC-1 THRU TC-349, TC-351 THRU TC-160795, B95, D95A, E95 TD-2 THRU TD-721B95A, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55A, E55A, 58, 58AC55, D55, E55 TC-350, TE-1 THRU TE-937, TE-939 THRU

TE-942SI NO. 0365-281, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL VELCRO PILE ON THE FUEL CELL LINER TOACCOMMODATE 35-380135 OR 96-384046 FUEL CELLS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : N/A

35-9018-3 SFUEL FLOW TRANSDUCER ATA :58P TJ-1 THRU TJ-49758TC TK-1 THRU TK-151THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ENGINE FUEL FLOWTRANSDUCER AND A LONGER HOSE ASSEMBLY AS SPARES FOR TRANSDUCER PART NUMBERS102-389012-1, 102-389012-5, 102-389012-11 AND 102-389034-1 CURRENTLY INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

36-3012-1 SWARNING HORN, FULL FLAP ATA :95B55 TC-2003 THRU TC-245695C55, D55, E55, 58 TH-1 THRU TH-1544, EXCEPT TH-1543SB NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW FLAP DOWN LIMIT SWITCH THAT WILLACTIVATE THE GEAR UP ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)


KIT CATALOG

36-3013-1 SLANDING GEAR WARNING LIGHT ATA :58 TH-773 THRU TH-1395 EXCEPT TH-138995B55 TC-2003 THRU TC-2456E55 TE-1084 THRU TE-1201SB NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A "GEAR UP"' LANDING GEAR WARNINGANNUNCIATOR LIGHT. THE LIGHT IS TO FLASH WHEN THE LANDING GEAR WARNING HORN SOUNDS ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 7 TO 8MEN : 1 (MAN)

36-3014-3 SLANDING GEAR RETRACT PREVENTION RELAY INSTALLATION LOWTHROTTLE

ATA :

58 TH-1389, TH-1396 THRU TH-1542, TH-1544SB NO. 2366 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SWITCHES AND A LATCHING RELAY THATWILL PREVENT THE LANDING GEAR FROM RETRACTING WHEN BOTH THROTTLES ARE SET SO THEENGINE MANIFOLD PRESSURES ARE BELOW 15-INCHES OF HG FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

36-3018-3 STACHOMETER INDICATOR - SPARES ATA :58, 58TC, 58PTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 102-380011-25 TACHOMETER ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

36-4007-1 SDOOR - CABIN CENTER 3RD LATCH POINT ATA :58, 58A TH-385 THRU TH-166458TC, 58TCA TK-1 THRU TK-15195B55, 95B55A TC-1608 THRU TC-2456E55, E55A TE-938, TE-943 THRU TE-1201"MANDATORY" SB NO. 2457, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING THIRD LATCH POINTMECHANISM WITH A THIRD LATCH POINT MECHANISM THAT GOES OVER CENTER WHEN THE DOORLATCH ASSEMBLY IS LATCHED AND REPLACES THE DOOR LATCH MECHANISM STOP.

NOTENOTENOTENOTE:::: IT MAY BE NECESSARY TO MODIFY THE ARM-REST TO INSTALL THIS KIT AS THEBELLCRANK MAY STRIKE THE ARM-REST ON SOME AIRCRAFT. (TIME TO MAKE ANYMODIFICATIONS TO THE ARM-REST NOT INCLUDED IN ESTIMATED MAN-HOURS).



KIT CATALOG

36-4008-1 SCABIN DOOR OVER CENTER THIRD LATCH POINT INSTALLATION ATA :56TC TG-16, TG-17, TG-33, TG-34, TG-44, TG-45,

TG-47 THRU TG-8358, 58A TH-1 THRU TH-38495-B55, 95-B55A TC-1093 THRU TC-160795-B55B TF-66 THRU TF-70D55, D55A TE-560 THRU TE-767E55, E55A TE-768 THRU TE-942 EXCEPT TE-938E95 TD-717 THRU TD-721"MANDATORY" SB NO. 2457, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING THIRD LATCH POINTMECHANISM WITH A THIRD LATCH POINT MECHANISM THAT GOES OVER CENTER WHEN THE DOORLATCH MECHANISM IS LATCHED.

NOTENOTENOTENOTE:::: IT MAY BE NECESSARY TO MODIFY THE ARM-REST TO PREVENT BELLCRANK STRIKINGARMREST ON SOME AIRCRAFT (EXTRA TIME ITEM).


36-4009-1 SBLOWER, FRESH AIR REPLACEMENT - SPARES ATA :58 SERIES"OPTIONAL" SB NO. 2380, REV. 2THIS KIT PROVIDES PARTS NECESSARY TO INSTALL A FRESH AIR BLOWER ASSEMBLY ON INSERVICEAIRCRAFT.

THIS KIT PROVIDES DETAILS WHICH ARE NOT NEEDED FOR THE REPLACEMENT OF THE FRESH AIRBLOWER INSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

36-4013-1CABIN DOOR SEAL ATA :58 TH-733 THRU TH-188358TC TK-1 THRU TK-15195-B55 TC-1936 THRU TC-2456E55 TE-1070, TE-1081 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEALS ON THE CABIN DOOR.




KIT CATALOG

36-4014-1OPENABLE WINDOW SEAL ATA :58 TH-902, TH-905 THRU TH-188358TC TK-61, TK-69 THRU TK-15195-B55 TC-2119, TC-2123 THRU TC-2456E55 TE-1123 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW SEAL FOR THE OPENABLE WINDOW.



36-4015-1SEALS, UTILITY DOOR ATA :58 TH-1 THRU TH-188358TC TK-1 THRU TK-151THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEALS ON THE CABIN DOOR.



36-5012-1 SFUEL FILLER NECK RESTRICTOR ATA :58P TJ-1 AND AFTER58TC TK-1 AND AFTERSB NO. 2045, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LIGHTNING RESISTANT FUEL CAPS ANDINSERTS. THIS KIT CONSISTS OF 2 CAPS AND INSERTS, 1 TOOL, AND KIT DRAWING. QUANTITY ASREQUIRED FOR AIRCRAFT OPTIONAL FUEL SYSTEMS.

NOTENOTENOTENOTE:::: THIS KIT REQUIRES THE USE OF "ALODINE 1200" WHICH IS NOT INCLUDED IN THIS KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

36-5013-1 SFUEL FILLER NECK RESTRICTOR ATA :55-B55 TC-75 THRU TC-245656TC TG-1 THRU TG-9458 TH-1 THRU TH-145095 TD-453 THRU TD-721C55-E55 TE-1 THRU TE-1201SB NO. 2045, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NONLIGHTING RESISTANT FUEL CAPS ANDINSERTS. THIS KIT CONSISTS OF 2 CAPS AND INSERTS, 1 TOOL AND KIT DRAWING. QUANTITY ASREQUIRED FOR AIRCRAFT OPTIONAL FUEL SYSTEMS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5MEN : 1 (MAN)

36-5017-1 SFIRE EXTINGUISHER REPLACEMENT REPLACEMENT KITS LISTEDBELOW ONLY FOR REFERENCE MODELS. SPARES SEE KIT CATALOGFOR AIRCRAFT MODELS AND SERIAL NUMBERS EXCEPT FORAIRCRAFT LISTED.

ATA :

95, B55, 95, C55, D55, E55, 56TC, A56TC,(SEE 36-5025-3 KIT)

58, 58TC AND 58P, (SEE 36-5025-1 KIT).

THIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL A FIRE EXTINGUISHER REPLACEMENT FORAIRCRAFT EQUIPPED WITH 890017 OR 890275 FIRE EXTINGUISHER (PART NUMBER OF WALTER KIDDE)OR FR-2 1/2 FIRE EXTINGUISHER (PART NUMBER OF GENERAL FIRE EXT. CORP) OR MODEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

36-5025-1FIRE EXTINGUISHER (*RESTRICTED ARTICLE* IS FIRE BOTTLE) -SPARES

ATA :

5858P58TCFIRE EXTINGUISHER SPARES KIT (RESTRICTED ARTICLE IS FIRE BOTTLE). THIS KIT PROVIDES PARTSAND INFORMATION TO INSTALL A "352TS" FIRE EXTINGUISHERS THAT WERE PREVIOUSLY EQUIPPEDWITH THE "FR-2 1/2" FIRE EXTINGUISHER (PART NUMBER GENERAL FIRE EXTINGUISHER CO

NOTENOTENOTENOTE:::: FOR OTHER LIGHT SINGLE AND TWIN PISTON AIRCRAFT SEE KIT: 37-5025-3.WT. CHANGE : WT: 5 LBS -WT. OF FULL WT. OF FIRE EXTINGUISHER BEING REPLACED.EST. MAN/HRS: : 3 TO 4 ARM: 118, MOMENT: TBDMEN : 1 (MAN)


KIT CATALOG

36-5027-1COVER ASSEMBLY, RH CONTROL WHEEL ATA :95-B55, E55, 58, 58TC, 58P,THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 36-530171-23 COVER ASSEMBLY ONINSERVICE AIRCRAFT THAT PREVIOUSLY AHD 50-534846-11 PLATE INSTALLED ON THE RH CONTROLWHEEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

36-5040-0003G36/G58 MODEL NAME EMBLEM INSTL ATA :BARON G58 TH-2125 THRU TH-2135THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A MODEL NAME EMBLEM FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "9372DK" FOAM ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. A PRODUCT OF 3MBONDING SYSTEMS IN ST. PAUL, MINN. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.


36-8005-3ROLLER ASSEMBLY, RETRACTION MECHANISM, NOSE LANDING GEARSHAFT

ATA :

58 TH-578 AND AFTER58P TJ-3 THRU TJ-49758TC TK-1 THRU TK-15195-B55 TC-1749, TC-1828 THRU TC-2456E55 TE-1027 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE THE SERVICE LIFE OF THE NOSE GEARRETRACT MECHANISM ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

55-2001-1 SEXTERIOR PLACARD ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-2456C55, D55, E55 TC-350, TE-1 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS. A SPRAY CAN OF PROTECTIVE FINISH IS INCLUDED WITH THEKIT.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

55-2002-1 SINTERIOR PLACARD ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-2456C55, D55, E55 TC-350, TE-1 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

55-2003-1 SEXTERIOR PLACARD ATA :56TC, A56TC TG-2 THRU TG-94THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS. A SPRAY CAN OF PROTECTIVE FINISH IS INCLUDED WITH THEKIT.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

55-2004-1 SINTERIOR PLACARD ATA :56TC, A56TC TG-2 THRU TG-94THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

55-3017-1 SOVERVOLTAGE RELAY REPLACEMENT ATA :55, A55, B55 TC-1 THRU TC-104256TC, A56TC TG-1 THRU TG-9495, B95, D95A, E95 TD-1 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-449THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT OVERVOLTAGE RELAY FORTHE 138-2 RELAY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-3019-1 SFUEL TRANSMITTER - SPARES ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-2 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-49, TE-51 THRU

TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES FUEL GAGE TRANSMITTER ONAIRPLANES EQUIPPED WITH A 95-380012-13 TRANSMITTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

55-3021-1 SFUEL QUANTITY INDICATING SYSTEM ATA :56TC TG-2 THRU TG-83THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH FUEL QUANTITY INDICATINGSYSTEM. THIS INCLUDES THE FUEL QUANTITY GAGE, PC BOARD AND THE INBOARD, OUTBOARD ANDNACELLE TRANSMITTERS. (91- OR 103-GAL. SYSTEM)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3021-2 SFUEL QUANTITY SYSTEM ATA :56TC TG-2 THRU TG-83THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RH FUEL QUANTITY INDICATINGSYSTEM. THIS INCLUDES THE FUEL QUANTITY GAGE, PC BOARD, AND THE INBOARD, OUTBOARD, ANDNACELLE TRANSMITTERS. (91- OR 103-GAL. SYSTEM)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3022-1 SLIGHT INSTALLATION, STARTER ENERGIZED ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-2339,

TC-2341 THRU TC-235456TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-1193 TH-1 THRU TH-1193}58P TJ-3 THRU TJ-31658TC TK-1 THRU TK-13395, B95, D95A, E95 TD-1 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-1180THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STARTER ENERGIZED LIGHT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-3023-1 SFUEL QUANTITY PRINTED CIRCUIT BOARD, IMPROVED ATA :58 TH-410 THRU TH-124958P TJ-3 THRU TJ-36858TC TK-1 THRU TK-144B55 TC-1632 THRU TC-2402E55 TE-956 THRU TE-1189SI NO. 1196 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED PRINTED CIRCUIT BOARDDESIGNED TO ELECTRICALLY DAMPEN THE FUEL QUANTITY INDICATOR MOVEMENT.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

55-3024-1DUAL VOLTAGE REGULATOR INSTL ATA : 24WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

55-3024-1 SKIT-S-DUAL VT REG ATA : 24WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

55-3025-3 SPRINTED CIRCUIT BOARD INSTALLATION ATA :58 TH-1 THRU TH-1376B55 TC-1178 THRU TC-2456D55, E55 TE-650 THRU TE-1201SB NO. 2016 OR SUBSEQUENTTHIS KIT PROVIDES IMPROVED CIRCUIT PROTECTION BY REPLACING THE ALTERNATOR AUXILIARYTERMINAL WIRE IN-LINE FUSE WITH A PC BOARD.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

55-3026-1 SALTERNATOR FIELD FUSE INSTALLATION ATA :58 TH-995 THRU TH-1376B55 TC-2203 THRU TC-2456E55 TE-1150 THRU TE-1201SB NO. 2077 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ALTERNATOR FIELD FUSE TO REDUCE THEPOSSIBILITY OF A SHORTED FIELD ON ONE ALTERNATOR DISABLING BOTH ALTERNATORS.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

55-3028-3 PCLOCK INSTALLATION CONTROL WHEEL (28-VOLT) ATA :E55, 95-C55, A56-TC, 58, 58P, 58-TC, D95ATHIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-3, 50-534622-13, 50-534622-17,50-534622-21, 50-384209-1, 50-384210-1, OR 50-384211-1 8-DAY CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3029-3 PCLOCK INSTALLATION, INSTRUMENT PANEL, (28-VOLT) - SPARES ATA :D55, E55, 95-B55, 56TC, 58THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 50-380013-5 AND 58-380015-3 8-DAY CLOCKS OR58-380077-3 AND 58-380077-7 ELECTRIC CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3030-1 SFLASHER INSTALLATION ATA :55, A55, B55, C55, 95, B95, D95ATHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE 624 FLASHER WITH 76259-1.WT. CHANGE : N/AEST. MAN/HRS: : 1MEN : 1 (MAN)

55-4014- PMODERNIZATION-GROS WT 5100#-MODEL 95 ATA :B55 TC-371, TC-502 THRU TC-954THIS KIT PROVIDES THE PARTS AND INFORMATION TO INCREASE THE GROSS WEIGHT TO 5100 POUNDS.(PROPELLERS ARE NOT INCLUDED)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-4016- PWINDSHIELD INSTALLATION - ONE PIECE ATA : 5655, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-94495, B95, B95A, D95A TD-2 THRU TD-707B55B (T42A) TF-1 THRU TF-65THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A "TINTED" NOT LONG SLOPE, 1/4 INCH THICK,ONE PIECE WINDSHIELD.

NOTENOTENOTENOTE:::: (SEE BROCHURE FIGURES 1 THRU 4).WT. CHANGE : WT: 4 LBS @ 68 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)


KIT CATALOG

55-4020-1 SELEVATOR TRIM TAB ACTUATOR LINKAGE, IMPROVED ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-1070,

TC-107256TC TG-1 THRU TG-41, TG-43, TG-44, TG-46

THRU TG-49, TG-52 THRU TG-54, TG-56THRU TG-62

95, B95, D95A, E95 TD-2 THRU TD-706, TD-708 THRU TD-714C55, D55 TC-350, TE-1 THRU TE-520, TE-522 THRU

TE-524, TE-526, TE-527, TE-539 THRUTE-542

SI NO. 0610-152, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE THE ELEVATOR TRIM TAB ACTUATOR RODEND ATTACHMENT.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

55-4029-1 SRUDDER PEDAL BELL CRANK BRACKET REPLACEMENT, IMPROVED ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-194495, B95, D95A, E55 TD-1 THRU TD-721SERVICE LETTER NO. 0869-154, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BELL CRANK SUPPORT BRACKETASSEMBLIES WITH LH AND RH CASTINGS, REPLACING SHEET METAL BRACKET ASSEMBLIES.

THIS KIT CONSIST OF 2 BRACKETS, BOLTS, NUTS, SCREWS, WASHERS, COTTER PINS, RIVETS AND KITDRAWING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24MEN : 2 (MEN)

55-4029-3 SRUDDER PEDAL BELL CRANK BRACKET REPLACEMENT, IMPROVED ATA :C55, C55A TC-350, TE-1 THRU TE-49, TE-51 THRU

TE-300SI NO. 0869-154, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BELL CRANK SUPPORT BRACKET ASSEMBLESWITH LH AND RH CASTINGS, REPLACING SHEET METAL BRACKET ASSEMBLIES.

NOTENOTENOTENOTE:::: THIS KIT CONSISTS OF MOUNTING, BOLTS, NUTS, SCREWS, WASHERS, COTTER PINS,RIVETS AND KIT DRAWING.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24MEN : 2 (MEN)


KIT CATALOG

55-4030-1 SFUSELAGE BULKHEAD REINFORCEMENT, STABILIZER ATTACHMENT ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-2124B95, D95A, E95 TD-21 THRU TD-721SI NO. 0990, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED FOR THE INSPECTION OF THE BULKHEADS ATTHE HORIZONTAL STABILIZER STUB SPARS AND FOR THE REPAIR OR REPLACEMENT OF CRACKEDPARTS.WT. CHANGE : WT: 0.6 LBS @ 257.6 ARMEST. MAN/HRS: : 60MEN : 1 (MAN)

55-4030-3 SFUSELAGE BULKHEAD REINFORCEMENT, STABILIZER ATTACHMENT ATA :58P TJ-3 THRU TJ-14158TC TK-1 THRU TK-68SI NO. 0990, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED FOR THE INSPECTION OF THE BULKHEADS ATTHE HORIZONTAL STABILIZER STUB SPARS AND FOR THE REPAIR OR REPLACEMENT OF CRACKEDPARTS.WT. CHANGE : WT: 0.6 LBS @ 257.6 ARMEST. MAN/HRS: : 60MEN : 1 (MAN)

55-4030-5 SFUSELAGE BULKHEAD REINFORCEMENT, STABILIZER ATTACHMENT ATA :56TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-908C55, D55, E55 TC-350, TE-1 THRU TE-1124SI NO. 0990, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED FOR THE INSPECTION OF THE BULKHEADS ATTHE HORIZONTAL STABILIZER STUB SPARS AND FOR THE REPAIR OR REPLACEMENT OF CRACKEDPARTS.WT. CHANGE : WT: 0.6 LBS @ 257.6 ARMEST. MAN/HRS: : 60MEN : 1 (MAN)

55-4031-1 SNOSE BAGGAGE DOOR SECONDARY LATCH ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-238456TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-124658P TJ-3 THRU TJ-37058TC TK-1 THRU TK-139C55, D55, E55 TC-350, TE-1 THRU TE-1189THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SECONDARY LATCH ON THE NOSEBAGGAGE DOOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-4034-1 SAIR CONDITIONER RECEIVER DRYER INSTALLATION ATA :58 TH-873 THRU TH-123858TC TK-68 THRU TK-138THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RECEIVER DRYER ON AIRPLANES WITH AFACTORY INSTALLED AIR CONDITIONER.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : 1 (MAN)

55-4034-3 SAIR CONDITIONER RECEIVER DRYER INSTALLATION ATA :E55 TE-1119, TE-1128, TE-1130, TE-1133,

TE-1142, TE-1152, TE-1166, TE-1181 THRUTE-1189

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RECEIVER DRYER ON AIRPLANES WITH AFACTORY INSTALLED AIR CONDITIONER.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : 1 (MAN)

55-5012-1 PSHOULDER HARNESS INSTALLATION (BEIGE ONLY) ATA : 2556TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-173B55 TC-966 THRU TC-1400C55, D55, E55 TC-350, TE-1 THRU TE-847SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE PAGES 3-42 AND 3-43 FOR MORE INFORMATION)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES, COMPLETE WITH ANINERTIA REEL, FOR THE PILOT AND COPILOT SEATS. BEIGE ONLY.WT. CHANGE : B55 THROUGH E55, 56TC AND A56TC: WT: 4 LBS @ 97 ARM 58: WT: 4 LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 1 (MAN)

55-5012-3 PSHOULDER HARNESS INSTALLATION (BLACK ONLY) ATA : 2556TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-173B55 TC-966 THRU TC-1400C55, D55, E55 TC-350, TE-1 THRU TE-847SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE PAGES 3-42 AND 3-43 FOR MORE INFORMATION)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES, COMPLETE WITH ANINERTIA REEL, FOR THE PILOT AND COPILOT SEATS.WT. CHANGE : B55 THROUGH E55, 56TC AND A56TC: WT: 4 LBS @ 97 ARM @ 97 ARM 58: WT: 4 LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 1 (MAN)


KIT CATALOG

55-5012-5 PSHOULDER HARNESS INSTALLATION (BLACK ONLY) ATA : 2555, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-96595, B95, D95A TD-2 THRU TD-637SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE PAGES 3-42 AND 3-43 FOR MORE INFORMATION)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES, COMPLETE WITH ANINERTIA REEL, FOR THE PILOT AND COPILOT SEATS.WT. CHANGE : WT: 4 LBS @ 97 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

55-5012-7 PSHOULDER HARNESS INSTALLATION (BEIGE ONLY) ATA : 2555, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-96595, B95, D95A TD-2 THRU TD-637SB NO. 2031, REV. 2 OR SUBSEQUENT (SEE PAGES 3-42 AND 3-43 FOR MORE INFORMATION)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES, COMPLETE WITH ANINERTIA REEL FOR THE PILOT AND COPILOT SEATS. BEIGE ONLY.WT. CHANGE : WT: 4 LBS @ 97 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

55-5014-1 SHEATER PRESSURE DIFFERENTIAL SWITCH RELOCATION ATA :58 TH-437 THRU TH-633B55 TC-1658 THRU TC-1875E55 TE-959, TE-969 THRU TE-1048SI NO. 0721-412, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE HEATER PRESSURE DIFFERENTIALSWITCH TO AVOID THE ACCUMULATION OF MOISTURE IN THE SWITCH.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

55-8002- PWHEEL AND BRAKE INSTALLATION (SINGLE CONTROL ONLY) ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-1288THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED WHEEL, TIRE AND BRAKEASSEMBLY AND MASTER CYLINDERS.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)


KIT CATALOG

55-8002-3 PWHEEL AND BRAKE INSTALLATION (SINGLE CONTROL ONLY) ATA :D95A TD-534 THRU TD-696, TD-698THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED WHEEL, TIRE AND BRAKEASSEMBLY AND MASTER CYLINDERS.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURES 5 AND 6 FOR ADDITIONAL INFORMATION.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)

55-8005- PBRAKE INSTALLATION, DUAL CONTROL ATA :58 TH-1 THRU TH-383D55 -695 THRU TE-767E55 TE-768 THRU TE-945THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BRAKE CONTROLS FOR THE COPILOT.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURES 5 AND 6 FOR ADDITIONAL INFORMATION.WT. CHANGE : D55 AND E55; WT: 4 LBS @ 54 ARM M58: WT: 4 LBS @ 44 ARMEST. MAN/HRS: : 40MEN : 1 (MAN)

55-9011-1 SFUEL BOOST PUMP INSTALLATION (1/2 INCH FUEL LINE) ATA :B55 TC-955 THRU TC-1419C55 THRU E55 TE-1 THRU TE-856SI NO. 0584 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED HIGH AND LOW PRESSUREFUEL BOOST PUMP ON AIRPLANES EQUIPPED WITH ONE-HALF INCH FUEL LINES IN THE WING FUELSYSTEM.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURES 5 AND 6 FOR ADDITIONAL INFORMATION.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

55-9011-3 SFUEL BOOST PUMP INSTALLATION ( 3/8 INCH FUEL LINE) ATA :A55, B55 TC-421 THRU TC-954SI NO. 0584-285 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED HIGH AND LOW PRESSUREFUEL BOOST PUMP ON AIRPLANES EQUIPPED WITH THREE-EIGHTHS INCH FUEL LINES IN THE WING FUELSYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

55-9013-1 SCOWL FLAP, MANUAL INSTALLATION ATA :95-C55, 95-C55A, D55, D55A, E55, E55A TC-350, TE-1 THRU TE-937, TE-939 THRU

TE-942CLASS III, SI NO. 0652-242, REV. 1THIS KIT NO LONGER OFFERED, BUT YOU CAN CONVERT 55-9013-3 S KIT FOR USE ON REFERENCEDAIRCRAFT BY PURCHASING THE 55-9013-3 S KIT PLUS 2 EACH 96-910028-29 PUSH RODS AND 2 EACH55-4853-2010 CABLES. GETTING LOCAL 337 FORM APPROVAL OF THE INSTALLATION USING KWT. CHANGE : N/AEST. MAN/HRS: : 32MEN : 2 (MEN)

55-9013-3 SCOWL FLAP, MANUAL INSTALLATION ATA :58 TH-1 THRU TH-384CLASS III, SI NO. 0652-242, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A MANUAL COWL FLAP SYSTEMON INSERVICE AIRCRAFT.WT. CHANGE : WT: -1 LBS; ARM: 56 IN.EST. MAN/HRS: : 32MEN : 2 (MEN)

55-9018-1 SFUEL TRANSMITTER INSTALLATION, AC GAGE ATA :55, A55, B55 TC-1 THRU TC-349 TC-351 THRU TC-129895, B95, D95A, E95 TD-403 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE INBOARD AND OUTBOARD TRANSMITTERSFOR 39-OR 40-GALLON SYSTEMS. THIS KIT MAY BE INSTALLED TO REPLACE EITHER THE LH OR RHTRANSMITTER SYSTEM. EACH KIT PROVIDES PARTS FOR ONE SYSTEM ONLY. AIRPLANES MUST BE EWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9018-3 SFUEL TRANSMITTER INSTALLATION, AC GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A AND E95 TD-403 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH 25-GALLON MAIN TRANSMITTER.AIRPLANES MUST BE EQUIPPED WITH AC GAGE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-9018-4 SFUEL TRANSMITTER INSTALLATION, AC GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-403 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RH 25-GALLON MAIN TRANSMITTER.AIRPLANES MUST BE EQUIPPED WITH AC GAGE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9018-5 SFUEL TRANSMITTER INSTALLATION, AC GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-403 THRU TD-767C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH INBOARD AND OUTBOARD 31-GALLON AUXILIARY TRANSMITTERS. AIRPLANES MUST BE EQUIPPED WITH AC GAGE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9018-6FUEL TRANSMITTER INSTALLATION, AC GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-403 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RH INBOARD AND OUTBOARD 31-GALLON AUXILIARY TRANSMITTERS. AIRPLANES MUST BE EQUIPPED WITH AC GAGE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9018-6 SRH FUEL TRANS W/EX GAGE 31GAL AUX ATA : 28WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

55-9019-1 SFUEL TRANSMITTER INSTALLATION, ROCHESTER GAGE ATA :55, A55, B55 TC-1 THRU TC-349,

TC-351 THRU TC-129895, B95, D95A, E95 TD-2 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GAGE, INBOARD AND OUTBOARDTRANSMITTERS FOR 39- OR 40-GALLON FUEL SYSTEMS. THIS KIT MAY BE INSTALLED TO REPLACEEITHER THE LH OR RH GAGING SYSTEM. ONE KIT PROVIDES PARTS FOR ONE SYSTEM ONLY.

NOTENOTENOTENOTE:::: WHEN REPLACING AN AC GAGE WITH A ROCHESTER GAGE, IT IS IMPERATIVE THAT ALLTRANSMITTERS BE REPLACED ON THAT SIDE. IT IS PERMISSIBLE TO HAVE AROCHESTER GAGE INSTALLED ON ONE SIDE OF THE AIRPLANE AND AN AC GAGE ONTHE OTHER SIDE.


55-9019-3 SFUEL TRANSMITTER INSTALLATION, ROCHESTER GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-2 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GAGE, LH MAIN AND LH INBOARD ANDOUTBOARD AUXILIARY TRANSMITTERS ON 25-GALLON MAIN AND 31-GALLON AUXILIARY FUEL SYSTEM.



55-9019-4 SFUEL TRANSMITTER INSTALLATION, ROCHESTER GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95. D95A, E95 TD-2 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GAGE, RH MAIN AND RH INBOARD ANDOUTBOARD AUXILIARY TRANSMITTERS ON 25-GALLON MAIN AND 31-GALLON AUXILIARY FUEL SYSTEM.




KIT CATALOG

55-9019-5 SFUEL TRANSMITTER INSTALLATION, ROCHESTER GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-2 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767EFTD-2 THRU TD-721F}SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GAGE, LH INBOARD MAIN, LH OUTBOARDMAIN AND LH INBOARD AND OUTBOARD AUXILIARY TRANSMITTERS ON A 40-GALLON MAIN, 31-GALLONAUXILIARY FUEL SYSTEM.



55-9019-6 SFUEL TRANSMITTER INSTALLATION, ROCHESTER GAGE ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-129895, B95, D95A, E95 TD-2 THRU TD-721C55, D55 TC-350, TE-1 THRU TE-767SI NO. 0925, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GAGE, RH INBOARD MAIN, RH OUTBOARDMAIN AND RH INBOARD AND OUTBOARD AUXILIARY TRANSMITTERS ON A 40- GALLON MAIN, 31-GALLONAUXILIARY FUEL SYSTEM.

NOTENOTENOTENOTE:::: WHEN REPLACING AN AC GAGE WITH A ROCHESTER GAGE, IT IS IMPERATIVE THAT ALLTRANSMITTERS BE REPLACED, ON THAT SIDE. IT IS PERMISSIBLE TO HAVE AROCHESTER GAGE INSTALLED ON ONE SIDE OF THE AIRPLANE AND AN AC GAGE ONTHE OTHER SIDE.


55-9020-1 SCOWL FLAP ACTUATOR - SPARES ATA :95, B95, D95A, E95 TD-2 THRU TD-721THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COWL FLAP ACTUATOR ASSEMBLY,95-910035-1, AS A SPARES REPLACEMENT FOR THE 95-369011-5 FLAP ACTUATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9021-1 SFUEL BOOST PUMP - SPARES ATA :55, A55 TC-1 THRU TC-250, TC-252 THRU TC-336THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO REPLACEMENT FUEL BOOST PUMPS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

55-9022-1 PPROPELLER DEICE, 2-BLADE HARTZELL ATA :B55 TC-1416 THRU TC-2456E55 TE-849 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A THERMALLY EFFICIENT ELECTRICPROPELLER DE-ICER ON AIRPLANES WITH POST LIT INSTRUMENTS AND HARTZELL 2-BLADEPROPELLERS.WT. CHANGE : WT: 12 LBS @ 30 ARMEST. MAN/HRS: : 50 TO 60MEN : 1 (MAN)

55-9022-3 PPROPELLER DEICE, 2-BLADE HARTZELL ATA :B55 TC-1416 THRU TC-2456E55 TE-849 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A THERMALLY EFFICIENT ELECTRICPROPELLER DE-ICER ON AIRPLANES WITH WEDGE LIT INSTRUMENTS AND HARTZELL 2-BLADEPROPELLERS.WT. CHANGE : WT: 12 LBS @ 30 ARMEST. MAN/HRS: : 50 TO 60MEN : 1 (MAN)

55-9022-5 PPROPELLER DEICE, 3-BLADE HARTZELL ATA :B55 TC-502 THRU TC-2456E55 TE-849 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A THERMALLY EFFICIENT ELECTRICPROPELLER DE-ICER ON AIRPLANES WITH POST LIT INSTRUMENTS AND HARTZELL 3-BLADEPROPELLERS.WT. CHANGE : WT: 12 LBS @ 30 ARMEST. MAN/HRS: : 60MEN : 2 (MEN)

55-9022-7 PPROPELLER DEICE, 3-BLADE HARTZELL ATA :E55 TC-502 THRU TC-2456, TE-849 THRU

TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A THERMALLY EFFICIENT ELECTRICPROPELLER DE-ICER ON AIRPLANES WITH WEDGE LIT INSTRUMENTS AND HARTZELL 3-BLADEPROPELLERS.WT. CHANGE : WT: 12 LBS @ 30 ARMEST. MAN/HRS: : 60MEN : 2 (MEN)


KIT CATALOG

55-9023-1 PPROPELLER DEICE, 3-BLADE MCCAULEY ATA :D55 TE-452 THRU TE-767THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTROTHERMAL PROPELLER DE-ICERON AIRPLANES WITH POST LIT INSTRUMENTS AND MCCAULEY 3-BLADE 3AF32C75/82NB-6 PROPELLERS.WT. CHANGE : N/AEST. MAN/HRS: : 60MEN : 2 (MEN)

55-9023-3 PPROPELLER DEICE, 3-BLADE MCCAULEY ATA :E55 TE-768 THRU TE-849THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTROTHERMAL PROPELLER DE-ICERON AIRPLANES WITH POST LIT INSTRUMENTS AND MCCAULEY 3-BLADE 3AF82C75/82NB-6 PROPELLERS.WT. CHANGE : N/AEST. MAN/HRS: : 60MEN : 2 (MEN)

55-9023-5 PPROPELLER DEICE, 3-BLADE MCCAULEY ATA :E55 TE-768 THRU TE-849THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTROTHERMAL PROPELLER DE-ICERON AIRPLANES EQUIPPED WITH WEDGE LIT INSTRUMENTS AND MCCAULEY 3-BLADE 3AF32C75/82NB-6PROPELLERS.WT. CHANGE : N/AEST. MAN/HRS: : 60MEN : 2 (MEN)

55-9024-1 SFUEL VENT, FLUSH ATA :58 TH-1 THRU TH-854E55 TE-1084 THRU TE-1107THIS KIT CONTAINS PARTS AND INFORMATION TO INSTALL FLUSH FUEL VENTS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-9025-1 SENGINE MOUNT - SPARES ATA :55 TC-1 THRU TC-35, TC-37, TC-39 THRU

TC-41, TC-43 THRU TC-95, TC-97 THRUTC-112, TC-114 THRU TC-167, TC-169 THRUTC-175

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 96-910005-75 ENGINE MOUNT AS A SPARESREPLACEMENT FOR THE 96-910005-55 ENGINE MOUNT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-2002-1 SEXTERIOR PLACARD ATA :58 TH-1 AND AFTER58P TJ-3 AND AFTER58TC TK-1 THRU TK-151THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS. A SPRAY CAN OF PROTECTIVE FINISH IS INCLUDED WITH THEKIT.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

58-2003-1 SINTERIOR PLACARD ATA :58 TH-1 AND AFTER58P TJ-3 AND AFTER58TC TK-1 THRU TK-151THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

58-3003-1 SANTENNA, B-6 - SPARES ATA :58 TH-175 THRU TH-77258TC TK-1 THRU TK-34B55 TC-1403 THRU TC-2002E55 TE-847 THRU TE-1083THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 58-380112 ANTENNA AS A SPARESREPLACEMENT FOR THE B-6 ANTENNA.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-3004-1 PTAXI LIGHT INSTALLATION, NOSE GEAR ATA :95-C55, D55, E55, 56TCTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE EXISTING TAXI LIGHTFROM THE NOSE CONE TO THE NOSE GEAR ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT INCLUDE A NOSE CONE. IF KIT IS BEING USED IN CONJUNCTIONWITH A NOSE MOUNTED RADAR KIT, NOSE CONE WILL BE PROVIDED WITH THE RADARKIT.



KIT CATALOG

58-3004-3 PTAXI LIGHT INSTALLATION, NOSE GEAR ATA :95-B55THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE EXISTING TAXI LIGHTFROM THE NOSE CONE TO THE NOSE GEAR.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT INCLUDE A NOSE CONE. IF KIT IS BEING USED IN CONJUNCTIONWITH A NOSE MOUNTED RADAR KIT, NOSE CONE WILL BE PROVIDED WITH THE RADARKIT.


58-3005-1 PALTERNATOR INSTALLATION, 100-AMPERE ATA :58 TH-94 THRU TH-597, TH-599 THRU TH-647E55 TE-768 THRU TE-1063THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EXISTING 50-AMP ALTERNATORS WITH 100-AMP ALTERNATORS. ALTERNATORS ARE INCLUDED.

NOTENOTENOTENOTE:::: OTHER TH SERIES SEE 58-3005-3 P OR -5 P OR 58-3007-1 P KITS.WT. CHANGE : WT: 22.1 LBS @ 40.6 ARMEST. MAN/HRS: : 36 TO 40MEN : 1 (MAN)

58-3005-3 PALTERNATOR INSTALLATION, 100-AMPERE ATA :58 TH-598, TH-648 THRU TH-774E55 TE-1064 THRU TE-1083THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EXISTING 50-AMP ALTERNATORS WITH 100-AMP ALTERNATORS. ALTERNATORS ARE INCLUDED.WT. CHANGE : WT: 16.4 LBS @ 34.4 ARMEST. MAN/HRS: : 36 TO 40MEN : 1 (MAN)

58-3005-5 PALTERNATOR INSTALLATION, 100-AMPERE ATA :58 TH-775 THRU TH-1193E55 TE-1084 THRU TE-1182TH-775 THRU TH-1193F}THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EXISTING 50-AMP ALTERNATORS WITH 100-AMP ALTERNATORS. ALTERNATORS ARE INCLUDED.WT. CHANGE : WT: 14.5 LBS @ 31.3 ARMEST. MAN/HRS: : 37 TO 40MEN : 1 (MAN)


KIT CATALOG

58-3007-1 PALTERNATOR INSTALLATION, 100-AMPERE ATA :58 TH-895 THRU TH-1053, TH-1056, TH-1057E55 TE-1122 THRU TE-1162THIS KIT SUPPLIES PARTS AND INFORMATION TO CONVERT TWO PRESTOLITE ALTERNATORS TO TCMCRITTENDEN 100-AMPERE ALTERNATORS. THIS KIT DOES NOT SUPPLY ALTERNATORS PART NUMBER:646491A1 OR GASKETS PART NUMBER: 629436. YOU WILL HAVE TO ORDER THESE ITEMS OR REPLACWT. CHANGE : N/AEST. MAN/HRS: : 36 TO 40MEN : 1 (MAN)

58-3007-3ALTERNATOR INSTALLATION, 100-AMPERE ATA :58 TH-895 THRU TH-1053, TH-1056, TH-1057E55 TE-1122 THRU TE-1162THIS KIT SUPPLIES PARTS AND INFORMATION NECESSARY TO REPLACE (2) 85 AMP PRESTOLITEALTERNATOR WITH TCM CRITTENDEN 100 AMP ALTERNATOR ON INSERVICE AIRCRAFT.WT. CHANGE : WT: -6.8 LBS; ARM: 26.6 : MOMENT: - 181 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

58-3009-1 PSTALL WARNING LIFT DETECTOR, HEATED ATA :58 TH-1 THRU TH-1376D55 AND E55 TE-938, TE-943 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED HEATED STALL WARNING LIFTDETECTOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-3010-1 SANTENNA, VHF COMM ATA :58 TH-973 THRU TH-136458P TJ-169 THRU TJ-44358TC TK-85 THRU TK-151B55 TC-2181 THRU TC-2456E55 TE-1143 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT VHF COMMANTENNA.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-3011-1 STURN AND SLIP INDICATOR - SPARES ATA :58 TH-188 THRU TH-1388, TH-1390 THRU

TH-1395THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE96-384063-1 TURN AND SLIP INDICATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-3012-1 SHEATED WINDSHIELD INSTALLATION - SPARES ATA :D55, E55, 58, 58TCTHIS KIT IS THE SPARES REPLACEMENT FOR 102-364044-51 HEATED WINDSHIELD ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 48MEN : 1 (MAN)

58-3013-1 SWINDSHIELD, HEATED PATCH SEALING ATA :58TC TK-1 AND AFTERD55, E55, 58 PRIOR TO TC-1615THIS KIT PROVIDES PARTS NECESSARY TO IMPROVE THE SEALING OF THE LOWER FORWARD END OFTHE HEAT PATCH ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR 58P BARON, SEE 102-3011-1 S.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

58-3014-1KIT-GARMIN 530/SHADIN 200+/MD41-1469INFO ATA : 28WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

58-3016-1KIT -GLIDESLOPE ANTENNACHANGE-INFO ONLY ATA : 2358 TH-1940 THRU TH-1966 & TH-1968THIS KIT PROVIDES INFORMATION FOR THE REMOVAL OF THE GLIDESLOPE ANTENNA (100-384128), THEGLIDESLOPE ANTENNA MOUNTING BRACKET ASSY (58-340450-3), THE GLIDESLOPE COAX CABLE(36-340486-41), THE GLIDESLOPE ANTENNA COUPLER (101-380043), AND THE NAV (VOR) ANTEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

58-3018-0001AIR CONDITIONING TIME DELAY RELAY ATA :58P & 58TCTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE OBSOLETE AIRCONDITIONING THERMAL TIME DELAY RELAY, P/N TLR117300 OR TNR117300, WITH AN AVAILABLEELECTRONIC RELAY ASSY ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

58-4002-1 SSPAR INSTALLATION, OUTBOARD WING FORWARD ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-160756TC TG-2 THRU TG-9458 TH-1 THRU TH-23495, B95, D95A TD-2 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-937, TE-939 THRU

TE-942THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMMONALITY SPAR 000-110011-3, -4, -5 OR-6. (SPAR IS NOT A COMPONENT PART OF THE KIT, ONE KIT PER SPAR).WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-4003-1 SSEATING STRUCTURE TIE-DOWN, AFT ATA :55, A55, B55 TC-1 THRU TC-349 TC-351 THRU TC-200956TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-77658P TJ-2 THRU TJ-9058TC TK-1 THRU TK-38C55, D55, E55 TC-350, TE-1 THRU TE-1085SI NO. 0910 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REVISED TIE-DOWN FOR THE 5TH AND/OR6TH SEATS TO PROVIDE ADDITIONAL LOAD-CARRYING CAPABILITIES. THIS KIT MUST BE INSTALLEDPRIOR TO OR IN CONJUNCTION WITH KITS 58-5009-5 P, -7 P, -9 P, -11 P. ONE KIT REWT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

58-4007-1 PDEICE SYSTEM, OUTBOARD WING, PNEUMATIC ATA :58 TH-1 AND AFTERD55, E55 TE-452 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PNEUMATIC SURFACE DE-ICER SYSTEM ONAIRPLANES WITH NO WET WINGS. BOOTS ARE NOT INCLUDED WITH KIT. YOU WILL HAVE TO ORDER 1EACH OF THE FOLLOWING BOOTS FOR USE WITH THIS KIT: 25S-7D5057-01, -02, -07, -08

NOTENOTENOTENOTE:::: BEFORE YOU PURCHASE THIS KIT YOU NEED TO PURCHASE THE CORRECT 58-5012 KITFOR YOUR AIRCRAFT SERIAL NUMBER TO ENSURE YOU CAN GET YOUR AIRCRAFTCERTIFIED FOR FLIGHT IN KNOWN ICING CONDITIONS. IT WILL ADVISE WHAT YOU NEEDTO HAVE ON YOUR AIRCRAFT OR IF THERE IS A BEECH KIT THAT YOU CAN ADD TO YOURAIRCRAFT TO GET CERTIFIED FOR FLIGHT IN KNOWN ICING AS WELL AS FURNISH YOUTHE REQUIRED WARNING PLACARD FOR FLIGHT IN KNOWN ICING.

NOTENOTENOTENOTE:::: WHEN AIRPLANE IS EQUIPPED WITH A B-5 OR B-7 AUTOPILOT, KIT 55-4026 P OR 55-4026-1P RESPECTIVELY MUST BE INSTALLED DURING INSTALLATION OF THIS KIT.


58-4007-3 PDEICE SYSTEM, OUTBOARD WING, PNEUMATIC ATA :58 TH-1 AND AFTERD55, E55 TE-452 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PNEUMATIC SURFACE DEICER SYSTEM ONAIRPLANES WITH NO WET WINGS. BOOTS ARE NOT INCLUDED WITH KIT.

THIS KIT FURNISHES DETAILS FOR THE VERTICAL AND HORIZONTAL STABILIZER LESS THE DE-ICEBOOTS, JUST AS IT


NOTENOTENOTENOTE:::: BEFORE YOU PURCHASE THIS KIT YOU NEED TO PURCHASE THE CORRECT 58-5012 KITFOR YOUR AIRCRAFT SERIAL NUMBER TO ENSURE YOU CAN GET YOUR AIRCRAFTCERTIFIED FOR FLIGHT IN KNOWN ICING CONDITIONS. IT WILL ADVISE WHAT YOU NEEDTO HAVE ON YOUR AIRCRAFT OR IF THERE IS A BEECH KIT THAT YOU CAN ADD TO YOURAIRCRAFT TO GET IT CERTIFIED FOR FLIGHT IN KNOWN ICING AS WELL AS FURNISH YOUA REQUIRED WARNING PLACARD FOR FLIGHT IN KNOWN ICING.


58-4007-5 PDEICE SYSTEM, OUTBOARD WING, PNEUMATIC ATA :58 TH-1 AND AFTERTHIS KIT PROVIDES DETAILS FOR THE VERTICAL AND HORIZONTAL STABILIZER LESS THE DE-ICE BOOTS,JUST AS IT DOES FOR THE SURFACE DEICE OUTBOARD WING AREA LESS THE BOOTS.


NOTENOTENOTENOTE:::: NOTE }BEFORE YOU PURCHASE THIS KIT YOU NEED TO PURCHASE THE CORRECT58-5012 KIT FOR YOUR AIRCRAFT SERIAL NUMBER TO ENSURE YOU CAN GET YOURAIRCRAFT CERTIFIED FOR FLIGHT IN KNOWN ICING CONDITIONS. IT WILL ADVISE WHATYOU NEED TO HAVE ON YOUR AIRCRAFT OR IF THERE IS A BEECH KIT THAT YOU CANADD TO YOUR AIRCRAFT TO GET IT CERTIFIED FOR FLIGHT IN KNOWN ICING AS WELL ASFURNISH YOU A REQUIRED WARNING PLACARD FOR FLIGHT IN KNOWN ICING.



KIT CATALOG

58-4007-7 PDEICE SYSTEM, OUTBOARD WING, PNEUMATIC ATA :58 TH-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PNEUMATIC SURFACE DEICER SYSTEM ONAIRPLANES WITH WET WING TIPS AND EDGE LIT INSTRUMENTS. BOOTS ARE NOT INCLUDED WITH KIT.

THIS KIT PROVIDES DETAILS FOR THE VERTICAL AND HORIZONTAL STABILIZER LESS THENOTENOTENOTENOTE:::: WHEN THE AIRPLANE IS EQUIPPED WITH A B-5 OR B-7 AUTOPILOT, KIT 55-4026 OR

55-4026-1 P RESPECTIVELY MUST BE INSTALLED DURING INSTALLATION OF THIS KIT.NOTENOTENOTENOTE:::: BEFORE YOU PURCHASE THIS KIT YOU NEED TO PURCHASE THE CORRECT 58-5012 KIT

FOR YOUR AIRCRAFT SERIAL NUMBER TO ENSURE YOU CAN GET YOUR AIRCRAFTCERTIFIED FOR FLIGHT IN KNOWN ICING CONDITIONS. IT WILL ADVISE WHAT YOU NEEDTO HAVE ON YOUR AIRCRAFT OR IF THERE IS A BEECH KIT THAT YOU CAN ADD TO YOURAIRCRAFT TO GET IT CERTIFIED FOR FLIGHT IN KNOWN ICING AS WELL AS FURNISH YOUREQUIRED WARNING PLACARD FOR FLIGHT IN KNOWN ICING.


58-4007-9 PDEICE SYSTEM, INBOARD WING, PNEUMATIC ATA :58 TH-1 AND AFTERD55, E55 TE-452 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INBOARD PNEUMATIC SURFACE DEICESYSTEM. BOOTS ARE NOT INCLUDED WITH KIT. TYPE INSTRUMENTS DOES MATTER ON THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : 40 TO 60MEN : 1 (MAN)

58-4008-1 SSPAR FRONT CARRY-THRU REINFORCEMENT ATA :56TC TG-1 THRU TG-8395-55 TC-1 THRU TC-19095-A55 TC-191 THRU TC-1470, TC-1472 THRU

TC-152595-C55 TC-350, TE-1 THRU TE-49, TE-51 THRU

TE-45195-E55 TE-768 THRU TE-896A56TC TG-84 THRU TG-94"MANDATORY" SB NO. 2269THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ON THEFRONT FRAME, FORWARD SPAR CARRY THROUGH STRUCTURE ON INSERVICE AIRCRAFT. REPEAT -1SKIT TO REINFORCE FRONT FRAME, FORWARD SPAR CARRY-THRUS. (1 KIT WILL FIX BOTH LH AND

NOTENOTENOTENOTE:::: ALODINE 1200, EA9309NA OR EA9309 QT, EC2216A/B 2 OZ OR EC2216A/B QT OR EC2216,AND MIL-C-16173 REQUIRED BUT NOT FURNISHED WITH KIT, NEED TO BE ORDEREDSEPARATELY.

WT. CHANGE : WT: + 2.0 LBS ARM: 81.6" MOMENT + 163 IN.-LBSEST. MAN/HRS: : 48 TO 70MEN : 1 (MAN)


KIT CATALOG

58-4008-11 SFRONT SPAR CARRY-THRU STRUCTURE REINFORCEMENT ATA :58 TH-255, TH-304 AND AFTERB55 TC-1471, TC-1526 THRU TC-2456E55 TE-897 THRU TE-1201"MANDATORY" SB NO. 2269THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ON THEREAR FRAME, FORWARD SPAR CARRY-THRU STRUCTURE ON INSERVICE AIRCRAFT.

THIS KIT REINFORCES BOTH SIDES OF THE REAR FRAME OF FRONT SPAR CARRY-THRU STRUCTURE. IFYOU ALSO

NOTENOTENOTENOTE:::: ALODINE 1200, EA9309NA OR EA9309 QT, EC2216A/B 20Z OR EC2216A/B QT OR EC2216,AND MIL-C-16173 REQUIRED BUT NOT FURNISHED WITH KIT, NEED TO BE ORDEREDSEPARATELY.

WT. CHANGE : WT: + 2.0 LBS; ARM: 84.4 IN.; MOMENT: + 169 IN.-LBSEST. MAN/HRS: : 48 TO 70MEN : 1 (MAN)

58-4008-3 SFRONT SPAR CARRY-THRU REINFORCEMENT ATA :56TC TG-1 THRU TG-8395-55 TC-1 THRU TC-19095-A55 TC-191 THRU TC-349, TC-351 THRU TC-37095-B55 TC-371, TC-502 THRU TC-1470, TC-1472

THRU TC-152595-C55 TC-350, TE-1 THRU TE-49, TE-51 THRU

TE-45195-E55 TE-768 THRU TE-896A56TC TG-84 THRU TG-94"MANDATORY" SB NO. 2269THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ON THEREAR FRAME, FORWARD SPAR CARRY-THRU STRUCTURE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALODINE 1200, EA9309NA OR EA9309 QT, EC2216A/B 2 OR OR EC2216A/B QT OR EC2216,AND MIL-C-16173 REQUIRED BUT NOT FURNISHED WITH KIT NEED TO BE ORDEREDSEPARATELY.

NOTENOTENOTENOTE:::: -3 S KIT TO REINFORCE REAR FRAME OF FORWARD SPAR CARRY-THRU STRUCTURE. (1KIT WILL FIX CRACKS, BOTH LH AND RH SIDE OF REAR FRAME OF FORWARD SPARCARRY-THRU ASSEMBLY).

WT. CHANGE : WT: + 2.0 LBS; ARM: 84.4 INS.; MOMENT: + 69 IN.-LBSEST. MAN/HRS: : 48 TO 70MEN : N/A


KIT CATALOG

58-4008-5 SFRONT SPAR CARRY-THRU STRUCTURE REINFORCEMENT ATA :58 TH-1 THRU TH-254, TH-256 THRU TH-303"MANDATORY" SB NO. 2269THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ON THEFRONT FRAME, FORWARD SPAR CARRY-THRU STRUCTURE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALODINE 1200, EA9309NA OR EA9309 QT, EC2216A/B 2 OZ OR EC2216A/B QT OR EC2216AND MIL-C-16173 REQUIRED BUT NOT FURNISHED WITH KIT NEED TO BE ORDEREDSEPARATELY.


58-4008-7 SFRONT SPAR CARRY-THRU STRUCTURE REINFORCEMENT ATA :58 TH-1 THRU TH-254, TH-256 THRU TH-303"MANDATORY" SB NO. 2269THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ON THEREAR FRAME, FORWARD SPAR CARRY-THRU STRUCTURE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALODINE 1200, EA9309NA OR EA9309 QT, EC2216A/B 2 OZ OR EC2216A/B QT OR EC2216,AND MIL-C-16173 REQUIRED NOT FURNISHED WITH KIT NEED TO BE ORDEREDSEPARATELY.


58-4008-9 SFRONT SPAR CARRY-THRU STRUCTURE REINFORCEMENT ATA :58 TH-255, TH-304 AND AFTERB55 TC-1471, TC-1526 THRU TC-2456E55 TE-897 THRU TE-1201"MANDATORY" SB NO. 2269THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REINFORCEMENT PARTS ON THEFRONT FRAME, FORWARD SPAR CARRY-THRU STRUCTURE ON INSERVICE AIRCRAFT.

THIS KIT IS FOR REINFORCEMENT OF BOTH SIDES OF THE FRONT SPAR CARRY-THRU STRUCTUREREINFORCEMENT

NOTENOTENOTENOTE:::: ALODINE 1200, EA9309NA OR EA9309 QT, EC2216A/B 2 OZ OR EC2216A/B QT OR EC2216,AND MIL-C-16173 REQUIRED. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


58-4011-1LOCK ASSY INSTL, NOSE BAGGAGE DOOR ATA : 52WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

58-4013-0001HEATED WINDSHIELD INSTL ATA :D55, E55, 58 & 58TCTHIS KIT IS FOR THE SPARES REPLACEMENT FOR 102-364044-63 OR 102-364044-95 HEATED WINDSHIELDASSY ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "RTV108" SEALANT OR EQUIVALENT REQUIRED, BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


58-5002- SDOORS - PROVISIONS FOR FLIGHT WITH UTILITY DOORS REMOVED ATA : 5258, 58A TH-1 AND AFTERSI NO. 0387-107THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REMOVE BAGGAGE DOOR AND INSTALLAIR DEFLECTOR FOR AERIAL PHOTOGRAPHY UTILIZATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : 1 (MAN)

58-5005-1 PBEIGE HARNESSES FOR PILOT & CO-PILOT ATA : 2558 TH-233 THRU TH-732B55 TC-1454 THRU TC-1946E55 TE-861 THRU TE-1077SB NO. 2031, REV. 2 OR SUBSEQUENT

NOTENOTENOTENOTE:::: THIS KIT CAN BE USED ON LATER MODELS, BUT THEY SHOULD OF AND FACTORYINSTALLATION ON AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES,COMPLETE WITH INERTIA REELS, FOR THE PILOT AND COPILOT SEATS ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: FOR EARLIER B55 & 58 SEE 55-012-1 P AND -3P KITS.NOTENOTENOTENOTE:::: THIS KIT CAN BE USED ON LATER MODELS, BUT THEY SHOULD HAVE HAD FACTORY

INSTALLATION ON AIRCRAFT.NOTENOTENOTENOTE:::: FOR EARLIER B55 AND 58, SEE 55-5012-1 P AND -3 P KITS.

WT. CHANGE : B55 AND E55: WT: 3 LBS @ 97 ARM 58: WT: 3 LBS 1 @ 87 ARMEST. MAN/HRS: : 224MEN : 1 (MAN)


KIT CATALOG

58-5005-3 PSHOULDER HARNESS INSTALLATION (BEIGE ONLY) SEE PAGE 3-43 AND3-44

ATA :

58 TH-174 THRU TH-232B55 TC-1401 THRU TC-1453E55 TE-848 THRU TE-860THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES, COMPLETE WITHINERTIA REELS, FOR THE PILOT AND COPILOT SEATS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT ONLY COMES IN BEIGE, NO OTHER COLOR IS OFFERED. FOR LATER SERIALNUMBERS SEE 58-5005-1 P KIT AND FOR EARLIER SERIAL NUMBERS SEE 55-5012-1 P OR-3 P KITS.

WT. CHANGE : B55 AND E55: WT: 3 LBS@ 97 ARM 58: WT: 3 LBS @ 87 ARM

EST. MAN/HRS: : 26MEN : 1 (MAN)

58-5006-1 SSTATIC AIR VALVE, ALTERNATE ATA :58 TH-1 THRU TH-106B55 TC-371, TC-502 THRU TC-1372E55 TE-768 THRU TE-832SI NO. 0613-394 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING EMERGENCY STATIC AIRVALVE WITH A NEW VALVE WHICH SEPARATES THE EMERGENCY AND NORMAL STATIC SYSTEMS.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

58-5009-1 PHARNESS RESTRAINT, SHOULDER ATA : 2555, A55, B55 TC-1 THRU TC-349, C-351 THRU TC-194656TC, A56TC TG-2 THRU TG-9495, B95, D95A, E95 TD-2 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-1077SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES ON THE THIRD ANDFOURTH PASSENGER SEATS. BEIGE ONLYWT. CHANGE : WT: 2.6 LBS @ 145 ARMEST. MAN/HRS: : 12/SEATMEN : 1 (MAN)


KIT CATALOG

58-5009-11 PHARNESS RESTRAINT, SHOULDER ATA : 2558 TH-1 THRU TH-732SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SHOULDER HARNESS ON THE SIXTHPASSENGER SEAT. BEIGE ONLY

NOTENOTENOTENOTE:::: KIT 58-4003-1 P MUST BE INSTALLED PRIOR TO OR IN CONJUNCTION WITH THEINSTALLATION OF THIS KIT.

WT. CHANGE : WT: 1.8 LBS @ 172 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5009-3 PHARNESS RESTRAINT, SHOULDER ATA : 2558 TH-1 THRU TH-732SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESS ON THE THIRD ANDFOURTH PASSENGER SEATS. BEIGE ONLY.WT. CHANGE : WT: 2.6 LBS @ 145 ARMEST. MAN/HRS: : 12/SEATMEN : 1 (MAN)

58-5009-5 PHARNESS RESTRAINT, SHOULDER ATA : 2555, A55, B55 TC-1 THRU TC-349,

TC-351 THRU TC-194656TC, A56TC TG-2 THRU TG-94B95, B95A, E95 TD-453 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-1077SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SHOULDER HARNESS ON THE FIFTHPASSENGER SEAT. BEIGE ONLY.


WT. CHANGE : WT: 1.8 LBS @ 172 ARMEST. MAN/HRS: : 12MEN : 1 (MAN)


KIT CATALOG

58-5009-7 PHARNESS RESTRAINT, SHOULDER ATA : 2555, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-194656TC, A56TC TG-2 THRU TG-94B95, D95A, E95 TD-453 THRU D-721C55, D55, E55 TC-350, TE-1 THRU TE-1077SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SHOULDER HARNESS ON THE SIXTHPASSENGER SEAT. BEIGE ONLY



58-5009-9 PHARNESS RESTRAINT, SHOULDER ATA : 2558 TH-1 THRU TH-732SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SHOULDER HARNESS ON THE FIFTHPASSENGER SEAT. BEIGE ONLY



58-5010-1 SGROSS WEIGHT MODIFICATION ATA :58P TJ-2 AND AFTERTHIS KIT PROVIDES INFORMATION TO CONVERT MODEL 58P TO A 5995 LBS. GROSS WEIGHT TO BEREDESIGNATED AS MODEL 58PA.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

58-5011-3 SOXYGEN REGULATOR AND BOTTLE - SPARES ATA :58 TH-1 THRU TH-456, TH-473A56TC TG-84 THRU TG-94E55 TE-938, TE-943 THRU TE-975THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 66-CUBIC FOOT OXYGEN BOTTLE AND AREGULATOR AS A SPARES REPLACEMENT FOR THE 24555-9 REGULATOR AND 65- CUBIC FOOT BOTTLE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-5012-1 PICING FLIGHT REQUIREMENT LIST ATA :58 TH-94 THRU TH-1388, TH-1390 THRU

TH-1395THIS KIT CONTAINS INFORMATION, FLIGHT MANUAL AND PLACARD.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5012-3 PICING FLIGHT REQUIREMENT LIST ATA :58 TH-1389, TH-1396 THRU TH-1471, TH-1487

AND TH-1489THIS KIT CONTAINS INFORMATION, FLIGHT MANUAL AND PLACARD.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5012-5 PICING FLIGHT REQUIREMENT LIST ATA :58 TH-1389, TH-1396 THRU TH-1471, TH-1476,

TH-1487, TH-1489, TH-1498THIS KIT CONTAINS INFORMATION, FLIGHT MANUAL AND PLACARD.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5012-7 PICING FLIGHT REQUIREMENT LIST ATA :58 TH-1472 AND AFTER, EXCEPT TH-1476,

TH-1487, TH-1489, TH-1498THIS KIT PROVIDES A CHECKLIST OF ITEMS REQUIRED TO BE INSTALLED TO EQUIP THE AIRCRAFT FORFLIGHT IN ICING CONDITIONS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5012-9 PICING FLIGHT REQUIREMENT LIST ATA :58A TH-1472 AND AFTER, EXCEPT TH-1476,

TH-1487, TH-1489, TH-1498THIS KIT PROVIDES A CHECKLIST OF ITEMS REQUIRED TO BE INSTALLED TO EQUIP THE AIRCRAFT FORFLIGHT IN ICING CONDITIONS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-5013-1 PICING FLIGHT APPROVAL PLACARD INSTALLATION ATA :58 TH-1 AND AFTERD55, E55 TE-452 THRU TE-2083THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ICING FLIGHT APPROVAL PLACARD.

NOTENOTENOTENOTE:::: ALL EQUIPMENT LISTED ON KIT 58-5012 OR 55-5019 ICING FLIGHT REQUIREMENTS LISTMUST HAVE BEEN INSTALLED EITHER AS A FACTORY INSTALLATION OR AS ABEECHCRAFT KIT BEFORE ICING FLIGHT APPROVAL PLACARD CAN BE INSTALLED.


58-5013-3 PICING FLIGHT APPROVAL PLACARD INSTALLATION ATA :E55 TE-1084 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ICING FLIGHT APPROVAL PLACARD.

NOTENOTENOTENOTE:::: ALL EQUIPMENT LISTED ON KIT 58-5012 OR 55-5019 ICING FLIGHT REQUIREMENTS LISTMUST HAVE BEEN INSTALLED EITHER AS A FACTORY INSTALLATION OR AS ABEECHCRAFT KIT BEFORE ICING FLIGHT APPROVAL PLACARD CAN BE INSTALLED.


58-5014-1 SFIRESLEEVE INSTALLATION - INSTRUMENT AIR ATA :58P TJ-260 THRU TJ-39358TC TK-117 THRU TK-150SB NO. 2041, REV. 1 OR SUBSEQUENTTHIS KIT IS TO BE USED ON AIRCRAFT WHICH ARE NOT EQUIPPED WITH DEICE BOOTS.WT. CHANGE : N/AEST. MAN/HRS: : 3.5MEN : 1 (MAN)

58-5014-7 SFIRESLEEVE INSTALLATION - INSTRUMENT AIR ATA :58P, 58PA TJ-3 THRU TJ-25958TC, 58TCA TK-2 THRU TK-116SB NO. 2041, REV. 1 OR SUBSEQUENTTHIS KIT TO BE USED ON AIRCRAFT WHICH ARE EQUIPPED WITH DEICE BOOTS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-5016-1 SENGINE CONTROLS SUPPORT ANGLE BRACKETS ATA :58, 58A TH-1389, TH-1396 THRU TH-166258P, 58PA TJ-436, TJ-444 THRU TJ-47958TC, 58TCA TK-147 AND TK-151"MANDATORY" SB NO. 2439THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE ENGINE CONTROLS SUPPORT ANGLEATTACHMENT CLIPS WITH BRACKETS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5 TO 8MEN : 1 (MAN)

58-5019-1KIT"M"SPEC INTERIOR ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

58-8001-3 SLANDING GEAR SWITCH GUARD ATA :56TC TG-2 THRU TG-9458 TH-1 THRU TH-1337A55, B55 TC-191 THRU TC-2442C55, D55, E55 TC-350, TE-1 THRU TE-1198D95A, E95 TD-534 THRU TD-721MODE56TCL} TG-2 THRU TG-94}SI NO. 1215 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LANDING GEAR SWITCH GUARD.

NOTENOTENOTENOTE:::: THIS KIT IS NOT APPLICABLE FOR AIRPLANES EQUIPPED WITH AN OPTIONAL LANDINGGEAR SAFETY SYSTEM.


58-8003-1 STORQUE KNEE COMPONENTS, (MAIN LANDING GEAR) ATA :56TC, A56TC TG-2 THRU TG-9458P TJ-3 THRU TJ-49758TC TK-1 THRU TK-151"OPTIONAL" SB NO. 2147THIS KIT FURNISHES IMPROVED TORQUE KNEES FOR MAIN LH AND RH GEAR AND ATTACHINGHARDWARE REQUIRED FOR INSTALLATION. SEE SB NO. 2417 AND MAINTENANCE MANUALSSPECIFICATIONS TO DETERMINE IF ANY ADDITIONAL HARDWARE IS REQUIRED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

58-8003-3 STORQUE KNEE COMPONENTS, (NOSE LANDING GEAR) ATA :56TC, A56TC TG-2 THRU TG-9458P TJ-3 THRU TJ-49758TC TK-1 THRU TK-151SEE SB NO. 2147, REV. 1 BEFORE ORDERING TO CONFIRM SERIAL NUMBER EFFECTIVITY. RECOMMENDYOU REVIEW SB NO. 2147 TO CONFIRM YOU WILL NOT REQUIRE ADDITIONAL HARDWARE IF YOUR OLDHARDWARE CAN NOT BE REUSED BECAUSE IT DOES NOT MEET MAINTENANCE MANUAL SPECIFICATHIS KIT CONTAINS IMPROVED TORQUE KNEE COMPONENTS FOR THE NOSE LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-9002-1 PPROPELLER DEICE, 2-BLADE HARTZELL ATA :58 TH-1 THRU TH-209, TH-211 THRU TH-1388,

TH-1390 THRU TH-1395THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTROTHERMAL PROPELLER DEICERON AIRPLANES EQUIPPED WITH POST LIT INSTRUMENTS AND HARTZELL BHC-J2YF-2C/C8475-6 OR BHC-J2YF-2CF/FC8475-6 PROPELLERS. IF YOUR AIRCRAFT HAS POST LIGHTED INSTRUMENTS SEE K

NOTENOTENOTENOTE:::: POWER SUPPLY TO NEW BOOTS MUST BE 12 AMPS.WT. CHANGE : N/AEST. MAN/HRS: : 60 TO 80MEN : 1 (MAN)

58-9003-1 PPROPELLER DEICE, 3-BLADE HARTZELL ATA :58 AND 58A TH-1 THRU TH-1193 FOR AIRCRAFT WITH

POST LIGHTSTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTROTHERMAL PROPELLER DEICERON AIRPLANES EQUIPPED WITH POST LIT INSTRUMENTS AND HARTZELL PHC-C3YF-2C7663-2R AND PHC-C3YF-2UF/FC7663-2R PROPELLERS.WT. CHANGE : N/AEST. MAN/HRS: : 60 TO 80MEN : 1 (MAN)

58-9003-3 PPROPELLER DEICE, 3-BLADE HARTZELL ATA :58, 58A TH-1 THRU TH-1193 FOR AIRCRAFT WITH

WEDGE LIGHTSTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTROTHERMAL PROPELLER DEICERON AIRPLANES EQUIPPED WITH WEDGE LIT INSTRUMENTS AND HARTZELL PHC-C3YF-2C7663-2R ANDPHC-C3YF-2UF/FC7663-2R PROPELLERS.WT. CHANGE : N/AEST. MAN/HRS: : 60 TO 80MEN : 1 (MAN)


KIT CATALOG

58-9005-1 SEXHAUST CLAMP - SPARES ATA :58 TH-1336 THRU TH-1486B55 TC-2428, TC-2433 THRU TC-2456E55 TE-1199 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR TA0310005EXHAUST CLAMP. (ONE KIT PER ENGINE).WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-9006-1 SFUEL PUMP REFERENCE LINE CHANGE ATA :58 TH-1389, TH-1396 THRU TH-1531SB NO. 2268 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

58-9007-1 SENGINE MOUNT REINFORCEMENT ATA :58 TH-1 AND AFTER95C55 TC-350D55, E55 TE-1 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ENGINE MOUNT REINFORCEMENTS ON ONEENGINE MOUNT.WT. CHANGE : N/AEST. MAN/HRS: : 3 TO 8MEN : 1 (MAN)

58-9008-1 SENGINE MOUNT ASSEMBLY ATA :95-C55, D55, E55, 58THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REWORK PART NUMBER 96-910010-1, -57,-61 AND -67 ENGINE MOUNT ASSEMBLIES TO INCREASE CLEARANCE BETWEEN THE ENGINE MOUNTASSEMBLY AND THE ENGINE MOUNTED INSTRUMENT AIR/SURFACE DEICE AIR PUMP ON INSERVICEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

58-9010-0001HOOK INSTL, ENGINE CONTROL CABLE ATA :58/58A TH-1389, TH-1392 & AFTER UP TO THE

EFFECTIVITY OF ECR13912.THIS KIT PROVIDES PARTS & INFORMATION FOR THE INSTALLATION OF SUPPLEMENTAL PROPELLORCONTROL CABLE RETAINING HOOKS ON BOTH LEFT AND RIGHT ENGINES ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

58-9011-0001EXTENDED RANGE FUEL TANK IMPROVEMENT ATA :58 TH-766, & TH-773 & AFTER UP TO

ECR14356 WITH A USABLE 194 GALLONEXTENDED RANGE FUEL TANK.

THIS KIT PROVIDES INFORMATION AND PARTS TO REPLUMB THE SIPHON BREAK AND PRESSURE RELIEFTUBES ON THE RIGHT AND LEFT WING EXTENDED RANGE FUEL TANKS FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

60-9002-1 SFUEL CELL, LH BAFFLED - SPARES ATA :56TC, A56TC TG-2 THRU TG-9456TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-38458P TJ-3 THRU TJ-9058TC TK-1 THRU TK-23SI NO. 0585-281 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LH LEADING EDGE FUEL CELLS (58-380030-7OR -9) AND VELCRO PILE ON TOP AND BOTTOM FUEL TANK LINERS, ROOT RIB AND ON THE FRONT SPARON INSERVICE AIRCRAFT, WHEN BAFFLED FUEL CELLS ARE INSTALLED AS SPARES.

NOTENOTENOTENOTE:::: ON AIRPLANE SERIALS TG-2 THRU TG-4, THE FOLLOWING PARTS MUST BE ORDERED INADDITION TO THIS KIT: 60-369032 INSULATOR (TWO REQUIRED), MS1266-2N GROMMET(TWO REQUIRED), 60-921025 PLATE ASSEMBLY (ONE REQUIRED), MS20073-04-04 BOLT(SIX REQUIRED) AND AN960-416L WASHER (TWELVE REQUIRED).


60-9002-2 SFUEL CELL, RH BAFFLED - SPARES ATA :58 TH-1 THRU TH-38458P TJ-3 THRU TJ-9058TC TK-1 THRU TK-23SI NO. 0585-281 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL RH LEADING EDGE FUEL CELLS (58-380030-8OR -10) AND VELCRO PILE ON TOP AND BOTTOM FUEL TANK LINERS, ROOT RIB AND ON THE FRONTSPAR ON INSERVICE AIRCRAFT, WHEN BAFFLED FUEL CELLS ARE INSTALLED AS SPARES.

NOTENOTENOTENOTE:::: ON AIRPLANE SERIALS TG-2 THRU TG-4, THE FOLLOWING PARTS MUST BE ORDERED INADDITION TO THIS KIT: 60-369032 INSULATOR (TWO REQUIRED), MS21266-2N GROMMET(TWO REQUIRED), 60-921025 PLATE ASSEMBLY (ONE REQUIRED), MS20073-04-04 BOLT(SIX REQUIRED) AND AN960-416L WASHER (TWELVE REQUIRED).



KIT CATALOG

60-9005-1 SFUEL BOOST PUMP, REPLACEMENT ATA :56TC, A56TC TG-2 THRU TG-94SI NO. 0650-285, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FUEL BOOST PUMP.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

90-3072-1 SOVERVOLTAGE RELAY REPLACEMENT ATA :56TC, A56TC TG-3 THRU TG-86SI NO. 0645-355 AND NO. 0766-354, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES A RELAY AND INFORMATION TO REPLACE THE 138-5 ORIGINAL EQUIPMENT RELAYFOR IMPROVED OVERVOLTAGE PROTECTION OF THE GENERATOR SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

90-3085-1 SBRUSH BLOCK ASSEMBLY, MODULAR ATA :B55 TC-973 THRU TC-2172E55 TE-105 THRU TE-1199SI NO. 1075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE 4E1387-1AND -5 BRUSH BLOCK ASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : 1 (MAN)

90-3085-5 SBRUSH BLOCK ASSEMBLY, MODULAR ATA :58 TH-72 THRU TH-134958P TJ-3 THRU TJ-173, TJ-175 AND TJ-17658TC TK-1 THRU TK-86E55 TE-1074 THRU TE-1151SI NO. 1075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR 4E1350-5BRUSH BLOCK ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : 1 (MAN)


KIT CATALOG

90-3093-1 SIGNITION VIBRATOR - SPARES ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-165756TC, A56TC TG-2 THRU TG-9458 TH-1 THRU TH-436B95A, D95A, E95 TD-453 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-958, TE-960 THRU

TE-967THIS KIT PROVIDES PART AND INFORMATION TO INSTALL A HEATER IGNITION VIBRATOR AS A SPARESREPLACEMENT FOR THE 12C60 AND 12C60-1 VIBRATORS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3093-3 SIGNITION UNIT - SPARES ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-165756TC AND A56TC TG-2 THRU TG-9458 TH-1 THRU TH-436B95A, D95A, E95 TD-453 THRU TD-721C55, D55, E55 TC-350, TE-1 THRU TE-958, TE-960 THRU

TE-967THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATER IGNITION UNIT AS A SPARESREPLACEMENT FOR THE 11C30 IGNITION UNIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5058-1 SOUTFLOW AND SAFETY VALVE GASKET - SPARES ATA :58P TJ-3 THRU TJ-94THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED GASKET AT THE OUTFLOW ANDSAFETY VALVES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9056-3 SFUEL CELL, 13-GALLON LEADING EDGE ATA :56TC, A56TC TG-2 THRU TG-94THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH 13-GALLON LEADING EDGE FUEL CELL.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-9056-4 SFUEL CELL, 13-GALLON LEADING EDGE ATA :56TC, A56TC TG-2 THRU TG-94THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RH 13-GALLON LEADING EDGE FUEL CELL.WT. CHANGE : N/AEST. MAN/HRS: : 15MEN : 1 (MAN)

95-2001-1 SEXTERIOR PLACARD ATA :95, B95, D95A, E95 TD-2 THRU TD-721THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.

NOTENOTENOTENOTE:::: MS20995C32 LOCK WIRE WILL BE REQUIRED FOR USAGE WITH THIS KIT, BUT IS NOTFURNISHED WITH THE KIT. IF YOU DO NOT HAVE ANY IN YOUR STOCK IT CAN BEPROCURED LOCALLY IN A 1 LB. ROLL.


95-2002-1 SINTERIOR PLACARD ATA :95, B95, D95A AND E95 TD-2 THRU TD-721THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.

NOTENOTENOTENOTE:::: MS20995C32 SAFETY WIRE WILL BE REQUIRED FOR USAGE WITH THIS KIT, BUT IS NOTFURNISHED AS PART OF THE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY IN A 1 LB. ROLL.


95-3001-1 SBATTERY - SPARES ATA :55, A55, B55 TC-1 THRU TC-349, TC-351 THRU TC-245658 TH-1 THRU TH-1388, TH-1390 THRU TH-139558P TJ-3 THRU TJ-435, TJ-437 THRU TJ-44458TC TK-1 THRU TK-146, TK-148 THRU TK-15095, B95, D95A, E95 TD-2 THRU TD-721C55, D55 AND E55 TC-350, TE-1 THRU TE-1201THIS KIT PROVIDES PARTS AND INFORMATION FOR A SPARES REPLACEMENT FOR THE 118654 (24-VOLT)BATTERY. (ELECTROLYTE NOT FURNISHED WITH BATTERY)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 1 (MAN)


KIT CATALOG

95-4001- SFLAP RUBBER BUMPER, ADDITION ATA : 57THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLAP RUBBER BUMPER IN THE PLACE OFTHE RUBBER PADS IN THE FLAP TRACKS. THIS BUMPER REDUCES VIBRATION OF THE FLAP IN THE UPPOSITION.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 1 (MAN)

95-5002-1 PHARNESS INSTALLATION, SHOULDER ATA :D95A, E95 TD-638 THRU TD-721THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES FOR THE PILOT ANDCOPILOT SEATS. BEIGE ONLY.WT. CHANGE : WT: 2.37 LBS @ 112 ARMEST. MAN/HRS: : 26MEN : 1 (MAN)

95-5002-5 PHARNESS INSTALLATION, SHOULDER ATA :D95A, E95 TD-638 THRU TD-721THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SHOULDER HARNESSES FOR THE PILOT ANDCOPILOT SEATS. BLACK ONLY.WT. CHANGE : WT: 2.37 LBS @ 112 ARMEST. MAN/HRS: : 26MEN : 1 (MAN)

95-8100-0001ACTUATOR ASSY, SEAL REPLACEMENT ATA :50, 55THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE SEALANT OR GASKETS WITH NEW GASKETSIN THE 95-810017 LANDING GEAR ACTUATOR (ALL DASH NUMBERS), TO REDUCE LEAKS AND PROVIDEEASIER ASSEMBLY AT OVERHAUL ON IN-SERVICE AIRCRAFT.


95-9002-1 SANNUNCIATOR LIGHT, FUEL TANK SELECTOR ATA :95 TD-1 THRU TD-302B95 TD-303 THRU TD-452B95A TD-453 THRU TD-464"MANDATORY" SB NO. 2449THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ANNUNCIATOR LIGHT THATINDICATES THAT EITHER AUXILIARY FUEL TANK HAS BEEN SELECTED ON AIRCRAFT WITH AUXILIARYFUEL TANKS INSTALLED. SEE -3 S FOR LATER AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)


KIT CATALOG

95-9002-3 SANNUNCIATOR LIGHT, FUEL TANK SELECTOR ATA :B95A TD-465 THRU TD-533D95A TD-534 THRU TD-707E95 TD-708 THRU TD-721"MANDATORY" SB NO. 2449THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ANNUNCIATOR LIGHT THATINDICATES THAT EITHER AUXILIARY FUEL TANK HAS BEEN SELECTED ON AIRCRAFT WITH AUXILIARYFUEL TANKS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)

96-9001-1 SANNUNCIATOR LIGHT AUXILIARY FUEL TANK SELECTOR ATA :95-55, 95-A55, 95-B55, 95-B55A TC-1 THRU TC-160795-B55B TF-1 THRU TF-7095-C55, 95-C55A, D55, D55A, E55, E55A TE-1 THRU TE-942 EXCEPT TE-938"MANDATORY" SB NO. 2449THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ANNUNCIATOR LIGHT THAT INDICATESTHAT EITHER AUXILIARY FUEL TANK HAS BEEN SELECTED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberMARKER BEACON ANTENNA - SPARES - (100-3016-7 S) 1


YAW DAMPER SWITCH INSTALLATION - (101-3060-9 S) 1

EMERGENCY LOCATOR TRANSMITTER SWITCH GUARD - (101-3062-1 S) 1





BRAKE SHUTTLE VALVE - (101-8008-1 S) 2

NOISE SUPPRESSOR, FUEL BOOST PUMP FILTER INSTALLATION - (102-3006-1 S) 2

TELESCOPING TUBE, WING HINGE PIN INSTALLATION - (35-0588-1) 3

FUEL FILLER NECK RESTRICTER - (36-5013-1 S) 3


FUEL QUANTITY SYSTEM (LH) - (55-3021-3 S) 3

FUEL QUANTITY SYSTEM (RH) - (55-3021-4 S) 3

STARTER ENERGIZE LIGHT - (55-3022-1 S) 4

FUEL QUANTITY PRINTED CIRCUIT BOARD - (55-3023-5 S) 4

CONTROL WHEEL CLOCK INSTALLATION (28-VOLT) - (55-3028-3 P) 4

SPAR INSTALLATION - (58-4002-1 S) 4

FIRESLEEVE INSTALLATION, INSTRUMENT AIR - (58-5014-3 S) 4

TORQUE KNEE COMPONENTS, LANDING GEAR (MAIN GEAR) - (58-8003-1 S) 5

TORQUE KNEE DETAILS MAIN LANDING GEAR - (58-8003-5 S) 5



BATTERY LEAD ACID INSTALLATION - (60-3007-1 P) 5

BAGGAGE DOOR LATCH, SECONDARY - (60-4007-1 S) 6

RELIEF TUBE PASSENGER COMPARTMENT (AFT) - (60-5004-1 P) 6

SHOULDER HARNESS INSTALLATION, BEIGE - (60-5021-1 P) 6

AIR CONDITIONER COMPRESSOR CLUTCH GUARD - (60-5026-1 S) 6

AIR CONDITIONER COMPRESSOR CLUTCH AND CLUTCH GUARD - (60-5026-3 S) 7

FUEL CELL VELCRO TAPE INSTALLATION - (60-9002-1 S) 7

FUEL CELL, BAFFLED (RH) - (60-9002-2 S) 7

FUEL BOOST PUMP REPLACEMENT - (60-9005-1 S) 7

THROTTLE CONTROL CABLE - SPARES - (60-9009-1 S) 8

MIXTURE CONTROL CABLE - SPARES - (60-9009-3 S) 8

PROP GOVERNOR CONTROL CABLE - SPARES - (60-9009-5 S) 8




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberTURN AND BANK INDICATOR - SPARES - (90-5063-1 S) 8

MIC SELECT SWITCH INSTALLATION (PILOT AND COPILOT) - SPARES - (90-5072-3 S) 9

MIC SELECT SWITCH INSTALLATION (PILOT AND COPILOT) - SPARES - (90-5072-5) 9

FUEL CELL - 13-GALLON (LH) - (90-9056-3 S) 9

FUEL CELL - 13-GALLON (RH) - (90-9056-4 S) 9


KIT CATALOG

100-3016-7 SMARKER BEACON ANTENNA - SPARES ATA :60, A60, B60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A SPARE REPLACEMENTMARKER BEACON ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)

101-3039-1 SEMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH ATA :ALL MODELS WITH TR70-13 E.L.T.SI NO. 1139, REV. 1 OR SUBSEQUENTTHE KIT PROVIDES REMOTE SWITCHING FOR TR70-13 E.L.T. KIT DOES NOT INCLUDE E.L.T. AND BATTERYPACK.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 15MEN : 1 (MAN)

101-3060-9 SYAW DAMPER SWITCH INSTALLATION ATA :60, A60, B60THIS KIT CONSIST OF PARTS AND INFORMATION TO REPLACE 391222PDA8L41WIL SWITCH.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3062-1 SEMERGENCY LOCATOR TRANSMITTER SWITCH GUARD ATA :A60, B60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A SWITCH GUARD TORETAIN THE E.L.T. G SWITCH IN THE ARM POSITION WHEN CONNECTED TO THE REMOTE SWITCH ONAIRPLANES THAT ARE EQUIPPED WITH A TR70-13, (CIR-11) AND 101-3039-1 S REMOTE SWITCH INWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3170-1 SANTENNA MARKER BEACON INSTALLATION ATA :60, A60, B60THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION FOR SPARES REPLACEMENT OF101-384120 MARKER BEACON ANTENNA WITH A 101-384179 MARKER BEACON ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG




101-8008-1 SBRAKE SHUTTLE VALVE ATA :60, A60, B60SI NO. 1056 OR SUBSEQUENTTHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE BRAKE SHUTTLE VALVESWITH IMPROVED SHUTTLE VALVES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

102-3006-1 SNOISE SUPPRESSOR, FUEL BOOST PUMP FILTER INSTALLATION ATA :60, A60, B60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL AN IMPROVED EMI FILTERAT FUEL BOOST PUMP FOR REDUCTION OF RADIO NOISE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

35-0588-1TELESCOPING TUBE, WING HINGE PIN INSTALLATION ATA :60THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO AID WITH THE INSTALLATION OF THEHINGE PINS USED TO ATTACH THE WING L.E. TO THE FRONT SPAR TO THE BOX SECTION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 36MEN : 1 (MAN)

36-5013-1 SFUEL FILLER NECK RESTRICTER ATA :60 P-1 THRU P-596SB NO. 2045, REV. 3, OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO NON-LIGHTNING RESISTANT FUEL CAPSAND INSERTS. KIT ALSO PROVIDES KIT DRAWING AND ONE TOOL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

36-5027-1COVER ASSEMBLY, RH CONTROL WHEEL ATA :A60, B60THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 36-530171-23 COVER ASSEMBLY ONINSERVICE AIRCRAFT THAT PREVIOUSLY AHD 50-534846-11 PLATE INSTALLED ON THE RH CONTROLWHEEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

55-3021-3 SFUEL QUANTITY SYSTEM (LH) ATA :60, A60 P-4 THRU P-174, EXCEPT P-155, P-158,

P-163 THRU P-166THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE LH P.C. BOARD, INBOARD,OUTBOARD, AND NACELLE TRANSMITTERS ON INSERVICE AIRCRAFT. THE INBOARD AND OUTBOARDSIDE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

55-3021-4 SFUEL QUANTITY SYSTEM (RH) ATA :60, A60 P-4 THRU P-174, EXCEPT P-155, P-158,

P-163 THRU P-166THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE NACELLETRANSMITTERS AND THE LH AND RH P.C. BOARDS ON THE INBOARD AND OUTBOARD SIDE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

55-3022-1 SSTARTER ENERGIZE LIGHT ATA :60, A60, B60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A STARTER ENERGIZELIGHT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3023-5 SFUEL QUANTITY PRINTED CIRCUIT BOARD ATA :A60, B60 P-186 THRU P-575 OR EARLIER AIRPLANES

WITH 90-OHM TRANSMITTER INSTALLEDTHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL IMPROVED LH AND RH FUELQUANTITY P.C. BOARD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

55-3028-3 PCONTROL WHEEL CLOCK INSTALLATION (28-VOLT) ATA :60, A60, B60THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-3, 50-534622-13, 50-534622-17,50-534622-21, 50-384209-1, 50-384210-1 OR 50-384211-1 8-DAY CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

58-4002-1 SSPAR INSTALLATION ATA :60, A60REPLACE THE FORWARD OUTBOARD WING SPARS WITH NEW, COMMONALITY SPARS. KIT PROVIDESINSTALLATION INSTRUCTIONS AND NECESSARY PARTS. SPARS ARE NOT INCLUDED IN THIS KIT ANDMUST BE ORDERED SEPARATELY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-5014-3 SFIRESLEEVE INSTALLATION, INSTRUMENT AIR ATA :60 P-509 THRU P-594SB NO. 2041, REV. 1 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

58-8003-1 STORQUE KNEE COMPONENTS, LANDING GEAR (MAIN GEAR) ATA :60 P-4 THRU P-596THIS KIT CONTAINS IMPROVED TORQUE KNEE COMPONENTS FOR THE MAIN LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

58-8003-5 STORQUE KNEE DETAILS MAIN LANDING GEAR ATA :60, A60, B60 P-4 THRU P-596SB NO. 2147, REV. 1 OR SUBSEQUENTTHIS KIT ONLY PROVIDES 2 IMPROVED TORQUE KNEES, COPY OF SB NO. 2147 AND KIT DRAWING. IF YOUHAVE ANY ATTACHING HARDWARE THAT DOES NOT MEET MAINTENANCE MANUAL SPECIFICATIONS YOUWILL HAVE TO ORDER THOSE ITEMS SEPARATELY.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : 1 (MAN)

60-2003-1 SEXTERIOR PLACARD ATA :60, A60, B60 WITH BAFFLED FUEL CELLS ON BOTH

SIDESTHIS KIT INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED PRESSURE SENSITIVEEXTERIOR PLACARDS AND INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

60-2004-3 SINTERIOR PLACARD ATA :60, A60, B60 WITH BAFFLED FUEL CELLS ON BOTH

SIDESTHIS KIT INCLUDES A STANDARD REPLACEMENT SET OF EASILY INSTALLED PRESSURE SENSITIVEINTERIOR PLACARDS INSTRUCTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

60-3007-1 PBATTERY LEAD ACID INSTALLATION ATA :THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR INSTALLATION OF A LEAD ACIDBATTERY IN PLACE OF A NICKEL-CADMIUM TYPE. BATTERY IS NOT INCLUDED IN KIT.

NOTENOTENOTENOTE:::: WILL REQUIRE 2 EACH 58-380056-1 BATTERIES AS NOT FURNISHED AS PART OF KIT.NOTENOTENOTENOTE:::: 60-590000-9A5 P.O.H. REVISION HAS SUPPLEMENT ON LEAD ACID BATTERY FLIGHT

MANUAL CHANGES. IF REVISION -9A5 NO LONGER AVAILABLE, YOU WILL HAVE TOPURCHASE A NEW 60-590000-9 P.O.H.

WT. CHANGE : CALCULATED AFTER INSTALLATIONEST. MAN/HRS: : 40MEN : 1 (MAN)


KIT CATALOG

60-4007-1 SBAGGAGE DOOR LATCH, SECONDARY ATA :60, A60, B60 P-4 THRU P-569SI NO. 1169 OR SUBSEQUENTA SECONDARY LATCH IS ADDED TO NOSE BAGGAGE DOOR.WT. CHANGE : WT: + 2 LBS @157 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

60-5004-1 PRELIEF TUBE PASSENGER COMPARTMENT (AFT) ATA :60, A60, B60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A RELIEF TUBE FOR THE AFTPASSENGERS. RELIEF TUBES ARE NECESSARY EQUIPMENT ON FLIGHTS ON LONG DURATION.

NOTENOTENOTENOTE:::: MC0C57117-3 TUBE IS REQUIRED FOR INSTALLATION OF THIS KIT BUT IS NOTFURNISHED AS PART OF THIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


60-5021-1 PSHOULDER HARNESS INSTALLATION, BEIGE ATA : 2560, A60 B60 P-4 THRU P-388SB NO. 2031, REV. 2 OR SUBSEQUENTADD AN EXTRA MARGIN OF SAFETY WITH COMFORTABLE SHOULDER HARNESS, COMPLETE WITHINERTIAL REEL. INCLUDES PARTS AND INFORMATION TO INSTALL NEW SEAT BELTS AND SHOULDERHARNESSES FOR BOTH PILOT AND COPILOT SEATS.WT. CHANGE : WT: + 1.72 LBS; ARM: 132.6; MOMENT: + 228.0 IN.-LBSEST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)

60-5026-1 SAIR CONDITIONER COMPRESSOR CLUTCH GUARD ATA :60 THRU B60 P-4 THRU P-592, EXCEPT P-578, P-588 WITH

AIR CONDITIONERSI NO. 1236 OR SUBSEQUENTTHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A CLUTCH GUARD OVERTHE AIR CONDITIONER COMPRESSOR CLUTCH TO PROTECT SURROUNDING EQUIPMENT.WT. CHANGE : WT: 30 LBS @ 134.0 ARM; 4020 MOMENT @ 134.0 ARM; 4020 MOMENTEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

60-5026-3 SAIR CONDITIONER COMPRESSOR CLUTCH AND CLUTCH GUARD ATA :60 THRU B60 P-4 THRU P-592, EXCEPT P-578, P-588 WITH

AIR CONDITIONERSI NO. 1236 OR SUBSEQUENTTHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A NEW CLUTCH ONAIRPLANES WITH OLD STYLE CLUTCH WITHOUT RECESSED AREA FOR LOCK WASHER. INCLUDES ACLUTCH GUARD OVER THE NEW CLUTCH TO PROTECT SURROUNDING EQUIPMENT.WT. CHANGE : WT: +1 LB. @ +142 ARMEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

60-9002-1 SFUEL CELL VELCRO TAPE INSTALLATION ATA :60, A60 P-4 THRU P-195SI NO. 0585-281 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LEADING EDGE FUEL CELLS AND VELCROPILE ON TOP AND BOTTOM FUEL TANK LINERS, ROOT RIB AND ON THE FRONT SPAR ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

60-9002-2 SFUEL CELL, BAFFLED (RH) ATA :60, A60 P-4 THRU P-195SI NO. 0585-281 OR SUBSEQUENTTHIS KIT INCLUDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE INBOARD LEADINGEDGE FUEL CELLS WITH NEW, BAFFLED CELLS. KIT IS REQUIRED WHEN MAKING INITIAL REPLACEMENTOF ORIGINAL FUEL CELLS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5MEN : 1 (MAN)

60-9005-1 SFUEL BOOST PUMP REPLACEMENT ATA :60, A60, B60 P-4 THRU P-280SI NO. 0650-285, REV. 1 OR SUBSEQUENTASSURE CORRECT POSITIONING OF THE NEW REPLACEMENT FUEL BOOST PUMPS WITHOUT LOCATORPINS. PRESSURE SENSITIVE PLACARDS INSTALLS QUICKLY ON THE BOOST PUMP MOUNTING BRACKETTO ASSIST IN CORRECT ALIGNMENT.WT. CHANGE : WT: + 1 LB. @ +237 ARMEST. MAN/HRS: : 2 TO 4 HRSMEN : 1 (MAN)


KIT CATALOG

60-9009-1 STHROTTLE CONTROL CABLE - SPARES ATA :60, A60, B60 P-2 THRU P-436, EXCEPT P-406, P-409THIS KIT PROVIDES REPLACEMENT FOR P/N 41539-1 AND 41539-2 CONTROL CABLES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

60-9009-3 SMIXTURE CONTROL CABLE - SPARES ATA :60, A60, B60 P-2 THRU P-436, EXCEPT P-406, P-409THIS KIT PROVIDES REPLACEMENT FOR P/N 50-389010-25 CONTROL CABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

60-9009-5 SPROP GOVERNOR CONTROL CABLE - SPARES ATA :60, A60, B60 P-2 THRU P-436, EXCEPT P-406, P-409THIS KIT PROVIDES REPLACEMENT FOR 40851-63 AND -65 CONTROL CABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3072-1 SOVERVOLTAGE RELAY REPLACEMENT ATA :SI NO. 0766-354, REV. 2 AND SI NO. 0645-355 OR SUBSEQUENTIMPROVE THE OVERVOLTAGE PROTECTION OF THE GENERATOR SYSTEM BY INSTALLATION OF A NEW,IMPROVED OVERVOLTAGE RELAY. KIT IS REQUIRED FOR INITIAL REPLACEMENT OF ORIGINAL RELAYS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

90-5063-1 STURN AND BANK INDICATOR - SPARES ATA :A60, B60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A SPARE REPLACEMENTTURN AND BANK INDICATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-5072-3 SMIC SELECT SWITCH INSTALLATION (PILOT AND COPILOT) - SPARES ATA :60, A60, B60, H90THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE PILOT AND COPILOT MICSELECT SWITCH ASSEMBLY P/N: PA037-258 (1K POT) WITH RV6NAYSL102A POT WITH P/N: 54D30-03-AJN,ADD RV6NAYSL102A POT TO SWITCH (1K POT) SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: -3 S KIT FOR AIRCRAFT WITH MASTER VOL POT (1K POT). NEED TO CONTACT PRODUCTSUPPORT FOR CONFIRMATION OF SYSTEM ON YOUR AIRCRAFT.

NOTENOTENOTENOTE:::: MUST HAVE AVIONICS WIRING DIAGRAMS FOR YOUR AIRPLANE TO INSTALL THIS KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


90-5072-5MIC SELECT SWITCH INSTALLATION (PILOT AND COPILOT) - SPARES ATA :60, A60, B60THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE PILOT AND COPILOT MICSELECT SWITCH ASSEMBLY P/N: PA037-179IDI WITH RV6NAY5L103C POT WITH 54D30-03-2-AJN, ADDRV6NAY5L103C POT TO SWITCH (10K POT) SYSTEM ON INSERVICE AIRCRAFT.


NOTENOTENOTENOTE:::: -5 KIT FOR AIRCRAFT WITH MASTER VOL POT (10 POT). NEED TO CONTACT PRODUCTSUPPORT FOR CONFIRMATION OF SYSTEM ON YOUR AIRCRAFT.


90-9056-3 SFUEL CELL - 13-GALLON (LH) ATA :56TC, A56TCPER CO F52474 THIS KIT COVERS REPLACEMENT OF CELLS ON IN-SERVICE AIRCRAFT. THIS IS AREPLACEMENT KIT ONLY, IT IS NOT USED FOR NEW INSTALLATIONS.

NOTENOTENOTENOTE:::: THESE FUEL CELLS 002-920013-1, -2, -3, -4 ARE NOT COMPATIBLE WITH AIRCRAFT WITHWET WING TIPS.


90-9056-4 SFUEL CELL - 13-GALLON (RH) ATA :60, A60THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE 13-GALLON LEADINGEDGE FUEL CELLS.WT. CHANGE : N/A (INSTALLATION AID)EST. MAN/HRS: : 2MEN : 1 (MAN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberBATTERY CHARGE CURRENT SENSOR - (100-3009-1 S) 1





FUEL QUANTITY INDICATOR REPLACEMENT - (101-3169-3 S) 2




STRESS FREE WINDSHIELD INSTALLATION - (101-5041-1 S) 3


INSTAL OF STRESS FREE WINDSHIELD - (101-5041-3 S) 3

CARPET FASTENERS - SPARES - (101-5081-1 S) 4

LANDING GEAR BUSHING, NOSE - (101-8017-1 S) 4

ALUMINUM NOSE LANDING GEAR KIT - (101-8021-1 P) 4

ALUMINUM NOSE LANDING GEAR KIT - (101-8021-5 P) 5

NOSE LANDING GEAR WHEEL INSTALLATION - (101-8027-3 P) 5

NOSE LANDING GEAR WHEEL INSTALLATION - (101-8027-5 P) 5

NOSE LANDING GEAR PISTON ASSEMBLY REPLACEMENT - (101-8030-1 S) 5







BSP INTERIOR PLACARD - (50-1002- BSP) 7

EXHAUST STACK CLAMP IMPROVEMENT - (50-134- S) 7

NACELLE LH FUEL CELL REPLACEMENT - (50-9004-1 S) 7

NACELLE RH FUEL CELL REPLACEMENT - (50-9004-3 S) 8

CLOCK INSTALLATION CONTROL, WHEEL (28-VOLT) - (55-3028-3 P) 8


FLASHER INSTALLATION - (55-3030-1 S) 8

TORQUE KNEE, MAIN LANDING GEAR - (58-8003-5 S) 8

FIRE SHIELD, NACELLE INTERIOR - (65-9008-1 S) 9

INTERIOR AND EXTERIOR, (USABLE AND MINIMUM FUEL) PLACARD - (80-2001-33 S) 9





Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberEXTERIOR PLACARD - (80-2002-5 S) 10



INTERCONNECTED FUEL SYSTEM PLACARD - (80-2004-1 S) 10

FUEL SYSTEM BOOST PUMP - SPARES - (80-9009-3 S) 10

RELAY REPLACEMENT, OVERVOLTAGE - (90-3072-1 S) 11

BAGGAGE DOOR, NOSE SECONDARY LATCH INSTALLATION - (90-4076-1 S) 11

RUDDER PEDAL ARM ASSEMBLY - SPARES - (90-4085-1 S) 11




SHOULDER HARNESS INSTALLATION, PILOT AND COPILOT - (90-5034-1 P) 12

LANDING GEAR GREASE PROVISIONS, NOSE - (90-8002-1 S) 12


KIT CATALOG

100-3009-1 SBATTERY CHARGE CURRENT SENSOR ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-458, LD-460 THRU LD-47188 LP-1 THRU LP-47SI NO. 0587-356 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BATTERY CHARGE CURRENT DETECTINGDEVICE TO MONITOR THE CONDITION OF THE NICKEL-CADMIUM BATTERY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

100-4002-1 SSPAR INSTALLATION, OUTBOARD WING FORWARD ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-47588 LP-1 THRU LP-47THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN OUTBOARD WING FORWARD SPAR. (SPARIS NOT INCLUDED IN THIS KIT.)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

100-4002-3 SSPAR INSTALLATION, OUTBOARD WING FORWARD ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-47588 LP-1 THRU LP-47THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH OUTBOARD WING FORWARD SPAR.(SPAR IS INCLUDED IN THIS KIT)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

100-4002-4 SSPAR INSTALLATION, OUTBOARD WING FORWARD ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-47588 LP-1 THRU LP-47THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RH OUTBOARD WING FORWARD SPAR.(SPAR IS INCLUDED IN THIS KIT.)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)


KIT CATALOG

101-3039-1 SEMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH ATA :65B80 LD-450 THRU LD-511SI NO. 1139, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A REMOTE SWITCH FOR THETR70-13 E.L.T.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

101-3169-3 SFUEL QUANTITY INDICATOR REPLACEMENT ATA :A90-1 LM-101, LM-107, LM-115, LM-125

LM-127 THRU LM-129, LM-132, LM-133LM-136 THRU LM-138

A90-4 (RU-21H) LU-2, LU-5, LU-6, LU-9 THRU LU-13 ANDLU-15

THIS KIT WILL PROVIDE PARTS AND INFORMATION NECESSARY TO REPLACE THE 91-380028-13 FUELQUANTITY INDICATOR WITH A REPLACEMENT INDICATOR.

NOTENOTENOTENOTE:::: FOR RC-12H AIRCRAFT WITH 100-384189-3 INDICATOR SEE KIT 101-3169-1 S.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

101-3227-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : 0 (MEN)

101-3227-3ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. ALSO VIDEO IN PAL FORMAT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : 0 (MEN)

101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES FOR PROPER ELECTRICAL BONDING TO METALS ON ALL NON-COMPOSITEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : 0 (MEN)


KIT CATALOG

101-5041-1 SSTRESS FREE WINDSHIELD INSTALLATION ATA :QUEEN AIR 65-88THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON INSERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR BOTH WINDSHIELDS.

NOTENOTENOTENOTE:::: THIS IS THE NEW AIRCRAFT APPLICABILITY FOR THIS KIT.NOTENOTENOTENOTE:::: PR1440B1/2 6 OZ K SEALER (6 EACH PER KIT), EC1300L 1/2 PT, AND A400 ADHESIVE (2

EACH PER KIT) REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY, OR THRU RAPID.


101-5041-3 SSTRESS FREE WINDSHIELD INSTALLATION ATA :QUEEN AIR 65-88THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON INSERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR ONE WINDSHIELD.

NOTENOTENOTENOTE:::: HAZMAT REMOVED FROM KIT, MUST ORDER SEPARATELY.1 EA SILPAK A400, 1 EA EC1300L QT, & 3 EA PR1440B1/2 6OZ KPER KIT (DO NOT ORDER 101-5044-1 S)

NOTENOTENOTENOTE:::: THIS IS THE NEW AIRCRAFT APPLICABILITY FOR THIS KIT.NOTENOTENOTENOTE:::: PR1440B1/2 6 OZ K SEALER (6 EACH PER KIT), EC1300L 1/2 PT, AND A400 ADHESIVE (2


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8 HRSMEN : 1 (MAN)

101-5041-3 SINSTAL OF STRESS FREE WINDSHIELD ATA :65-88THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON IN SERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR ONE WINDSHIELD, BUT NOWINDSHIELD. PROCURE LOCALLY.

NOTENOTENOTENOTE:::: "PR1440B1/2 6OZ K"SEALER(3 EA PER KIT)"EC1300L 1/2 PT"&"A400"ADHESIVE(1 EA PERKIT) REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE LOCALLY OR THROUGHRAPID.


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8 HRSMEN : N/A


KIT CATALOG

101-5081-1 SCARPET FASTENERS - SPARES ATA :A65, 70, B80, A90-1(U-21A), A90-1(RU21N),A90-4(RU21N)THIS KIT PROVIDES A SPARES REPLACEMENT FOR SJ3283 HEDLOCK FASTENERS USED ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: ADHESIVE "EC847 QT" WILL BE REQUIRED FOR USE WITH THIS KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES 25 PAIRS OF CARPET FASTENERS (50 PARTS, 25 FOR ATTACHMENTTO CARPET BACKING AND 25 FOR ATTACHMENT TO THE FLOORPANEL.) YOU NEED TOCHANGE ALL YOUR SJ3283 FASTENERS TO THE REPLACEMENT FASTENERS AT THESAME TIME FOR OVERALL INTEGRITY OF THE SYSTEM.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5 TO 2.5MEN : 1 (MAN)

101-8017-1 SLANDING GEAR BUSHING, NOSE ATA :70 LB-1 THRU LB-3588 LP-1 THRU LP-47A65 LC-240 THRU LC-335A80 AND B80 LD-151 THRU LD-466THIS KIT PROVIDES PARTS AND INFORMATION TO REWORK THE NOSE LANDING GEAR BRACE.

NOTENOTENOTENOTE:::: THIS KIT CANNOT BE INSTALLED IF KIT 90-8002-1 S HAS BEEN PREVIOUSLY INSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

101-8021-1 PALUMINUM NOSE LANDING GEAR KIT ATA : 32A65, 70, A80, B80, 88KING AIR: 200/300 COMMUNIQUE NO. 47THIS KIT CONSIST OF BRACE ASSEMBLY, BOLTS, NUTS, BUSHINGS, COTTER PINS, LUBE FITTING, 3INSTRUCTION PLATES (SUCH AS: TOW LIMITS) AND KIT DRAWING.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENTFOR 50-820204-41 BRACE ASSEMBLY ON IN-SERVICE AIRCRAFT.

WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)


KIT CATALOG

101-8021-5 P ALUMINUM NOSE LANDING GEAR KIT ATA : 32A65, 70, A80, B80, 88, A90-1, A90-2, A90-3AND A90-4KING AIR: 200/300 COMMUNIQUE NO. 47THIS KIT PROVIDED PARTS AND INFORMATION FOR A REPLACEMENT FOR 50-820196-651, 97-820000-652AND -671 NOSE GEAR ASSEMBLY ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR 99 AIRLINERS WITH 50-820196-671 GEAR, SEE 101-8021-7 P KIT.NOTENOTENOTENOTE:::: THIS KIT DOES NOT PROVIDE A NOSE GEAR WITH A WHEEL AND TIRE ASSEMBLY, IF YOU

DESIRE THOSE ALSO, YOU WILL NEED TO ORDER THE P/N CALLED OUT IN YOUR I.P.C.OR SEE 101-8027 KITS IN KIT CATALOG.

WT. CHANGE : WT: + 16 LBS; MOMENT: - 52 IN.-LBSEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

101-8027-3 PNOSE LANDING GEAR WHEEL INSTALLATION ATA :A65, 70, B80, 88THIS KIT IS THE SPARES REPLACEMENT FOR 101-8015-11, 50-300011-43, 50-300011-29 OR 50-300011-1 TIREAND WHEEL ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

101-8027-5 PNOSE LANDING GEAR WHEEL INSTALLATION ATA :70, B80, 88THIS KIT IS THE SPARES REPLACEMENT FOR 101-8015-3, 50-300011-41, 50-300011-23 OR 50-300011-19WHEEL ASSEMBLYWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

101-8030-1 SNOSE LANDING GEAR PISTON ASSEMBLY REPLACEMENT ATA :88, B80, A80, 70, A65THIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT FOR 101-820072-1,101-820025-5, 101-820025-3, 101-820025-1, 115-820066-3, 115-820066, 50-820197-11, 50-820197-9, 50-820197-7,50-820197-5, 50-820197-3 AND 50-820197-1 NOSE LANDING GEAR LOWER SWT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

33-5007-1 SGYRO, DIRECTIONAL - SPARES ATA : 3165, 65-80THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE DIRECTIONAL GYRO P/N 35-380039-1 OR50-380007-7 ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

33-5007-3 SGYRO, HORIZON - SPARES ATA :65, 65-80THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE HORIZON GYRO P/N 35-380043-1 OR50-380008-7 ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

35-5048-1 SFUEL FILLER NECK RESTRICTOR ATA :65 LC-1 THRU LC-10280 LD-1 THRU LD-15088 LP-1 THRU LP-47"OPTIONAL" SB NO. 2045, REV. 3(FOR OTHER MODELS SEE "OPTIONAL" SB NO. 2045, REV. III)

NOTENOTENOTENOTE:::: THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO MODIFY THE FUELFILLER NECK AND REPLACED THE FUEL FILLER CAPS TO REDUCE THE POSSIBILITY OFFUELING THESE AIRCRAFT WITH JET FUEL.


35-8010-7 SMAIN LANDING GEAR WHEEL BEARING REPLACEMENT ATA :65, 70, 80, 88THIS KIT CONSISTS OF PARTS AND INFORMATION TO BE USED WITH WHEEL ASSEMBLIES 50-300013-79OR -85 AND WHEEL HALF-INBOARD 50-300013-81 OR -87 THAT ARE EQUIPPED WITH 13600LA902A1 CONEAND SEAL AND 13621 CUP.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

36-5013-1 SFUEL FILLER NECK RESTRICTOR ATA :65 LC-103 THRU LC-33580 LD-151 THRU LD-511SB NO. 2045, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NON-LIGHTNING RESISTANT FUEL CAPS ANDINSERTS. KIT CONSISTS OF 2 CAPS AND INSERTS, 1 TOOL AND KIT DRAWING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.5MEN : 1 (MAN)


KIT CATALOG

36-5027-1COVER ASSEMBLY, RH CONTROL WHEEL ATA :65, B80THIS KIT PROVIDES PARTS AND INVORMATION TO INSTALL 36-530171-23 COVER ASSEMBLY ONINSERVICE AIRCRAFT THAT PREVIOUSLY AHD 50-534846-11 PLATE INSTALLED ON THE RH CONTROLWHEEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : 0 (MEN)

50-1002- BSPBSP INTERIOR PLACARD ATA :WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

50-134- SEXHAUST STACK CLAMP IMPROVEMENT ATA :65 AND A65 L-1, L-2, L-6, L-7, LF-8, LC-1 THRU LC-33580 AND A80 LD-1 THRU LD-130THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED EXHAUST CLAMPS TO PROVIDEIMPROVED SUPPORT.

NOTENOTENOTENOTE:::: THIS KIT CONSISTS OF 1 SET OF CLAMPS AND ATTACHING HARDWARE FOR ONE SET OFSTACKS, TAKES 2 KITS PER ENGINE OR 4 KITS PER AIRCRAFT.


50-9004-1 SNACELLE LH FUEL CELL REPLACEMENT ATA :65-A90-1 (U-21A AND U-21G)65-A90-4 (U-21E)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT LH NON SELF SEALINGNACELLE FUEL CELL ASSEMBLY AS SPARES FOR A 50-380135-1 LH SELF SEALING FUEL CELL ASSEMBLYON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PER BASI, FASTENERS OR CELL HANGERS ARE P/N: 18-120012 PER BASI COPY OF BS440.KIT DOES NOT INCLUDE 13 FASTENERS OR HANGERS THAT INSTALLATION INSTRUCTION3A ADVISES ARE REQUIRED TO HANG NEW CELL. YOU WILL NEED TO ORDER THESEPARTS SEPARATELY, IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.

WT. CHANGE : TO BE DETERMINED BY FORMULA SHOWN ON KIT DRAWING.EST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)


KIT CATALOG

50-9004-3 SNACELLE RH FUEL CELL REPLACEMENT ATA :65-A90-1 (U-21A AND U-21G)65-A90-4 (RU-21E)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT RH NON SELF SEALINGNACELLE FUEL CELL ASSEMBLY AS SPARES FOR A 50-380135-2 RH SELF-SEALING FUEL CELL ASSEMBLYON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PER RASI, FASTENERS OR CELL HANGERS ARE P/N: 18-120012 PER RASI COPY OF BS440.KIT DOES NOT INCLUDE 13 FASTENERS OR HANGERS THAT INSTALLATION INSTRUCTION3A ON KIT DRAWING ADVISES ARE REQUIRED TO HANG NEW CELL. YOU WILL NEED TOORDER THESE PARTS SEPARATELY, IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU MAYPROCURE LOCALLY.

WT. CHANGE : TO BE DETERMINED BY FORMULA SHOWN ON KIT DRAWINGEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

55-3028-3 PCLOCK INSTALLATION CONTROL, WHEEL (28-VOLT) ATA :60, A60, B60, 65B-80, 65-88, 65A-88THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-3, 50-534622-13, 50-534622-17,50-534622-21, 50-384209-1, 50-384210-1 OR 50-384211-1 8-DAY CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

55-3029-3 PCLOCK INSTALLATION, INSTRUMENT PANEL, (28-VOLT) - SPARES ATA :A65, 70, B80THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 50-380013-5 AND 58-380015-3 8-DAY CLOCKS OR58-380077-3 AND 58-380077-7 ELECTRIC CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

55-3030-1 SFLASHER INSTALLATION ATA :65, A65, 70, 80THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE 624 FLASHER WITH 76259-1.WT. CHANGE : N/AEST. MAN/HRS: : 1MEN : 1 (MAN)

58-8003-5 STORQUE KNEE, MAIN LANDING GEAR ATA :60, A60, B60 P-4 THRU P-596SB NO. 2147 OR SUBSEQUENTKIT CONSIST OF PARTS AND INFORMATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5MEN : 1 (MAN)


KIT CATALOG

65-9008-1 SFIRE SHIELD, NACELLE INTERIOR ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-47588 LP-1 THRU LP-47E50 THRU J50 ALL SERIALSSI NO. 0630-065 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FIRE SHIELD IN BOTH ENGINE NACELLES.WT. CHANGE : WT: 50: 11.5 LBS @105 ARM

OTHERS: WT: 11.5 LBS @140 ARMEST. MAN/HRS: : 20MEN : 1 (MAN)

80-2001-33 SINTERIOR AND EXTERIOR, (USABLE AND MINIMUM FUEL) PLACARD ATA :B80 LD-280 THRU LD-467SI NO. 0539-281, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT SET OF PRESSURESENSITIVE DECALS TO REFLECT A CHANGE IN UNUSABLE FUEL AND TO DENOTE THE NEW MINIMUMFUEL FOR TAKEOFF REQUIREMENT.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

80-2002-1 SEXTERIOR PLACARD ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80 LD-1 THRU LD-269THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

80-2002-3 SEXTERIOR PLACARD ATA :B80 LD-270 THRU LD-279THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)


KIT CATALOG

80-2002-5 SEXTERIOR PLACARD ATA :B80 LD-280 THRU LD-511THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

80-2003-1 SINTERIOR PLACARD ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80 LD-1 THRU LD-269THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

80-2003-3 SINTERIOR PLACARD ATA :B80 LD-270 THRU LD-511THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

80-2004-1 SINTERCONNECTED FUEL SYSTEM PLACARD ATA :65, A65 LC-230 THRU LC-33570 LB-1 THRU LB-3588 LP-28THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE CORRECT PLACARDS ON AIRPLANESEQUIPPED WITH INTERCONNECTED FUEL SYSTEMS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

80-9009-3 SFUEL SYSTEM BOOST PUMP - SPARES ATA :B80 LD-280 THRU LD-511THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE50-389041-3, -5 OR -7 FUEL BOOST PUMP.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

90-3072-1 SRELAY REPLACEMENT, OVERVOLTAGE ATA :65, A65 LC-165 THRU LC-33570 LB-1 THRU LB-3588 LP-1 THRU LP-47A80, B80 LD-227 THRU LD-499SI NO. 0637-354, 0645-355, 0766-354 AND 0779-358 OR SUBSEQUENTTHIS KIT PROVIDES A RELAY AND INFORMATION TO REPLACE THE 138-5 ORIGINAL EQUIPMENT RELAYFOR IMPROVED OVERVOLTAGE PROTECTION OF THE GENERATOR SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

90-4076-1 SBAGGAGE DOOR, NOSE SECONDARY LATCH INSTALLATION ATA :65 AND A65 LC-172 THRU LC-217, LC-230 THRU LC-33570 LB-1 THRU LB-29A80, B80 LD-152 THRU LD-257, LD-278 THRU LD-436THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SECONDARY LATCH ON HINGED NOSEBAGGAGE DOORS.

NOTENOTENOTENOTE:::: SERVICE INSTRUCTION NO. 0485-351 REV. I. OR SUBSEQUENT, MUST BE COMPLIED WITHPRIOR TO OR IN CONJUNCTION WITH INSTALLATION OF THIS KIT.

WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

90-4085-1 SRUDDER PEDAL ARM ASSEMBLY - SPARES ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-47588 LP-1 THRU LP-47THIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 50-524326-1 OR -11 LH RUDDER PEDAL ARMASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)

90-4085-2 SRUDDER PEDAL ARM ASSEMBLY - SPARES ATA :65, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33570 LB-1 THRU LB-3580, A80, B80 LD-1 THRU LD-47588 LP-1 THRU LP-47THIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 50-524326-2 OR -12 RH RUDDER PEDAL ARMASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 0 (MEN)


KIT CATALOG

90-4111-1 SWING ATTACH FITTING ATA :65 THRU A65, 65A80, B80THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE LOWER FORWARD LHWING 50-120073-7 ATTACH FITTING ON THE CENTER SECION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4111-2 SWING ATTACH FITTING ATA :65 THRU A65, 65A80, B80THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE LOWER FORWARD RHWING 50-120073-8 ATTACH FITTING ON THE CENTER SECION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-5034-1 PSHOULDER HARNESS INSTALLATION, PILOT AND COPILOT ATA : 2565, A65 L-1, L-2, L-6, LF-7, LF-8, LC-1 THRU LC-33580, A80, B80 LD-1 THRU LD-51188 LP-1 THRU LP-47SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW SEAT BELT AND SHOULDERHARNESSES FOR EITHER THE PILOT OR COPLIOT SEAT. ORIGINAL EQUIPMENT CHAIRS ONLY, ONE KITPER SEAT)WT. CHANGE : WT: 3 LBS @ 137 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

90-8002-1 SLANDING GEAR GREASE PROVISIONS, NOSE ATA :70 LB-1 THRU LB-3588 LP-1 THRU LP-47A65 LC-240 THRU LC-335A80, B80 LD-151 THRU LD-466SI NO. 0516-200, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL CURRENT PRODUCTION GREASE BUSHINGSAND FITTINGS.

NOTENOTENOTENOTE:::: THIS KIT CANNOT BE INSTALLED IF KIT 101-8017-1 S HAS BEEN PREVIOUSLY INSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : 15MEN : 1 (MAN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberMAIN SPAR INSPECTION ACCESS COVER - (100-1200-1 S) 1



BATTERY CHARGE CURRENT SENSOR - (100-3009-1 S) 1

MARKER BEACON LIGHT - SPARES - (100-3015-1 S) 2

MARKER BEACON ANTENNA - SPARES - (100-3016-1 S) 2

ITT INDICATOR ISOLATOR - (100-3017- S) 2

ISOLATOR INSULATION, TEMP - (100-3017-1 S) 2

BEACON, UPPER FLASHING - (100-3018-1 S) 2

AUTO IGNITION SYSTEM - (100-3019-1 S) 3

SPAR, OUTBOARD WING FORWARD - (100-4002-1 S) 3



SPAR INSTALLATIONWING FWD - (100-4002-5 S) 3

SPAR INSTALLATIONWING FWD - (100-4002-6 S) 4

PRESSURIZATION AIR CONTROLS, IMPROVED - (100-4004-1 S) 4

OUTFLOW AND SAFETY VALVE, IMPROVED - (100-4004-3 S) 4

PRESSURIZATION AIR CONTROLS, IMPROVED - (100-4004-5 S) 4

ELEVATOR ASSEMBLY, UP-DATE - (100-4005-1 S) 5

AIRSTAIR DOOR REMOVAL, CABIN - (100-4006-1 P) 5

INTEGRAL FITTING SPAR, CENTER SECTION AND OUTBOARD - (100-4007-1 S) 5

AUTOPILOT ELEVATOR SERVO SUPPORT - (100-4009-1 S) 5

BLEED AIR VENTURI - (100-5006-1 S) 6

SHOULDER HARNESS, AFT COMPARTMENT - (100-5009-1 SC) 6

AIR CONDITIONING CROSSOVER DUCT, IMPROVED - (100-5010-1 S) 6

GYRO, ATTITUDE - SPARES - (100-5012-1 S) 6

GLARESHIELD OUTLET, COCKPIT VENTILATION - (100-5013-3 S) 7

WINDOW PANE, POLARIZED - SPARES - (100-5015-1 S) 7

INSULATION RETAINER, HEAT EXCHANGER - (100-5016-1 S) 7

FIRE DETECTOR, ENGINE - SPARES - (100-5017-1 S) 8

AIR CONDITIONER R134A COMPRESSOR ASSEMBLY - (100-5018-1) 8

SPARE COMPRESSOR, AIR CONDITIONER - (100-5018-3) 8


ENGINE FUEL DRAIN COLLECTOR - (100-9008-1 S) 9


ENGINE CHIP DETECTOR - (100-9011-1 S) 9




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberOIL HOSE ASSEMBLY - SPARES - (100-9012-1 S) 10

CHIP DETECTOR WARNING, IMPROVED - (100-9013-1 S) 10

IGNITION SPARK - (100-9014-1 S) 11

FIRE EXTINGUISHER, ENGINE - (100-9015-1 P) 11

BLEED AIR WARNING PRESSURE SWITCH - SPARES - (100-9019-1 S) 11

MAIN SPAR INSPECTION ACCESS COVER - (101-1200-1 S) 12

WING TO FUSELAGE ADAPTER, REINFORCEMENT - (101-1202-1 S) 12





FLOODLIGHT, EMPENNAGE - (101-3027-1 P) 13

FLOODLIGHT, EMPENNAGE - (101-3027-5 P) 14

AIR CONDITIONING REAR EVAPORATOR - (101-3034-1 P) 14




STATIC NOISE REDUCTION, PRECIPITATION, WING - (101-3035-1 S) 15


EXTERNAL POWER OVERVOLTAGE SENSOR - (101-3042-1 S) 16

STARTER GENERATOR, 300 AMP - (101-3043-7 P) 16

STARTER GENERATOR, 300 AMP - (101-3043-9 P) 16

FLAP SWITCH, ASYMMETRICAL - (101-3044-1 S) 16

FLAP LIMIT AND WARNING SWITCHES, IMPROVED - (101-3044-3 S) 17

FLAP LIMIT AND WARNING SWITCHES, IMPROVED - (101-3044-5 S) 17

ELEVATOR TRIM SWITCH - SPARES - (101-3060-1 S) 17

YAW DAMPER SWITCH - SPARES - (101-3060-3 S) 18

SWITCH GUARD, E.L.T. - (101-3062-1 S) 18

RECOGNITION LIGHT, WING TIP - (101-3063-1 P) 18



AIR CONDITIONER PC BOARD - (101-3064-1 S) 19

AIR CONDITIONER ACCESS DOOR MODIFICATION - (101-3064-3 S) 20

LANDING GEAR MOTOR CIRCUIT BREAKER - (101-3069-1 S) 20

LANDING GEAR MOTOR CIRCUIT BREAKER - (101-3069-3 S) 20

LANDING GEAR MOTOR CIRC BRKR - (101-3069-7) 20

KIT"S"L/G MTR CB - (101-3069-7 S) 21



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberAVIONICS BLOWER - (101-3072-1 S) 21

LANDING GEAR CIRCUIT PROTECTION, HYDRAULIC - (101-3076-1 S) 21

LANDING GEAR CIRCUIT PROTECTION, HYDRAULIC - (101-3077-1 S) 21

RUDDER BOOST AND BRAKE DEICE WIRING - (101-3078-1 S) 21

STARTER GENERATOR - SPARES - (101-3086-1 S) 22

RUDDER BOOST SYSTEM WIRING - (101-3087-1 S) 22

RUDDER BOOST SYSTEM WIRING - (101-3087-3 S) 22


ELECTRIC HEAT EQUI - (101-3100-1 S) 23

ELECTRIC HEAT EQUIPMENT - (101-3101-1 S) 23

HYD LDG RELAY - (101-3106-1 P) 23

HYDRAULIC LANDING GEAR MOTOR RELAY - SPARES - (101-3106-1 S) 23

HYDRAULIC LANDING GEAR MOTOR RELAY - (101-3106-3 S) 23

HYD LDG RELAY - (101-3107-1 P) 23


FUEL QUANTITY INDICATOR - (101-3111-1 S) 24

EXTERNAL DC POWER REVERSE POLARITY PROTECTION - (101-3118-1 S) 24

DEICE BOOT REPLACEMENT - (101-3121-1 S) 24

EMERGENCY LOCATOR TRANSMITTER - SPARES - (101-3127-1 S) 25

KIT LANDING GEAR MOTOR CIRCUIT BRKR INST - (101-3133-1 S) 25

ANTENNA CARGO POD - (101-3134-1 P) 25

STATIC INVERTER RELOCATION, CAA CERTIFICATION - (101-3142-1 S) 25

STATIC INVERTERS RELOCATION FOR CAA CERTIFICATION - (101-3142-5 S) 25

FLAP SWITCH, UNITED KINGDOM REGULATIONS - (101-3143-1 S) 26

EMERGENCY LIGHT SWITCH AND CIRCUIT BREAKER - (101-3144-1 S) 26

WIRING MODIFICATION - B300 - UNITED KINGDOM CERTIFICATION - (101-3148-1 S) 26

ANNUNCIATOR MODIFICATION, CAA - (101-3149-1 S) 26

ANNUNCIATOR MODIFICATION, UK - (101-3149-3) 27

CIRCUIT BREAKER PANEL - (101-3150-7 S) 27

BATTERY BUS CHANGE - (101-3151-1 S) 27

SMOKE DETECTOR AND E/L PANEL - (101-3154-1 S) 27

CURRENT SENSOR, U.K. CERTIFICATION - (101-3155-1 S) 28

STALL WARNING MODIFICATION, CAA CERTIFICATION, U.K. - (101-3157-1 S) 28

ATTITUDE TRANSFORMER - (101-3158-1 S) 28






Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSWITCH, G OVERHEAD FUEL PANEL - (101-3165-1 S) 29

EXTERNAL POWER SWITCH MODULE - SPARES - (101-3168-1 S) 30

FUEL QUANTITY INDICATOR REPL INSTL - (101-3169-1 S) 30

ANTENNA MARKER BEACON - (101-3170-1 S) 30

INDICATOR PILOT AIRSPEED - (101-3174-1 S) 30

LIGHT, LANDING GEAR POSITION INDICATOR - (101-3175-1 S) 31

LIGHT, LANDING GEAR POSITION INDICATOR - (101-3176-1 S) 31

AIRSPEED LIMITATIONS IAS KNOTS - (101-3180-1) 31

ENGINE AND FATIGUE MONITORING SYSTEM - (101-3181-1 S) 31

ENGINE AND FATIGUE MONITORING SYSTEM - (101-3181-3 S) 32

CIRCUIT BREAKER FUEL CONTROL PANEL - (101-3186-1 S) 32

WIRING MODIFICATION COMPLY WITH DUTCH REGULATIONS - (101-3189-1 S) 32

ANNUNCIATOR LEGENDS MODIFICATION, (DUTCH CERTIFICATION) - (101-3190-1 S) 32

BATTERY BUS CHANGE (HOLLAND) - (101-3191-1 S) 32

BRACKET CONNECTOR, STRAIN GAGE - (101-3194-1) 33

STRAIN GAGE ACCESS COVER - (101-3196-1) 33

BULKHEAD CONNECTOR CHANGE (SPARE FOR 207201-1 AND 207200-1) - (101-3202-1) 33

WIRE HARNESS, ENGINE FIRE DETECTOR - (101-3208-1) 34

ELT REMOTE SWITCH - (101-3210-1) 34

ELT AND REMOTE SWITCH - (101-3214-1) 35

ELT AND REMOTE SWITCH - (101-3215-1) 36

ELT AND REMOTESWITCH KIT - (101-3215-3) 36




KIT - PITOT HEAT INDICATOR - (101-3238-1) 37

WINDSHIELD SCREW 12000 HOUR - (101-3259-1) 37

ALTIMETER INSTALLATION - (101-3266-1) 38

ALTIMETER INSTALLATION - (101-3266-3) 38

TRANSPONDER INSTL, FLIGHT ID-INFO ONLY - (101-3284-0001) 39

TRANSPONDER INSTL,FLIGHT ID-INFO ONLY - (101-3284-0003) 39

APPROACH MODE UNS-IM WITH FACTORY INSTALLED UNS-IM - (101-3401-1) 39

ELT INSTL, DUAL MODE INFO ONLY - (101-3402-3) 39


GROUND COM RELAY REPL INFO ONLY - (101-3407-1) 40

STANDBY BATTERY RELAY MODIFICATION - (101-3409-0001) 40

ESIS LIGHTING VOLTAGE MOD-INFO ONLY - (101-3410-0001) 41



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberTRANSPONDER WITH ENHANCED SURVEILLANCE INSTL - (101-3505-0001) 41

SEATS, AFT COMPARTMENT FOLDING - (101-4003-1 PC) 41





FOLD UP SEAT AFT C(COMM KT) - (101-4003-19 PC) 42





DUAL SUPPORT CABLE AIRSTAIR DOOR - (101-4010-1 S) 44

AIRSTAIR DOOR DUAL SUPPORT CABLE - (101-4010-3 S) 44

AIRSTAIR DOOR DUAL SUPPORT CABLE - (101-4010-5 S) 44

STROBE LIGHT ROCK SHIELD - (101-4014-3 P) 45

AIR CONDITIONER SOLENOID VALVE - (101-4015-1 S) 45

WINDSHIELD WASHER - (101-4016-1 P) 45

VENTRAL FIN - SPARES - (101-4019-1 S) 45



VENTRAL FIN INSTL - (101-4019-9 S) 46

WING BOLT, LOWER FORWARD - (101-4024-3 S) 46



WING BOLT, UPPER FORWARD - (101-4025-1 S) 47




WING BOLT, AFT UPPER OR LOWER - (101-4026-1 S) 48

WING BOLT, AFT UPPER OR LOWER - (101-4026-3 S) 49

WING BOLT INSTL, AFT - (101-4026-5) 49

WING BOLT INSTL, AFT - (101-4026-7) 49

RUDDER PEDAL LEVER - SPARES - (101-4030-1 S) 50

RUDDER PEDAL LEVER - SPARES - (101-4030-2 S) 50

WING CENTER SECTION, UPPER SKIN - (101-4032-1 S) 50

WING CENTER SECTION, UPPER SKIN - (101-4032-3 S) 51

AIRSTAIR DOOR REINFORCEMENT - (101-4034-1 S) 51



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberJACK PAD REINFORCEMENT, WING AND FUSELAGE - (101-4037-1 P) 51

FLAP CONTROL - (101-4038-1 P) 51

BATTERY RELAY COVER - (101-4039-1 S) 52

FUEL FILTER ACCESS DOOR - (101-4040-1 S) 52

AIRSTAIR DOOR DUAL SUPPORT - (101-4042-1 S) 52

DEFROSTER INSTL,COCKPIT&CABIN WINDOW - (101-4043-1 S) 52

DEFROSTER, COCKPIT AND CABIN WINDOW - (101-4043-11 S) 52

DEFROSTER, COCKPIT AND CABIN WINDOW - (101-4043-13 S) 53

DEFROSTER, COCKPIT AND CABIN - (101-4043-3 S) 53



DEFROSTER - (101-4043-9 S) 54

UPPER WING SKIN - (101-4045-1 S) 54



SEATS FOLD UP, AFT COMPARTMENT - (101-4046-1 PC) 55

FOLD UP - AFT COMPARTMENT SEAT, LEFT SIDE ONLY - (101-4046-3 PC) 55

FOLD UP - AFT COMPARTMENT SEAT, RIGHT SIDE ONLY - (101-4046-5 PC) 55

RIVET SEALING - UPPER WING PANEL - (101-4048-1 S) 56

CENTER SECTION LEADING EDGE - (101-4049-1 S) 56

CENTER SECTION LEADING EDGE - (101-4049-3 S) 56

SPAR BUSHING (1ST OVERSIZE) - (101-4050-1 S) 57

SPAR BUSHING (2ND OVERSIZE) - (101-4050-3) 57

FUEL BLADDER MOD., ADHESIVE AND SEALANTS - (101-4052-1 S) 57

BAGGAGE POD FAIRING EXTENSION MODIFICATION - (101-4053-1 P) 58

WINDSHIELD BIRD GUARD, CREW ENCLOSURE (U.K. CERTIFICATION) - (101-4060-1 S) 58

STIFFENER, AFT PRESSURE BULKHEAD (U.K. CERTIFICATION) - (101-4061-1 S) 58

CARGO DOOR AIRSTAIR HAND RAIL - (101-4062-1 S) 59

STRINGER REINFORCEMENT, AFT FUSELAGE - (101-4063-1 S) 60











Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSTRINGER REINFORCEMENT, AFT FUSELAGE - (101-4064-5 S) 66


STRINGER REINFORCEMENT, AFT FUSELAGE - (101-4064-9) 67

DOOR AIRSTAIR REINFORCEMENT - (101-4065-1 S) 68

SPAR CAP LOWER MAIN, CENTER SECTION - (101-4066-1 S) 68

SPAR CAP LOWER MAIN, CENTER SECTION - (101-4066-3 S) 69

STRINGER REINFORCEMENT, AFT FUSELAGE, LH SIDE - (101-4068-1 S) 69


STRINGER REINFORCEMENT, AFT FUSELAGE, RH SIDE - (101-4068-2 S) 70

STRINGER REINFORCEMENT, AFT FUSELAGE, LH SIDE - (101-4068-3 S) 71












STRINGERS, LH SIDE REINFORCEMENT, AFT FUSELAGE - (101-4070-1 S) 75

STRINGERS, RH SIDE REINFORCEMENT, AFT FUSELAGE - (101-4070-3 S) 75

BAGGAGE PLACARD MODEL B300 CIS - (101-4071-1) 75

BAGGAGE PLACARD MODEL B300 CIS - (101-4071-3) 76

FLAP RIB REPLACEMENT - (101-4072-1) 76

FLAP RIB REPLACEMENT, LH OR RH FIX - (101-4074-1) 77

DOUBLER, WING TO FUSELAGE - (101-4076-1) 77

SPAR ASSEMBLY FATIGUE INSPECTION, COLD WORKING - (101-4077-1) 78

SPAR ASSEMBLY FATIGUE INSPECTION, COLD WORKING - (101-4077-3) 78

SKIN CRACK, LOWER CENTER SECTION - INFORMATION ONLY - (101-4078-1) 79

PLACARD - OPERATING INSTRUCTIONS, AIRSTAIR DOOR - (101-4080-1) 79

SKIN ASSY,TRAILNG EDGE LOW INFO ONLY - (101-4081-1) 79

ATTACH BOLT, WING, LOWER FORWARD - (101-4083-1) 80

ATTACH BOLT, WING, LOWER FORWARD - (101-4083-3) 80

CABIN AIRSTAIR,LATCH BOLTS - (101-4084-1) 80

CABIN AIRSTAIR,UPPER HOOK MECH - (101-4085-1) 81



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCABLE, AIRSTAIR/CARGO DOOR 8,000 CYCLES REPLACEMNT - (101-4091-0001) 81

CABLE, AIRSTAIR/CARGO DOOR 8,000 CYCLES REPLACEMNT - (101-4091-0003) 81

PLACARD INSTALLATION, EMERGENCY EXIT - (101-4310-1) 82


STIFFNER, AFT SHELF - (101-4410-) 83

STIFFENER, AFT SHELF - (101-4410-1) 83

OXYGEN BOTTLE 76 CU. FT. - (101-5006-1 S) 83

INSTALLATION OF 76 CU. FT. OXYGEN BOTTLE - (101-5006-7 S) 83

OXYGEN SYSTEM AUTOMATIC DEPLOYMENT - (101-5007-1 S) 83






MASK INSTALLATION, CREW DILUTER DEMAND - (101-5008-1 S) 85

MIRROR INSTALLATION, RH AFT PARTITION - (101-5034-1 S) 85

AIR CONDITIONING PLUMBING AND PRESSURE SWITCH - (101-5035-1 S) 85



ELECTRIC BONDING, STATIC ELIMINATION - (101-5037-1 S) 86

DRAIN TUBE, FUSELAGE, IMPROVED - (101-5037-3 S) 86

ELECTRIC BONDING, STATIC ELIMINATION - (101-5037-5 S) 87

CHARTHOLDER, BEECHCRAFT CONTROL WHEEL, 720 SERIES - (101-5039-1 P) 87

CARGO RESTRAINT SYSTEM - (101-5040-1 P) 87

STRESS FREE WINDSHIELD - (101-5041-1 S) 88

STRESS FREE WINDSHIELD - (101-5041-3 S) 88

WINDOW, CABIN, FROST FREE - (101-5045-1 S) 88

WINDOW, CABIN, FROST FREE - (101-5045-3 S) 89

AIR CONDITIONER SERVICE PORT - (101-5046-1 S) 89

CONTAINER INSTL OXMASK (COMM KIT) - (101-5048-5 S) 89

FUEL QUANTITY PROBE INSTL - (101-5051-1 S) 89

FUEL QUANTITY PROBE INSTL - (101-5051-3 S)

90

FUEL QUANTITY PROBE INSTL - (101-5051-5 S) 90

VENT BLOWER INSTALLATION - (101-5062-1 S) 90

FLOW CONTROL VALVE(COMM KIT) - (101-5065-1 S) 91

BAGGAGE LIMITATION(COMM KIT) - (101-5068-1 P) 91

BAGGAGE LIMITATION,AFT COMPARTMENT - (101-5068-3 P) 91



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberBAGGAGE LIMITATIONAFT COMPT - (101-5068-5 P) 91

FUEL SYSTEM SPLICEINSTL (KIT) - (101-5082-1 S) 91

AIR INLET REINF (KIT) - (101-5083-1 S) 91

EXPORT ICAO ANNEX 8 INSTLN - (101-5084-1 P) 91

HYDRAULIC BRAKE RESERVOIR INSTAL - (101-5086-1) 92

BRAKE DEICECLAMP INSTAL KIT - (101-5088-1 S) 92

REINF INSTL, SEATBELT ATTACHMENT - (101-5092-1 S) 92

REDUCED GROSS WEIGHT MODEL 300 - (101-5093-7 P) 92

SPEED WARNING INST - (101-5095-1 P) 92

BARRIER INSTL NOSE COMPARTMENT - (101-5101-1 S) 92

SERVO COVER INSTL - (101-5106-1 S) 93

SERVO COVER INSTLSPERRY SPZ 4000 - (101-5107-1 S) 93

OVERBOARD PRESSURIZATION DUMP SYSTEM - (101-5109-1 S) 93

TABLE IMPROVEMENTB200 - (101-5119-1 S) 93

FOREIGN CERTPLACARD INSTL - (101-5136-1 S) 93

CLOCK INSTL CONTROL WHEEL - (101-5137-1 S) 93

FOREIGN CERTIFICATION FIRE EXTINGUISHER INSTALLATION - (101-5138-1 S) 94

SEAT BELT INSTL U.K. - (101-5141-1 S) 94

SPEAKER INSTALLCABIN - (101-5145-1 S) 94

AILERON TRIMPULLEY - (101-5146-1 S) 94

A/C RELIEF VALVE INSTALL - (101-5149-1 S) 94





FOREIGN CERTPLACARD INSTL - (101-5151-1 S) 95

R134A REFRIG CHANGE,AIR CONDITION - (101-5160-5) 96

REFRIGERANT CHANGE, A/C-FORWARD EVAPORATOR ONLY - (101-5164-1) 97

REFRIGERANT CHANGE, A/C-FORWARD EVAPORATOR ONLY - (101-5164-3) 97

FIRE EXTINGUISHER KIT - (101-5166-1) 98

COMPRESSOR, AIR CONDITIONING - (101-5170-1) 99



COMPRESSOR SERVICE FITTING CHANGE - (101-5171-1) 100






Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCOMPRESSOR SERVICE FITTING CHANGE - (101-5171-9) 102

HUMPSEAL INSTALLATION, WINDSHIELD - (101-5172-1) 102

CREW MASK REPLACEMENT, OXYGEN - (101-5178-1) 103






BOOST REGULATOR - (101-5196-0001) 104

EMERGENCY LIGHTING INSTL, JAR OPS - (101-5301-1) 105

EMERGENCY LIGHTING INSTL, JAR OPS - (101-5301-3) 105

FLOOR INSTL, CARGO - (101-5307-1) 105

EMPENNAGE INSPECTION PANELS - (101-6003-0001) 105


EMPENNAGE INSPECTION PANELS - (101-6003-0005)

106



107


107

BRAKE DEICER INSTL - (101-8005-11 S) 107





BRAKE DEICE HOSEINSTAL KIT - (101-8011-1 S) 108

MLG DOOR RETRACT MECHANISM IMPRO - (101-8013-3 S) 108

MLG DOOR RETRACT MECHANISM IMPRO - (101-8013-5 S) 109

HYDRAULIC LANDING GEAR INSTL KIT - (101-8018-1) 109

HYDRAULIC LANDING GEAR INSTALATION KIT - (101-8018-3) 109

DE ICE INSTL, WHEEL BRAKE - (101-8025-1 S) 109

ALUM NOSE WHEEL INSTL - (101-8027-1 P) 109

HIGH FLOTATION LANDING GEAR - (101-8031-1 P) 109

MAIN WHEEL ASSEM REPLACEMENT - (101-8032-1 S) 110

SUPPORT ASSEMBLY ACTUATOR BEARING - (101-8034-1) 110

ENG.FIRE EXTINGUISHER*RA - (101-9005-1 P) 110

KIT, FIRE EXTINGUISHER - (101-9005-3) 110

OIL VENT EXHAUST INSTL (COML KIT) - (101-9012-1 S) 111



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFUEL VENT PLUMB - (101-9015-1 S) 111

FUEL VENT PLUMBING - (101-9015-3 S) 111

FUEL VENT PLUMB - (101-9015-5 S) 111

WASH RING INSTALLATION, ENGINE PT6A-41 & -42 - (101-9016-1 S) 111

WASH RING INSTALLATION, ENGINE PT6A-41 & -42 - (101-9016-3)

112

WASH RING INSTALLATION, ENGINE PT6A-41 & -42 - (101-9016-5) 112

PROP AUTOFEATHER & SYNCHROPHASER - (101-9022-1) 112

SYNCHROPHASER TARGPROP INSTL (KIT) - (101-9025-1 S) 113

PROP MOUNT BOLT INSTALLATION - (101-9027-1 S) 113

FUEL PURGE TANK IN(COMM KIT) - (101-9030-1 S) 113

FUEL FLOW DIVI& DAMP VALVE - (101-9037-3 S) 113

SYNCHROPHASER TARGET INSTL - (101-9038-1 S) 113

HOT LIP DUCT STIFFINSTL - (101-9039-1 S) 114

MID COWLING GUIDE& AFT LATCH REIN - (101-9042-1 S) 114

S D4 STACK - (101-9044-1 S) 114

MID COWLING LATCHINSTL - (101-9047-1 S) 114

EXHAUST STACK INSTALLATION - (101-9048-1 S) 114

EXHAUST STACK INSTALLATION - (101-9048-11) 114





INLET DUCT REPLACEMENT KIT - (101-9049-1 S) 115

COWLING STIFFENERINSTALL - (101-9050-1 S) 115

COWLING DOOR LEDGE REPLACEMENT - (101-9052-1 S) 115

EXHAUST STACK CONSTANT AREA - (101-9059-1 S) 116

AMBIENT AIR DUCTINSTL BLEED AIR - (101-9060-1 S) 116

AIR INLET DUCTSLEEVE INSTL - (101-9061-1 S) 116

HOT LIP FLEX HOSEREPL - (101-9063-1 S) 116

DEICE BOOT REINFORCEMENT INFO ONLY - (101-9066-1 S) 116

PNEUMATIC AIRINSTAL - (101-9067-1 S) 116

PNEUMATIC AIRINSTAL - (101-9067-3 S) 116

FIRE RESISTHOSE - (101-9068-1 S) 116

EXHAUST PIPEASSEM REPL - (101-9074-1 S) 117

COWL BRACKET - (101-9075-1 S) 117

COWL BRACKET - (101-9075-3 S) 117

DETECTOR INSTL, FIRE AND OVERHEAT - (101-9077-1) 117



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberDETECTOR INSTL, FIRE AND OVERHEAT - (101-9077-3) 118

COMPRESSOR AIR CONDITIONING - (101-9078-1) 118

A/C COMPRESSORINSTL KIT - (101-9078-3) 118

A/C COMPRESSORINSTL KIT - (101-9078-5) 118

FUEL FLOAT VALVE, WING TIP - (101-9081-1) 118

FUEL FLOAT VALVE,WING TIP - (101-9081-5) 119

TUBE BREAK WARN BLEED AIR INFO ONLY - (101-9082-1) 119

REPR TUBE BREAKAGE WARNING INFO ONLY - (101-9083-1) 119

EXHAUST STACKINSTL KIT - (101-9085-1) 119

EXHAUST STACKINSTL KIT - (101-9085-3) 120

EXHAUST STACK INSTL KIT - (101-9085-5) 121

ENGINE IGNITION EXCITER BOX INSTALLATION - (101-9088-0001) 121

ENGINE IGNITION EXCITER BOX INSTALLATION - (101-9108-0001) 121

RIGHT AILERON SUBSPAR - (109-4011-1) 122

TANK INSTL FUEL PURGE - (109-9000-5) 122

TANK INSTL - (109-9011-1) 122

TANK INSTL, FUEL PURGE - (109-9012-1) 123

TANK INSTL, FUEL PURGE - (109-9013-1) 123

AIR CONDITIONER COMPRESSOR INSTALLATION, SPARES - (117-9000-1 S) 123

AIR CONDITIONER COMPRESSOR INSTALLATION, SPARES - (117-9000-3) 123

AIR CONDITIONER COMPRESSOR INSTALLATION, SPARES - (117-9000-5) 124

LEADING EDGE IMPROVEMENT - (130-1200-1) 124

FIELD PERFORMANCEIMPROVEMENT - (130-3004-1 S) 124

FIELD PERFORMANCEIMPROVEMENT - (130-3004-3 S) 125

PILOT HEATANNUNCIATION - (130-3008-1) 125

CIRCUIT BREAKER RE-LOCATION - (130-3016-1) 125

PITOT HEAT INDICATOR - (130-3017-1) 126


PITOT HEAT & STALL HEAT ANNUNCIATORS - (130-3018-1) 126

NI CAD BATTERY - (130-3019-1) 126

STALL WARNING MOD,MODEL B300 - (130-3022-0001) 127

COLD CATHODE LIGHTING PANEL-INFO ONLY - (130-3025-0001) 127

ALTIMETER REPLACEMENT KIT - (130-3404-1) 127

HF & ADF INSTL - (130-3405-1) 127

HF & ADF INSTL - (130-3405-3) 127

CVR INSTALLATION INFO ONLY - (130-3407-1) 128

ELT INSTALLATION,DUAL MODE INFO ONLY - (130-3408-1) 128



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberELT INSTALLATION,DUAL MODE INFO ONLY - (130-3408-3) 128

FRENCH MOD - (130-3410-1) 128

ALTIMETER INSTALLATION, RVSM - (130-3411-1) 129

AVIONICS UPGRADE ADC 85A - (130-3412-0001) 129

AUDIO SWITCH PANEL REPLACEMENT - (130-3413-0001) 129

AUDIO SWITCH PANEL REPLACEMENT - (130-3413-0003) 129

AVIONICS NOSE SHELF STRUCTURAL IMPROVEMENT - (130-3415-0001) 130

AVIONICS NOSE SHELF STRUCTURAL IMPROVEMENT - (130-3415-0003) 130

EXTERNAL DC POWERSWITCH TRANSIENT - (130-3600-1) 130

BREAKIN & EXITMARKINGS INSTL - (130-4000-1 M) 130

ICE PROTECTION NOSE DOOR - (130-4002-1) 131

ICE PROTECTION NOSE DOOR - (130-4002-3) 131

GRAVEL RUNWAY PROTECTION INSTL - (130-4008-1) 132

WINDSHIELD WASHERINSTALLATION - (130-4009-1) 132

WING BOLT COVER INSTALLATION KIT - (130-4011-0001) 132

CENTRAL FIN INSTL,DUAL - (130-4400-0001) 132

CENTRAL FIN INSTL,DUAL - (130-4400-0003) 133

REFRIGERANTCHANGE AIR - (130-5009-1) 133

REFIGERANTCHANGE AIR - (130-5009-3) 133

REFRIGERANT CHANGE, AIR - (130-5009-5) 133

INSTL, AFTHEAT DISTRIBUTIO - (130-5010-1) 133

ACTUATOR ASSY/INSTL ELEVATOR TRIM - (130-5011-3) 133

ACTUATOR ASSY/INSTL ELEVATOR TRIM - (130-5011-9) 134

FIRE EXTINGUISHERINSTALL - (130-5012-1) 134

CIS REQUIREMENTS - (130-5014-1) 134

SEAT BELT COVER TUBE, CABIN CHAIR KIT (DO NOT OCCUPY) - (130-5015-1) 134

PLACARDS, CHINESETRANSLATION - (130-5016-5) 134

CREW CHAIR UPDATE - (130-5017-1) 134

AIR CONDITIONINGINSTL, B300 - (130-5018-1) 134

AIR CONDITIONING INSTL - (130-5018-3) 135

FR12 REFRIGERANT CHANGE, AIR CONDITIONING - (130-5022-1) 135

PLACARD MOROCCAN CERTIFICATIONS KIT - (130-5023-1) 135

FURNISHINGINSTL - (130-5024-1) 135

PLACARDS, PORTUGUESE TRANSLATION - (130-5026-1) 135

PLACARDS, PORTUGUESE TRANSLATION - (130-5026-3) 135

SPANISH TRANSLATION PLACARD KIT - (130-5028-1) 136




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSPANISH TRANSLATION PLACARD KIT - (130-5028-5) 136


CABIN SEAT SHOULDERHARNESS STOP/OAK - (130-5068-1) 137

CABIN SEAT SHLDER HARNESS STOP/CLEAR - (130-5068-11) 137

CABIN SEAT SHLDR HARNES STOP/GRAPHIT - (130-5068-3) 138

CABIN SEAT SHOULDERHARNES STOP/BLUE - (130-5068-5) 138

CABN SEAT SHLDER HARNES STOP/NEUTRAL - (130-5068-7) 139

CABIN SEAT SHOULDERHARNESS STOP/RED - (130-5068-9) 139

SWIVELING CHAIR PEDESTAL REPLACEMENT - (130-5108-0001) 140

SWIVELING CHAIR PEDESTAL REPLACEMENT - (130-5108-0002) 140

B300 CRASH AXE KIT - (130-5300-1) 140

KIT - DUCTING, OVERHEAD - (130-5507-0001) 140

FIRE EXTINGUISHER INSTALLATION KIT - (130-5701-0001) 141

PISTON, MAIN LANDING GEAR - (130-8001-0001) 141

PISTON, MAIN LANDING GEAR - (130-8001-0003) 141

HIGH FLOTATION LANDING GEAR - (130-8002-0001) 142

HIGH FLOTATION LANDING GEAR - (130-8002-0003) 142

EXHAUST STACK FAIRING - (130-9001-1) 142

WASH RING INSTL ENGINE KIT - (130-9003-1) 142

WASH RING INSTAL ENGINE - KIT - (130-9003-5) 143

FUEL CELL COVER &GASKET INSTL - (130-9005-1) 143



GROUND IDLE SOLENOID SYSTEM - (130-9600-1) 145

FILTER,PNEUMATIC AIR,WIDOW DEFROST - (130-9700-1) 145

KIT TUBING, DEICE - (130-9701-0001) 145

KIT TUBING, DEICE - (130-9701-0003) 145

AIR CONDITIONER COMPRESSOR KIT - (130-9702-0001) 146


FIRE EXTINGUISHER REPLACEMENT - (36-5017-1 S) 146

FIRE EXTINGUISHER REPLACEMENT SPARES FOR FR-2 3/4 FIRE EXTINGUISHER - (36-5017-3 S) 147

FUEL VENT DEFLECTOR INSTL - (50-9005-0001) 147

CLOCK INSTALLATION, CONTROL WHEEL, (28 -VOLT) - (55-3028-3 P) 147







Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFLAP TRAVEL SWITCH COVER - (90-3089-1 S) 148

FLAP TRAVEL SWITCH COVER - (90-3089-3 S) 148

AIR CONDITIONER RELAY CONTROL - SPARES - (90-3096-1 S) 149

BATTERY AMP INDICATOR, DC VOLT - (90-3097-1 S) 149

WINDSHIELD, LH HEATED - (90-3100-1 P) 149

WINDSHIELD, RH HEATED - (90-3100-2 P) 150

WINDSHIELD DEICE ELECTRONICS INSTALLATION - (90-3100-3 P) 150

BEACON, VERTICAL STABILIZER, FLASHING - (90-3101-1 S) 150

BEACON, LOWER FLASHING - (90-3102-1 S) 151






OIL PRESSURE TRANSDUCER INSTALLATION - (90-3106-1 S) 152

ICE VANE ACTUATOR - (90-3107-1 P) 152


TIME DELAY RELAY INSTALL - (90-3109-1 S) 153

LIMITER - (90-3110-1 S) 153

INDICATOR LANDING GEAR POSITION LIGHT - (90-3111-1 S) 153

RADIO ALTIMETER ANTENNA RELOCATION - (90-3112-1 S) 154


REMOTE MOUNTED OIL PRESSURE TRANSDUCER - (90-3119-0001) 154



KIT EMERGENCY LIGHTING INSTALLATION - JAR-OPS - (90-3600-1) 155

DAMPENER AIR STADOOR (KIT) - (90-4023- M) 155

ELEVATOR, ALUMINUM - (90-4061- S) 155

LH ALUMINUM ELEVATKIT - (90-4062- S) 155

ELEVATOR, ALUMINUM - (90-4062-1 S) 156

CENTER SECTION SPAPROVISION (COMM - (90-4063- S) 156

MAIN SPAR INSPECTION PROVISIONS, CENTER SECTION - (90-4063-1 S) 156

WINDOW, POLARIZED, 6 WINDOWS - (90-4065- P) 156

WINDOW, POLARIZED, 7 WINDOWS - (90-4065-1 P) 156

DOOR SEAL PRESSURIZATION SOURCE - (90-4069-1) 157

DOOR SEAL PRESS SO(COMM KIT) - (90-4069-1 S) 157

DOOR SEAL PRESSURIZATION SOURCE - (90-4069-3 S) 157



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberBAGGAGE DOOR SECONDARY LATCH, NOSE - (90-4076-1 S) 157

WING TSPAR, CENTER SECTION AND OUTBOARD WING - (90-4077-1 S) 158

PRESSURIZATION VALVE - SPARES - (90-4080-1 S) 158

PRESSURIZATION VALVE - SPARES - (90-4080-3) 158

S SCD NS DR LB - (90-4081-1 S) 158

ELEVATOR - SPARES - (90-4082-1 S) 158

ELEVATOR - SPARES - (90-4082-2 S) 159

ELEVATOR HINGE - (90-4083-1 S) 159

ELEVATOR, MAGNESIUM - (90-4084-1 S) 159



EMERGENCY EXIT DOOR, PRESSURIZED SEAL - (90-4088-1 S) 160

WINDOW, AFT CLEAR TEARDROP - (90-4095-1 M) 160

KEEL REINFORCEMENT - (90-4096-1 S) 160

KEEL REINFORCEMENT - (90-4096-2 S) 161

ELEVATOR PULLEY BRACKET SUPPORT - (90-4098-1 S) 161

WING SPAR REINFORCEMENT - (90-4101-1 1S) 161

WING SPAR REINFORCEMENT - (90-4101-11 S) 161








STABILIZER AND FIN SEALING - (90-4102-1 S) 163














Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberWING ATTACH FITTING - (90-4112-2 S) 166





WING SPAR BRIDGE FASTENER REPLACEMENT - (90-4115-1) 167

WING TIP PODS REMOVAL AND REPLACEMENT WITH STANDARD C90A WING TIPS - (90-4116-1 S) 167

BATTERY ACCESS DOOR AIR SCOOP - (90-4118-1) 168

PLACARD, NOSE BAGGAGE/AVIONICS DOOR - (90-4119-1) 168

AILERON AERODYNAMIC BALANCE WEDGE INSTALLATION - (90-4121-1) 168

IMPROVED HEATERINSTALLATION KIT - (90-5015- S) 168

AIR CONDITIONER START CONTROL - (90-5027-1 S) 169



OXYGEN REGULATOR VALVE - SPARES - (90-5031-1 S) 169

SHOULDER HARNESS, PILOT AND COPILOT - (90-5034-1 P) 170

VENTILATION BLOWER - SPARES - (90-5041-1 S) 170

S PLRZD WD PNE - (90-5044-1 S) 170

CONTROL WHEEL, HEAVY TWINS - SPARES - (90-5046-1 P) 170

WINDSHIELD ANTI-STATIC TAB BONDING - (90-5048-1 S) 171

AIR CONDITIONER MOTOR, IMPROVED - (90-5051-1 S) 171

AIR CONDITIONER MOTOR, IMPROVED - (90-5051-7 S) 171


FIRE DETECTOR, ENGINE - (90-5053-1 P) 172

FIRE DETECTOR, ENGINE - (90-5053-3 P) 172

OUTFLOW AND SAFETY VALVE GASKET - SPARES - (90-5058-1 S) 172

CONDENSATION DRAIN SEAL - SPARES - (90-5059-1 S) 173

POWER TEST JACK - (90-5060-1 S) 173

TEMPERATURE SENSOR - SPARES - (90-5061-1 S) 173

ANTI-SIPHON, FUEL - (90-5062-1 S) 173

TURN AND BANK INDICATOR - SPARES - (90-5063-1 S) 174

AIR CONTROL VALVE, CABIN - (90-5064-1 S) 174

ELEVATOR TRIM TAB CABLE GUARD - (90-5065-1 S) 174







Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFIRE EXTINGUISHER, ENGINE - (90-5066-5 P) 176


FIRE EXTINGUISHER INSTALL ENGINE - (90-5066-9) 176

FIRE DETECTOR, ENGINE (3 DETECTOR SYSTEM) - (90-5067-1 P) 176

FIRE DETECTOR, ENGINE (4 DETECTOR SYSTEM) - (90-5067-3 P) 177

FIRE DETECTOR INSTL ENGINE - (90-5067-5) 177

SEALANT - BATTERY BOX - ELECTRICAL SHELF - (90-5068-1 S) 177

SEALANT - BATTERY BOX - ELECTRICAL SHELF - (90-5068-3 S) 177

HEAT DEFLECTOR SHIELD - (90-5069-1 S) 177

FUEL TOTALIZER GROUND STRAP - (90-5070-1 S) 178

MIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE - (90-5072-1 S) 178

MIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE - (90-5072-3 S) 178

MIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE - (90-5072-5) 179

MIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE - (90-5072-7) 179

REFRIGERANT CHANGE AIR CONDITIONER TO R134A - (90-5077-1) 180

REFRIGERANT CHANGE AIR CONDITIONER TO R134A - (90-5077-3) 181

FIRE EXTINGUISHERINSTL - (90-5078-1) 181

FIRE EXTINGUISHER (352TS) RELOCATION AFT CABIN FLOOR MOD - (90-5078-1 S) 181

PRESSURIZATION CONTROL TUBES - (90-5079-1) 182

PRESSURIZATION CONTROL TUBES - (90-5079-3) 183

CREW MASK REPL(-5-7-9-11 FOR MASK) - (90-5080-1) 183


CREW MASK REPL(-5-7-9-11 FOR MASK) - (90-5080-3) 184




FR12 REFRIGERANT CHANGE FOR R12 FREON SYSTEM - (90-5081-1) 185

FR12 REFRIGERANT CHANGE, AIR CONDITIONER - (90-5081-3) 185



FURNISHINGS - INFORMATION ONLY - (90-5085-1) 186


INDICATOR REPL TURN AND SLIP, AIR - (90-5087-1) 186


AIRCRAFT OWNERSHIP PLATES INFO ONLY - (90-5089-1) 186

PLACARD, SPANISH TRANSLATION - (90-5093-1) 187

ALTIMETER INSTL INFO ONLY - (90-5095-1) 187



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberALTIMETER INSTL INFO ONLY - (90-5095-3) 187

MAGAZINE RACK REPLACEMENT - (90-5328-0 1) 187

LANDING GEAR GREASE PROVISIONS, NOSE - (90-8002-1 S) 188

BRAKE DEICE, STANDARD LANDING GEAR - (90-8003-1 P) 188

BRAKE DEICE, HIGH FLOTATION LANDING GEAR - (90-8003-3 P) 188

LANDING GEAR, HYDRAULIC - (90-8011-1 P) 188

LANDING GEAR INSTALLATION, HYDRAULIC - (90-8011-3 P) 189

LANDING GEAR EMERGENCY EXTEND PLUMBING - (90-8012-1 S) 189

PLACARD INSTL,HYDRAULIC LANDING - (90-8013-1 S) 189

SUPPORT ASSY ACTUATOR BEARING, MLG - (90-8015-0001) 189

ENGINE HOT SECTION INSPECTION REPLACEMENT PARTS - (90-9001- S) 189

ENGINE HOT SECTION INSPECTION REPLACEMENT PARTS - (90-9001-1 S) 190



POWER CONTROL CABLE BOOT - (90-9060-1 S) 190

BLEED AIR WARNING PRESSURE SWITCH REPLACEMENT - (90-9061-1 S) 191

FUEL PRESSURE SWITCH, IMPROVED - (90-9062-3 S) 191

FUEL PRESSURESWITCH KIT - (90-9062-5 S) 191

PROPELLER SEAL DRAIN LINE - (90-9064-1 S) 191

PROPELLER SEAL DRAIN LINE - (90-9064-5 S) 192

AUTOPILOT ELEVATORSERVO - (90-9067-1 S) 192

WASH RING, ENGINE - (90-9068-3 S) 192

PROPELLER GROUND IDLE STOP - (90-9070-1 S) 192

FIREWALL SHUTOFF VALVE - SPARES - (90-9072-1 S) 193

FIREWALL SHUTOFF VALVE - SPARES - (90-9072-3 S) 193

CROSSFEED VALVE - SPARES - (90-9072-5) 193


DEICE, 3 BLADE HARTZELL PROPELLER - (90-9074-1 P) 194

PARALLELING RELAY DC GENERATOR - (90-9075-1 S) 194

ENGINE MOUNT VIBRATION ISOLATOR CORE - SPARES - (90-9077-1 S) 194

OIL VENT EXHAUST, PT6A ENGINE - (90-9078-1 S) 194




PLACARD, CAUTION - (90-9080-1 S) 195

ENGINE QUICK CHANGE, PT6A-21 - (90-9081-1 S) 195

COWLING REINFORCEMENT - LOWER FORWARD - (90-9083-1 S) 196



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberINVERTER, LH INSTALLATION - SPARES - (90-9084-1 S) 196

INVERTER, RH INSTALLATION - SPARES - (90-9084-2 S) 196

INVERTER - (90-9085-1 S) 196

INVERTER - (90-9085-3 S) 196

INVERTER - SPARES - (90-9086-1 S) 197

INVERTER - SPARES - (90-9087-1 S) 197

FIRE RESISTANT HOSE - (90-9088-1 P) 197





PLACARD INSTL,INTERIOR & EXTERIOR, SPANISH(CHILI) - (90-94-0001)

198

VHF ANTENNA ASSEMBLY - (91-3001-49) 198

LIFT TRANSDUCER HEAT CONTROL - (99-3027-1 S) 198

LIFT TRANSDUCER HEAT CONTROL FOR AIRCRAFT WITH 795-6 OR 795-9 TRANSDUCER - (99-3027-3 S) 199

DIRECTIONAL GYRO - SPARES - (99-3028-1 S) 199

SERVO AMPLIFIER - SPARES - (99-3038-1 P) 199

FLAP EXTENSION MECHANISM - (99-4017- S) 199

HORIZONTAL STABILIZER HINGE - (99-4026-1 S) 200

HORIZONTAL STABILIZER CHECK FIXTURE - (99-5012-1 S) 200

SEAT BELT EXTENDER (BLACK) AIRCRAFT PASSENGER SEATS WITHOUT SHOULDER HARNESS - (99-5017-1P)

200

SEAT BELT EXTENDER (BEIGE) AIRCRAFT PASSENGER SEAT WITH SHOULDER HARNESS - (99-5017-3 P) 200

HINGE ALIGNMENT FIXTURE HORIZONTAL STABILIZER - (99-5020-1 S) 201

LANDING GEAR GREASE PROVISIONS, MAIN - (99-8009-3 S) 201

LANDING GEAR GREASE PROVISIONS, MAIN - (99-8009-5 S) 201

IMPROVED PROPELLER SEAL DRAIN - (99-9017-1 S) 201

IMPROVED PROPELLER SEAL DRAIN - (99-9017-3 S) 202

PROPELLER SEAL DRAIN - (99-9017-7 S) 202

PROPELLER SEAL DRAIN - (99-9017-9 S) 202


KIT CATALOG

100-1200-1 SMAIN SPAR INSPECTION ACCESS COVER ATA :A200CT FE-9B200 BL-141B200 BB-1512B200C (12F) BL-73B200T BT-38B300 FL-127THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ACCESS COVER ON THELOWER INBOARD SIDE OF EACH NACELLE AND MAKE A CUTOUT IN THE FAIRING ANGLE WHICH WILLALLOW INSPECTION OF THE LOWER MAIN SPAR CAP IN THIS AREA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 16MEN : N/A

100-2003-1 SEXTERIOR PLACARD ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS. A SPRAY CAN OF PROTECTIVE FINISH IS INCLUDED WITH THEKIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

100-2004-1 SINTERIOR PLACARD ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-3009-1 SBATTERY CHARGE CURRENT SENSOR ATA :100 AND A100 B-1 THRU B-17590, A90, B90, C90 LJ-1 THRU LJ-601E90 LW-1 THRU LW-67SI NO. 0587-356 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BATTERY CHARGE CURRENT DETECTINGDEVICE TO MONITOR THE CONDITION TO THE NICKEL-CADMIUM BATTERY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A


KIT CATALOG

100-3015-1 SMARKER BEACON LIGHT - SPARES ATA :A90, B90, C90, E90, 100, A100, 200THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT MARKER BEACONLIGHT FOR P/N VM202-129.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : N/A

100-3016-1 SMARKER BEACON ANTENNA - SPARES ATA :B90, C90 AND E90, 100, A100, B100, 200,200TTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT MARKER BEACONANTENNA FOR P/N 35-5016.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : N/A

100-3017- SITT INDICATOR ISOLATOR ATA :B100 BE-1 THRU BE-135SI NO. 1251 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REDUCE THE POSSIBILITY OF ERRATIC ITTINSTRUMENT READINGS BY INSTALLING ISOLATORS FOR THE ITT INDICATORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

100-3017-1 SISOLATOR INSULATION, TEMP ATA : 77SI NO. 1252WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

100-3018-1 SBEACON, UPPER FLASHING ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON ASREPLACEMENT FOR THE GRIMES ROTATING BEACON.WT. CHANGE : N/AEST. MAN/HRS: : 3 TO 4MEN : N/A


KIT CATALOG

100-3019-1 SAUTO IGNITION SYSTEM ATA :B100SB NO. 2177 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AUTOMATIC IGNITION SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-4002-1 SSPAR, OUTBOARD WING FORWARD ATA :100 AND A100 B-1 THRU B-19390, A90, B90 LJ-1 THRU LJ-501C90 LJ-502 THRU LJ-624E90 LW-1 THRU LW-87E90 LW-1 THRU LW-87THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN OUTBOARD WING FORWARD SPAR. (SPARIS NOT INCLUDED IN THE KIT).WT. CHANGE : N/AEST. MAN/HRS: : 150MEN : N/A

100-4002-3 SSPAR, OUTBOARD WING FORWARD ATA :100, A100 B-1 THRU B-193C90 LJ-502 THRU LJ-624E90 LW-1 THRU LW-87THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH OUTBOARD WING FORWARD SPAR.(SPAR IS INCLUDED IN THIS KIT).WT. CHANGE : N/AEST. MAN/HRS: : 150MEN : N/A

100-4002-4 SSPAR, OUTBOARD WING FORWARD ATA :100, A100 B-1 THRU B-193C90 LJ-502 THRU LJ-624E90 LW-1 THRU LW-87THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RH OUTBOARD WING FORWARD SPAR.(SPAR IS INCLUDED IN THIS KIT).WT. CHANGE : N/AEST. MAN/HRS: : 150MEN : N/A

100-4002-5 SSPAR INSTALLATIONWING FWD ATA : 57WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

100-4002-6 SSPAR INSTALLATIONWING FWD ATA : 57WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

100-4004-1 SPRESSURIZATION AIR CONTROLS, IMPROVED ATA :100 AND A100 B-1 THRU B-20590, A90, B90, C90 LJ-76 THRU LJ-571, LJ-575 THRU LJ-640E90 LW-1 THRU LW-122SI NO. 0749-453 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING PRESSURE CONTROLLER ONTHE PEDESTAL WITH A NEW CONTROLLER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

100-4004-3 SOUTFLOW AND SAFETY VALVE, IMPROVED ATA :100 AND A100 B-1 THRU B-20590, A90, B90, C90 LJ-76 THRU LJ-571, LJ-575 THRU LJ-640E90 LW-1 THRU LW-122SI NO. 0749-453 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING OUTFLOW SAFETY VALVE103460-7 OR 103456-4 WITH A NEW OUTFLOW SAFETY VALVE.

NOTENOTENOTENOTE:::: YOU CAN NOT MIX VALVE, BOTH VALVES ON LEFT MUST BE REPLACED.NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 2 FOR ADDITIONAL INFORMATION.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 15MEN : N/A

100-4004-5 SPRESSURIZATION AIR CONTROLS, IMPROVED ATA :200 BB-2 THRU BB-48SI NO. 0749-453 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING PRESSURIZATION OUTFLOWAND SAFETY VALVES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)


KIT CATALOG

100-4005-1 SELEVATOR ASSEMBLY, UP-DATE ATA :100, A100 B-1 THRU B-230B100 BE-1 THRU BE-17SI NO. 0799-133, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK ONE ELEVATOR ASSEMBLY ON IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

100-4006-1 PAIRSTAIR DOOR REMOVAL, CABIN ATA :90, A90, B90, C90, C90A LJ-1 AND AFTERE90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE AND REINSTALL THE CABIN AIRSTAIR DOOR.WT. CHANGE : WT: -61.5 LBS @ 243.0 ARMEST. MAN/HRS: : 12 TO 16MEN : N/A

100-4007-1 SINTEGRAL FITTING SPAR, CENTER SECTION AND OUTBOARD ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INTEGRAL FITTING, LOWER MAIN CENTERSECTION SPAR CAP AND OUTBOARD WING MAIN SPAR.WT. CHANGE : WT: SEE KIT DRAWINGEST. MAN/HRS: : 1550MEN : N/A

100-4009-1 SAUTOPILOT ELEVATOR SERVO SUPPORT ATA :A100 B-240 THRU B-247B100 BE-2 THRU BE-119SI NO. 1197 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REINFORCE THE AUTOPILOT ELEVATOR SERVOSUPPORT BRACKET ON AIRPLANES EQUIPPED WITH THE SPERRY SPZ-200A AUTOPILOT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

100-5006-1 SBLEED AIR VENTURI ATA :100, A100 B-1 THRU B-145SI NO. 0704-452 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A VENTURI FOR EASE OFCHECKING PRESSURIZATION FLOWS FOR INSERVICE AIRCRAFT:WT. CHANGE : N/AEST. MAN/HRS: : 6 TO 8MEN : 2 (MEN)

100-5009-1 SCSHOULDER HARNESS, AFT COMPARTMENT ATA :100, A100 B-20 THRU B-171SI NO. 0942, REV. 1, AND SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SHOULDER HARNESS REPLACEMENT ONAIRPLANES HAVING A FORWARD FACING TOILET, FORWARD OF THE BAGGAGE WEBBING.WT. CHANGE : WT: 1.9 LBS @ 316.4 ARMEST. MAN/HRS: : 2MEN : N/A

100-5010-1 SAIR CONDITIONING CROSSOVER DUCT, IMPROVED ATA :100, A100 B-1 THRU B-230100, A100 B-1 THRU B-23090, A90, B90, C90 LJ-1 THRU LJ-701B100 BE-1 THRU BE-16E90 LW-1 THRU LW-202SI NO. 0912 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING CROSSOVER DUCT WITH ANIMPROVED DUCT ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24MEN : 1 (MAN)

100-5012-1 SGYRO, ATTITUDE - SPARES ATA :100, A100 B-1 THRU B-247200, B200 BB-2 THRU BB-833200C BL-1 THRU BL-31200CT BN-1200T BT-1 THRU BT-20B100 BE-1 THRU BE-114C90 LJ-502 THRU LJ-954E90 LW-1 THRU LW-347THIS KIT IS THE SPARES REPLACEMENT FOR 500-ECFB, 500ECF, 500E, 100-384070-1 OR 101-384120-1GYROS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

100-5013-3 SGLARESHIELD OUTLET, COCKPIT VENTILATION ATA :A100 B-90 THRU B-92, B-94 THRU B-247A100 B-90 THRU B-92, B-94 THRU B-247B100 BE-1 THRU BE-91C90 LJ-569 THRU LJ-910E90 LW-28 THRU LW-334SI NO. 0979, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL VENTILATION OUTLETS AT THE SIDES OF THEGLARESHIELD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 9MEN : 1 (MAN)

100-5015-1 SWINDOW PANE, POLARIZED - SPARES ATA :100, A100 B-1 AND AFTER200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTER90, A90, B90, C90 LJ-1 THRU LJ-568 WITH KIT 90-4065 P OR -1

P INSTALLEDB100 BE-1 AND AFTERC90 LJ-569 THRU LJ-1062E90 LW-1 AND AFTERF90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT POLARIZEDWINDOW.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : N/A

100-5016-1 SINSULATION RETAINER, HEAT EXCHANGER ATA :A100 B-234 THRU B-247B100 BE-1 THRU BE-89C90 LJ-719 THRU LJ-905E90 LW-229 THRU LW-334F90 LA-2 THRU LA-41SI NO. 1178, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INSULATION RETAINER TO REDUCE THEPOSSIBILITY OF HEAT EXCHANGER EXHAUST DUCTS BECOMING BLOCKED BY LOOSE INSULATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A


KIT CATALOG

100-5017-1 SFIRE DETECTOR, ENGINE - SPARES ATA :100 AND A100 B-1 THRU B-22490, A90, B90, C90 LJ-38 THRU LJ-669E90 LW-1 THRU LW-150THIS KIT PROVIDES A SPARES REPLACEMENT FIRE DETECTOR FOR P/N 30-215.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT, KIT CHANGES ALL SIX DETECTORS, 3 PER ENGINE. YOU CANNOT MIX OLD AND NEW DETECTORS AND MAINTAIN THE OVERALL RELIABILITY OF THESYSTEM.


100-5018-1AIR CONDITIONER R134A COMPRESSOR ASSEMBLY ATA :C90, C90A LJ-982 THRU LJ-1408THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE A FAILED R12 COMPRESSOR ONANY AIRCRAFT THAT HAS ALREADY HAD A 90-5077-1 KIT INSTALLED OR FOR ANY REASON DESIRES TOCHANGE THE COMPRESSOR TO AN R134A COMPRESSOR IN CONJUNCTION WITH THE INSTALLAT

NOTENOTENOTENOTE:::: 90-555039-5 COMPRESSOR ASSEMBLY MAY BE USED IN LIEU OF 100-555059-25COMPRESSOR ASSEMBLY IF EXISTING COMPRESSOR HOSES ARE REMOVED ANDREPLACED WITH 100-555061-25 AND 100-555061-27 COMPRESSOR HOSES.


100-5018-3SPARE COMPRESSOR, AIR CONDITIONER ATA :ALL MODEL 100’SC90, C90A LJ-982 THRU LJ-1408 WHICH HAVE

INSTALLED 90-5081THIS KIT PROVIDES COMPONENTS AND INFORMATION TO REPLACE THE COMPRESSOR IN THE AIRCONDITIONING SYSTEM OF ALL INSERVICE AIRCRAFT.




KIT CATALOG

100-5018-5SPARE COMPRESSOR, AIR CONDITIONER ATA :ALL MODEL 100’SC90, C90A LJ-982 THRU LJ-1408 WHICH HAVE R-12

REFRIGERANTTHIS KIT PROVIDES COMPONENTS AND INFORMATION TO REPLACE THE COMPRESSOR IN THE AIRCONDITIONING SYSTEM OF ALL INSERVICE AIRCRAFT.



100-9008-1 SENGINE FUEL DRAIN COLLECTOR ATA :90, A90, B90, C90 LJ-1 THRU LJ-641SI NO. 0673-282, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FUEL DRAIN COLLECTOR SYSTEM TOCATCH FUEL DUMPED DURING ENGINE SHUTDOWN AND RETURN IT TO THE FUEL SYSTEM. THISMODIFICATION IS MANDATORY IN COMPLIANCE WITH ENVIRONMENTAL PROTECTION AGENCYREQUIREMENTS SWT. CHANGE : WT: 10.3 LBS @ 98 ARMEST. MAN/HRS: : 8MEN : N/A

100-9008-3 SENGINE FUEL DRAIN COLLECTOR ATA :100, A100 B-1 THRU B-206E90 LW-1 THRU LW-123WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-9011-1 SENGINE CHIP DETECTOR ATA :100, A100 B-1 THRU B-22390, A90, B90, C90 LJ-1 THRU LJ-672E90 LW-1 THRU LW-154SI NO. 0733-257, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CHIP DETECTOR AND TEST POINTS TODETECT METAL PARTICLES IN THE OIL. (ONE KIT IS REQUIRED FOR EACH ENGINE).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

100-9011-3 SENGINE CHIP DETECTOR ATA :100, A100 B-1 THRU B-22390, A90, B90, C90 LJ-1 THRU LJ-672E90 LW-1 THRU LW-154SI NO. 0733-257, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CHIP DETECTOR (NOT FURNISHED WITHTHIS KIT) TO DETECT METAL PARTICLES IN THE OIL. (ONE KIT IS REQUIRED FOR EACH ENGINE).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : N/A

100-9012-1 SOIL HOSE ASSEMBLY - SPARES ATA :A100 B-96 THRU B-212E90 LW-1 THRU LW-130THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR130F006-12D-0220-180, 156F115-12D-0220 OR 41F11180-12D-0220 HOSES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A

100-9013-1 SCHIP DETECTOR WARNING, IMPROVED ATA :100, A100 B-1 THRU B-22890, A90, B90, C90 LJ-1 THRU LJ-691E90 LW-1 THRU LW-164SI NO. 0733-257, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO ADD AN ANNUNCIATOR PANEL WARNING LIGHT TO THECHIP DETECTOR INSTALLATION FOR IMPROVED OIL CONDITION MONITORING. AIRPLANES WITHOUT CHIPDETECTORS WILL REQUIRE INSTALLATION OF KIT 100-9011-1 S OR 100-9011-3 S FOR EWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 25MEN : N/A


KIT CATALOG

100-9014-1 SIGNITION SPARK ATA :100, A100 B-1 THRU B-247C90 LJ-586 THRU LJ-667, LJ-670 WITH KIT

90-9066-1 S INSTALLED (CONVERTSPT6A-20A TO A PT6A-21 ENGINE.), LJ-668,LJ-669, LJ-671 THRU LJ-916

E90 LW-1 THRU LW-337THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SPARK IGNITION ON AIRPLANES EQUIPPEDWITH PT6A-21, -27 OR -28 ENGINES (1 KIT PER AIRCRAFT).

NOTENOTENOTENOTE:::: KIT CONSISTS OF IGNITION EXITERS, IGNITERS, CABLE ASSEMBLIES, IGNITIONCONNECTOR PLUGS, BRACKET ASSEMBLIES, BRACKETS, KIT DRAWING, P AND WSERVICE BULLETIN AND REQUIRED HARDWARE TO COMPLETE THE INSTALLATION.

NOTENOTENOTENOTE:::: FOR MODEL 90S YOU WILL HAVE TO ORDER FOLLOWING ITEMS NOT FURNISHED WITHKIT: MS3456L12S3S CONNECTOR AND 2 EACH MS3417-12N BACK SHELLS FORELECTRICAL PLUG.

WT. CHANGE : MODEL 90S: WT: 3 LB.; ARM: 105 IN.; MOMENT: 315 IN.-LBS MODELS 100: WT: 3 LB.; ARM: 135 IN.; MOMENT:405 IN.-LBS

EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

100-9015-1 PFIRE EXTINGUISHER, ENGINE ATA :B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE FIRE EXTINGUISHER SYSTEM ONBOTH ENGINES.WT. CHANGE : WT: 27.41 LBS @ 166.3 ARMEST. MAN/HRS: : 80MEN : N/A

100-9019-1 SBLEED AIR WARNING PRESSURE SWITCH - SPARES ATA :100 B-2 THRU B-93, EXCEPT B-90, B-91,B-92B90 LJ-318 THRU LJ-501SI NO. 0604-160 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED FLAP DRIVE SYSTEM,COMPLETE WITH FLEX DRIVE SHAFTS, ACTUATORS, DRIVE MOTOR AND GEARBOX.WT. CHANGE : 90, A90, B90 AND C90: WT: 1 LBS @ 190 ARM

100 AND A100: WT: 1 LBS @ 220 ARMEST. MAN/HRS: : 40MEN : N/A


KIT CATALOG

101-1200-1 SMAIN SPAR INSPECTION ACCESS COVER ATA :300 FA-1 THRU FA-230300 (FAA) FF-1 THRU FF-19A200CT (C12D/C12F) BP-46 THRU BP-63A200CT (RC12) FE-1 THRU FE-9B200 BB-1158,BB-1167, BB-1193 THRU BB-1512B200C BL-124 THRU BL-141B200C (C12F) BL-73 THRU BL-112, BL-118 THRU BL-123B200C/CT (UC12/RC12) BU-1 THRU BU-12B200T BT-31 THRU BT-38B300 FL-1 THRU FL-127B300C FM-1 THRU FM-8B300C (CS) FN-1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ACCESS COVER ON THELOWER INBOARD SIDE OF EACH NACELLE AND MAKE A CUTOUT IN THE FAIRING ANGLE WHICH WILLALLOW INSPECTION OF THE LOWER MAIN SPAR CAP IN THIS AREA, ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 45MEN : N/A

101-1202-1 SWING TO FUSELAGE ADAPTER, REINFORCEMENT ATA :300 (FAA) FF-1 THRU FF-19B300 FL-1 THRU FL-177THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A REINFORCEMENT ON THEWING TO FUSELAGE ADAPTER FOR IMPROVED FATIGUE CHARACTERISTICS ON INSERVICE AIRCRAFT:

NOTENOTENOTENOTE:::: EA9309 QT OR EC2216 SEALER REQUIRED, BUT NOT PART OF KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


101-2001-1 SINTERIOR PLACARD ATA :200, B200 BB-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERB200C, B200C BL-1 AND AFTERB200C, B200C BL-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-2002-1 SEXTERIOR PLACARD ATA :200, B200 BB-1 AND AFTER200C, B200C BL-1 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

101-2003-1 SEXTERIOR PLACARD ATA :300 FA-88 AND AFTERB200 BB-1243 AND AFTERB200C BL-127 AND AFTERB200CT BN-5 AND AFTERB200T BT-31 AND AFTERC90A LJ-1138 AND AFTERF90 LA-237 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEMENT FOR THE 101-531347-1PLACARD. PAINT IS NOT INCLUDED IN THE KIT. PURCHASE RED P/N 2351.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-2004-1 SEXTERIOR PLACARD ATA :300 FA-1 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERTHIS KIT PROVIDES EXTERIOR PLACARDS FOR INSTALLATION ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THERE IS NO INTERIOR PLACARD KIT FOR MODEL 300 OR 350.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

101-3027-1 PFLOODLIGHT, EMPENNAGE ATA :200 BB-36 THRU BB-452200T BT-1 THRU BT-4THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TAIL LOGO ILLUMINATION LIGHTS.WT. CHANGE : N/AEST. MAN/HRS: : 16 TO 24MEN : N/A


KIT CATALOG

101-3027-5 PFLOODLIGHT, EMPENNAGE ATA :200, B200 BB-453 THRU BB-1129200C, B200C BL-1 THRU BL-68200C, B200C BL-1 THRU BL-68200CT, B200CT BN-1 THRU BN-4200T, B200T BT-5 THRU BT-29THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TAIL LOGO ILLUMINATION LIGHTS.WT. CHANGE : N/AEST. MAN/HRS: : 16 TO 24MEN : N/A

101-3034-1 PAIR CONDITIONING REAR EVAPORATOR ATA :200 BB-3 THRU BB-417, BB-449 EXCEPT BB-310,

BB-343, BB-383, BB-415, BB-416THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ADDITIONAL AIR CONDITIONEREVAPORATOR AND BLOWER FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 838 TAPE, REFRIGERANT AND OIL NOT SUPPLIED WITH THIS KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 38 LBS; ARM: 214; MOMENT: 8132 IN.-LBSEST. MAN/HRS: : 60MEN : N/A

101-3034-3 PAIR CONDITIONING REAR EVAPORATOR ATA :200 BB-310, BB-343, BB-383, BB-415, BB-416,

BB-418 AND AFTER EXCEPT BB-449300 FA-1 THRU FA-230THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ADDITIONAL AIR CONDITIONEREVAPORATOR AND BLOWER FOR INSERVICE AIRCRAFT.


WT. CHANGE : WT: + 38 LBS; ARM: F.S. 214; MOMENT: + 8132 IN.-LBSEST. MAN/HRS: : 60MEN : N/A

101-3034-5 PAIR CONDITIONING REAR EVAPORATOR ATA :200C, 200CT, B200C, B200CT, 300CTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ADDITIONAL AIR CONDITIONEREVAPORATOR AND BLOWER FOR INSERVICE AIRCRAFT.


WT. CHANGE : WT: + 38 LBS; ARM: F.S. 214; MOMENT: + 8123 IN.-LBSEST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

101-3034-7 PAIR CONDITIONING REAR EVAPORATOR ATA :B200, B200T, B200C, B200CT, 300, 300CTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ADDITIONAL AIR CONDITIONEREVAPORATOR AND BLOWER FOR INSERVICE AIRCRAFT WHICH HAVE AN AFT ELECTRIC HEATER BUT NOAFT AIR CONDITION.


WT. CHANGE : WT: + 38 LBS; ARM: F.S. 214; MOMENT: 8132 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3035-1 SSTATIC NOISE REDUCTION, PRECIPITATION, WING ATA :200 BB-2 THRU BB-297, BB-300 THRU BB-306SI NO. 0944 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REDUCE THE PRECIPITATION STATIC NOISE IN THEVHF FREQUENCY RANGE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

101-3039-1 SEMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH ATA :200 BB-2 THRU BB-659200C BL-1 THRU BL-8200T BT-1 THRU BT-15A100 B-103, B-106 THRU B-247B100 BE-1 THRU BE-90C90 LJ-548 THRU LJ-901E90 LW-1 THRU LW-333F90 LA-2 THRU LA-39SI NO. 1139, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REMOTE SWITCH FOR THE TR70-13 E.L.T.(E.L.T. AND BATTERY PACK ARE NOT PART OF THIS KIT)WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : N/A


KIT CATALOG

101-3042-1 SEXTERNAL POWER OVERVOLTAGE SENSOR ATA :100, A100 B-1 THRU B-240200 BB-2 THRU BB-363200T BT-1 THRU BT-3B100 BE-1 THRU BE-40C90 LJ-502 THRU LJ-772E90 LW-1 THRU LW-277THIS KIT PROVIDES PARTS AND INFORMATION TO ADD AN OVERVOLTAGE SENSOR TO PROTECTONBOARD CIRCUITS AND INSTRUMENTS DURING EXTERNAL POWER OPERATIONS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3043-7 PSTARTER GENERATOR, 300 AMP ATA : 27200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 300 AMP STARTER-GENERATORS. STARTER-GENERATORS INCLUDED IN KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3043-9 PSTARTER GENERATOR, 300 AMP ATA : 27200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 300 AMP STARTER-GENERATORS. (THIS KITDOES NOT PROVIDE GENERATORS, BUT IS COMPATIBLE WITH 23085-001 STARTER-GENERATORS).WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3044-1 SFLAP SWITCH, ASYMMETRICAL ATA :200 BB-2 THRU BB-424200T BT-1 THRU BT-4SI NO. 1121 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ASYMMETRICAL FLAP SWITCHES.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

101-3044-3 SFLAP LIMIT AND WARNING SWITCHES, IMPROVED ATA :200 BB-188 THRU BB-224, BB-226 THRU BB-259,

BB-261 THRU BB-294, BB-296 THRU BB-367,BB-369 THRU BB-398, BB-400, BB-402 THRUBB-430, BB-432 THRU BB-462, BB-464 THRUBB-503, BB-505 THRU BB-537, BB-539 THRUBB-546

200C BL-1 THRU BL-3200T BT-3 THRU BT-8SI NO. 1121 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED FLAP LIMIT AND WARNINGSWITCH.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

101-3044-5 SFLAP LIMIT AND WARNING SWITCHES, IMPROVED ATA :200 BB-225, BB-260, BB-295, BB-368, BB-399,

BB-401, BB-431, BB-436, BB-504 AND BB-538200T BT-1SI NO. 1121 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED FLAP LIMIT AND WARNINGSWITCH. (FRENCH MODIFICATION ONLY)WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : N/A

101-3060-1 SELEVATOR TRIM SWITCH - SPARES ATA :200, B200 BB-2 THRU BB-806200C BL-1 THRU BL-23200T BT-1 THRU BT-20C90 LJ-698 THRU LJ-1008E90 LW-185 THRU LW-347F90 LA-2 THRU LA-113THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELEVATOR TRIM SWITCH AS A SPARESREPLACEMENT FOR THE S229-33F4, S229-33F4/C1410 AWW-B327 OR S229-33F4/C2750CXG SWITCHES.WT. CHANGE : N/AEST. MAN/HRS: : 2.5MEN : N/A


KIT CATALOG

101-3060-3 SYAW DAMPER SWITCH - SPARES ATA :100, A100 B-1 THRU B-247C90 LJ-698 THRU LJ-1008E90 LW-185 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A YAW DAMPER SWITCH AS A SPARESREPLACEMENT FOR THE S229-33F4, S229-33F4/C1410 AWW-B327 OR S22933F4/C2750CXG SWITCHES.WT. CHANGE : N/AEST. MAN/HRS: : 2.5MEN : N/A

101-3062-1 SSWITCH GUARD, E.L.T. ATA :200 BB-2 THRU BB-659200C BL-1 THRU BL-8200T BT-1 THRU BT-15A100 B-103, B-106 THRU B-247B100 BE-1 THRU BE-90C90 LJ-548 THRU LJ-901E90 LW-1 THRU LW-333F90 LA-2 THRU LA-39THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REMOTE SWITCH GUARD ON AIRPLANESEQUIPPED WITH A TR70-13 E.L.T. AND REMOTE SWITCH KIT 101-3039-1 S INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : N/A

101-3063-1 PRECOGNITION LIGHT, WING TIP ATA :200 BB-1 AND AFTERB90 LJ-501 AND AFTERE90 LW-1 AND AFTERF90 LA-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WING TIP RECOGNITION LIGHTON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT FURNISH REPLACEMENT LENS COVER, REMOVE OLD WING TIP LENSCOVER, INSTALL KIT DETAILS AND REINSTALL ORIGINAL OLD LENS COVER.

WT. CHANGE : B90, C90 & E90: WT: + 1.70 LBS; ARM: 149.4; MOMENT: + 254.0 IN.-LBS200: WT: 1.70 LBS; ARM: 177.7; MOMENT: 302.0

EST. MAN/HRS: : 12 TO 16MEN : N/A


KIT CATALOG

101-3063-3 PRECOGNITION LIGHT, WING TIP ATA :THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WING TIP RECOGNITION LIGHTON INSERVICE AIRCRAFT.



WT. CHANGE : WT: 1.2 LBS;. ARM: 174.2; MOMENT: 209EST. MAN/HRS: : 12 TO 16MEN : N/A

101-3063-7 PRECOGNITION LIGHT, WING TIP ATA :F90 LA-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WING TIP RECOGNITION LIGHTON INSERVICE AIRCRAFT.


WT. CHANGE : WT: 1.12 LBS;. ARM: 145.2; MOMENT: 163.0EST. MAN/HRS: : 12 TO 16MEN : N/A

101-3064-1 SAIR CONDITIONER PC BOARD ATA :200 BB-1 THRU BB-687, BB-689 THRU BB-728200C BL-1 THRU BL-11200CT BN-1200CT BN-1200T BT-1 THRU BT-16, BT-18THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN R-12 REFRIGERANT PRESSURE CONTROLPRINTED CIRCUIT BOARD IN LIEU OF EXISTING 7.5 AMP FUSE PRINTED CIRCUIT BOARD.

NOTENOTENOTENOTE:::: INCORPORATION OF SERVICE INSTRUCTION NO. 0968 AND 0820-410 OR SUBSEQUENTAND PART I OF SERVICE INSTRUCTION NO. 0756-426 OR SUBSEQUENT SHOULD BEACCOMPLISHED IN CONJUNCTION WITH THE INSTALLATION OF THIS KIT.



KIT CATALOG

101-3064-3 SAIR CONDITIONER ACCESS DOOR MODIFICATION ATA :200, B200 BB-2 THRU BB-1157, BB-1159 THRU

BB-1166, BB-1168 THRU BB-1192200C, B200C BL-1 THRU BL-72200CT, B200CT BN-1 THRU BN-4200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30THIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE A HOLE IN THE CONDENSER SECTIONACCESS DOOR TO VIEW THE RECEIVER DRYER SIGHT GLASS WITHOUT REMOVING THE ACCESS DOOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3069-1 SLANDING GEAR MOTOR CIRCUIT BREAKER ATA :200, B200 BB-2, BB-6 THRU BB-1157, BB-1159 THRU

BB-1166, BB-1168 THRU BB-1192, EXCEPTBB -1158, BB-1167

200C, B200C BL-1 THRU BL-72200C, B200C BL-1 THRU BL-72200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30SB NO. 2035 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LANDING GEAR MOTOR CIRCUIT BREAKER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A

101-3069-3 SLANDING GEAR MOTOR CIRCUIT BREAKER ATA :A100 B-231 THRU B-237B100 BE-17 THRU BE-137SB NO. 2035 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LANDING GEAR MOTOR CIRCUIT BREAKER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : N/A

101-3069-7LANDING GEAR MOTOR CIRC BRKR ATA : 32"MANDATORY" SB 2035, REV 3WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-3069-7 SKIT"S"L/G MTR CB ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-3072-1 SAVIONICS BLOWER ATA :300 FA-2 THRU FA-17B200 BB-1089 THRU BB-1203B200C BL-70 AND BL-71SB NO. 2043 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK THE COOLING SYSTEM AND INSTALL ANADDITIONAL BLOWER FAN ON AIRPLANES EQUIPPED WITH COLLINS E.F.I.S. AVIONICS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : N/A

101-3076-1 SLANDING GEAR CIRCUIT PROTECTION, HYDRAULIC ATA :B200 BB-1158, BB-1167, BB-1193 THRU BB-1206SB NO. 2043 OR SUBSEQUENTTHIS KIT CONTAINS PARTS AND INFORMATION TO MODIFY THE LANDING GEAR SYSTEM TO PROTECTTHE LANDING GEAR MOTOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3077-1 SLANDING GEAR CIRCUIT PROTECTION, HYDRAULIC ATA :300 FA-1, FA-3 THRU FA-5, FA-7 THRU FA-9,

FA-11, FA-12, FA-14 THRU FA-22SB NO. 2046 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE LANDING GEAR SYSTEM TO PROTECTTHE LANDING GEAR MOTOR.WT. CHANGE : N/AEST. MAN/HRS: : 10MEN : N/A

101-3078-1 SRUDDER BOOST AND BRAKE DEICE WIRING ATA :300 FA-3, FA-4, FA-9, FA-11, FA-12, FA-15 THRU

FA-21SB NO. 2048 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO RECONFIGURE THE BRAKE DEICE ELECTRICAL WIRINGTO ALLOW IMPROVED OPERATION OF THE RUDDER BOOST WHEN THE BRAKE DEICE IS ON.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : N/A


KIT CATALOG

101-3086-1 SSTARTER GENERATOR - SPARES ATA : 24200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERKING AIR: 200/300 COMMUNIQUE NO. 49THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE100-389014-5 STARTER-GENERATOR. ONE GENERATOR PER KIT.

NOTENOTENOTENOTE:::: DUE TO CHANGES IN STARTING PROCEDURES, BOTH STARTER-GENERATORS MUST BECHANGED AT THE SAME TIME.


101-3087-1 SRUDDER BOOST SYSTEM WIRING ATA :300 FA-6 THRU FA-12, FA-14 THRU FA-23, FA-25,

FA-27, FA-28, FA-30, FA-32 THRU FA-36SB NO. 2080 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO ALLOW THE RUDDER BOOST SYSTEM TO REMAINFUNCTIONAL WHEN THE AUTOPILOT/TRIM DISCONNECT SWITCH IS ACTIVATED TO THE SECOND LEVEL.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : N/A

101-3087-3 SRUDDER BOOST SYSTEM WIRING ATA :300 FA-3 THRU FA-5SB NO. 2080 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO ALLOW THE RUDDER BOOST TO REMAIN FUNCTIONALWHEN THE AUTOPILOT/TRIM DISCONNECT SWITCH IS ACTIVATED TO THE SECOND LEVEL.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : N/A

101-3093-1 SBEACON, UPPER FLASHING ATA :200 BB-2 THRU BB-33THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AS AREPLACEMENT FOR THE GRIMES ROTATING BEACON.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-3100-1 SELECTRIC HEAT EQUI ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-3101-1 SELECTRIC HEAT EQUIPMENT ATA :300 FA-2 THRU FA-116SB NO. 2184 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INCREASE ENVIRONMENTAL HEAT OUTPUT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

101-3106-1 PHYD LDG RELAY ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-3106-1 SHYDRAULIC LANDING GEAR MOTOR RELAY - SPARES ATA :300 FA-1 AND AFTERSB NO. 2226, REV. 2 OR SUBSEQUENTTHIS KIT CONTAINS PARTS AND INFORMATION TO INSTALL THE HYDRAULIC LANDING GEAR MOTORRELAY.WT. CHANGE : N/AEST. MAN/HRS: : 7MEN : 1 (MAN)

101-3106-3 SHYDRAULIC LANDING GEAR MOTOR RELAY ATA :300 FF-1 THRU FF-17.SB NO. 2226, REV. 2 OR SUBSEQUENTTHIS KIT CONTAINS PARTS AND INFORMATION TO INSTALL THE HYDRAULIC LANDING GEAR MOTORRELAY.WT. CHANGE : N/AEST. MAN/HRS: : 7MEN : 1 (MAN)

101-3107-1 PHYD LDG RELAY ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-3107-1 SHYDRAULIC LANDING GEAR MOTOR RELAY ATA :B200 BB-1158, BB-1167, BB-1193 AND AFTERB200C BL-73 AND AFTERB200C BL-73 AND AFTERB200CT BN-5 AND AFTERB200T BT-31 AND AFTERSB NO. 2226, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE HYDRAULIC LANDING GEAR MOTORRELAY.WT. CHANGE : N/AEST. MAN/HRS: : 3.5MEN : N/A

101-3111-1 SFUEL QUANTITY INDICATOR ATA :C90, C90A, E90, F90, H90 (T-44A), A100,B100, 200, 200C, 200T, 200CT, A200C(UC-12B), B200, B200C, B200C (UC-12F),B200T, B200CT, 300THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE 100-380006-47, 101-384150-7AND 101-384151-5 FUEL QUANTITY INDICATORS WITH A 117-384019-3 INDICATOR.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS TO REPLACE ONE FUEL QUANTITY INDICATOR.WT. CHANGE : N/AEST. MAN/HRS: : 6 TO 8MEN : N/A

101-3118-1 SEXTERNAL DC POWER REVERSE POLARITY PROTECTION ATA :300 FA-2 AND AFTER300 (FAA) FF-1 THRU FF-19C90A LJ-1063 AND AFTERC90A LJ-1063 AND AFTERF90 LA-202, LA-205 AND AFTERTHIS KIT CONSIST OF PARTS AND INFORMATION TO ADD EXTERNAL POWER REVERSE POLARITYPROTECTION.WT. CHANGE : N/AEST. MAN/HRS: : 18MEN : N/A

101-3121-1 SDEICE BOOT REPLACEMENT ATA :300, 300CTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE 4E2575-7 DEICE BOOT AND 3E2017-8 WIREHARNESS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-3127-1 SEMERGENCY LOCATOR TRANSMITTER - SPARES ATA :THIS KIT IS NO LONGER AVAILABLE DUE TO NOT MEETING THE REQUIREMENTS OF TSO C-91A. SEE KIT101-3214-1. FACTORY INSTALLED SYSTEMS ARE MANUFACTURED BY ARTEX, INC. AND CAN BECONTACTED FOR PRICING AND AVAILABILITY OF AN ELT KIT WHICH WILL REQUIRE A LOCAL APPRWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3133-1 SKIT LANDING GEAR MOTOR CIRCUIT BRKR INST ATA : 32A200 BJ-1 THRU BJ-66, BP-1, BP-22, BP-24 THRU

BP-45, BP-7 THRU BP-11A200CT GR-1 THRU GR-19 & FC-1 THRU FC-3"MANDATORY" SB 2036, REV 3WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-3134-1 PANTENNA CARGO POD ATA :300 BB-1296, BB-1302, BB-1304, BB-1305,

BB-1309, BB-1314, BB-1338 THRU BB-1343THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CHANGE COAX ROUTING TO ANTENNASWITH EXTENDED BAGGAGE POD ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT WORKS WITH KIT 101-4053 AND WILL NOT WORK ALONE.WT. CHANGE : TO COMPLIANCE WITH FAR 23.25/CAR 3.74EST. MAN/HRS: : 4MEN : N/A

101-3142-1 SSTATIC INVERTER RELOCATION, CAA CERTIFICATION ATA :B300 FL-17 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE EXISTING STATIC INVERTORS ONINSERVICE AIRCRAFT WITHOUT FLIGHT DATA RECORDERS INSTALLED AS REQUIRED BY WORK ORDER.WT. CHANGE : WT: 2.5 LBS @ 212.4EST. MAN/HRS: : 18 TO 24MEN : N/A

101-3142-5 SSTATIC INVERTERS RELOCATION FOR CAA CERTIFICATION ATA :B300 FL-66 AND AFTER WITH A FLIGHT DATA

RECORDER INSTALLED AS REQUIRED BYWORK ORDER

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE EXISTING STATICINVERTERS ON INSERVICE AIRCRAFT.WT. CHANGE : WT: 2.5 LBS @ 212.4EST. MAN/HRS: : 18 TO 24MEN : 1 (MAN)


KIT CATALOG

101-3143-1 SFLAP SWITCH, UNITED KINGDOM REGULATIONS ATA :B300 FL-17 AND AFTERB300C FM-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLAP SWITCH AND GATE ALONG WITHPEDESTAL MODIFICATIONS TO COMPLY WITH BCAR 23.697 (D) FOR KING AIR 350’S SOLD UNDER UNITEDKINGDOM REGULATIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

101-3144-1 SEMERGENCY LIGHT SWITCH AND CIRCUIT BREAKER ATA :B300 FL-17 AND AFTER AS REQUIRED BY WORK

ORDERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR THE INSTALLATION OF EMERGENCYEXIT SIGNS TO COMPLY WITH CAA REGULATIONS FOR U.K. CERTIFICATION OF INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AIRCRAFT SERIAL NUMBER IS REQUIRED TO INSURE KIT AND AIRCRAFT WORK ORDERSYSTEM ARE IN AGREEMENT.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : N/A

101-3148-1 SWIRING MODIFICATION - B300 - UNITED KINGDOM CERTIFICATION ATA :B300 FL-17 AND AFTER AS REQUIRED BY WORK

ORDERB300C FM-2 AND AFTER AS REQUIRED BY WORK

ORDERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY REGARDING THE INSTALLATION OF WIRINGCHANGES REQUIRED FOR AIRCRAFT TO COMPLY WITH CAA REGULATIONS ON INSERVICE AIRCRAFT.


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 120 TO 160MEN : 2 (MEN)

101-3149-1 SANNUNCIATOR MODIFICATION, CAA ATA :B300 FL-17 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO REVISE ANNUNCIATOR LEGENDS AND REPLACECIRCUIT CARD ASSEMBLY - ANN CONTROL - IN ORDER TO COMPLY WITH CAA REGULATIONS FORINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : N/A


KIT CATALOG

101-3149-3ANNUNCIATOR MODIFICATION, UK ATA :B300 FL-163 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO REVISE ANNUNCIATOR LEGENDS AND REPLACECIRCUIT CARD ASSEMBLY - ANN CONTROL IN ORDER TO COMPLY WITH CAA REGULATIONS FORINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3150-7 SCIRCUIT BREAKER PANEL ATA :B300 (350) FL-66 AND AFTERTHIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION REGARDING THE INSTALLATION OFCIRCUIT BREAKER.

NOTENOTENOTENOTE:::: THIS KIT IS FOR UK CERTIFICATION OF AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 2MEN : N/A

101-3151-1 SBATTERY BUS CHANGE ATA :B300 FL-17 AND AFTER AS REQUIRED BY WORK

ORDERB300C FM-2 AND AFTER AS REQUIRED BY WORK

ORDERTHIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE INSTALLATION OF NEW BATTERY HOLDDOWN ASSEMBLIES AND BATTERY INSULATOR STRIPS TO ISOLATE THE BATTERY FROM THE AIRCRAFTSTRUCTURE, REPLACEMENT OF THE K135 RELAY AND CB154 CIRCUIT BREAKER, AND THE ADDITI



101-3154-1 SSMOKE DETECTOR AND E/L PANEL ATA :B300 FL-17 AND AFTERB300C FM-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE INSTALLATION OF SMOKE DETECTORAND EDGELIGHTED PANEL ASSEMBLY AS REQUIRED BY WORK ORDER.

NOTENOTENOTENOTE:::: EC2216A/B SEALER IN QUART CONTAINER AND EC1781 QT ADHESIVE IS REQUIRED, BUTARE NOT PART OF KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.

WT. CHANGE : WT: ARM: MOMENT: + 459 IN. LBSEST. MAN/HRS: : 2 TO 4MEN : N/A


KIT CATALOG

101-3155-1 SCURRENT SENSOR, U.K. CERTIFICATION ATA :B300 FL-17 AND AFTERB300C FM-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE INSTALLATION OF TWO CURRENTSENSORS ON INSERVICE AIRCRAFT AS REQUIRED BY WORK ORDER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : N/A

101-3157-1 SSTALL WARNING MODIFICATION, CAA CERTIFICATION, U.K. ATA :B300 FL-17 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE STALL WARNING COMPUTER IN ORDERTO COMPLY WITH CAA REGULATIONS FOR INSERVICE AIRCRAFT AS REQUIRED BY WORK ORDER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

101-3158-1 SATTITUDE TRANSFORMER ATA :B300 FL-1, FL-11, FL-18, FL-20, FL-21, FL-25,

FL-27, FL-29, FL-32, FL-35 THRU FL-37,FL-47

"MANDATORY" SB NO. 2423THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A SINGLE APC-65HAUTOPILOT COMPUTER, AND/OR 3 TUBE EFIS-85 (14) WITH ATTITUDE TRANSFORMER.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

101-3158-3 SATTITUDE TRANSFORMER ATA :B300 FL-2 THRU FL-6, FL-8, FL-12, FL-13, FL-15

THORUGH FL-17, FL-19, FL-22 THRU FL-24,FL-30, FL-33, FL-38 THRU FL-41, FL-43 THRUFL-46, FL-50, FL-51, FL-53, FL-55 THRUFL-57

"MANDATORY" SB NO. 2423THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A SINGLE APC-65HAUTOPILOT COMPUTER, AND/OR 3 TUBE EFIS-85 (14) WITH ATTITUDE TRANSFORMER.



KIT CATALOG

101-3158-5 SATTITUDE TRANSFORMER ATA :B300 FL-7, FL-9, FL-14, FL-26, FL-28B300C FM-1 AND AFTER"MANDATORY" SB NO. 2423THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A SINGLE OR DUAL APC-65HAUTOPILOT COMPUTER, AND/OR 3 OR 5 TUBE EFIS-85 (14) WITH ATTITUDE TRANSFORMER.


101-3159-1 SATTITUDE TRANSFORMER ATA :B200 BB-1349 THRU BB-1352, BB-1372, BB-1377,

BB-1380, BB-1395 AND BB-1397"MANDATORY" SB NO. 2423THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A SINGLE APC-65HAUTOPILOT COMPUTER, AND/OR 3 TUBE EFIS-85 (14) WITH ATTITUDE TRANSFORMER.


101-3165-1 SSWITCH, G OVERHEAD FUEL PANEL ATA :A200 (C-12A) BC-1 THRU BC-61, BD-1 THRU BD-30A200 (C12C) BC-62 THRU BC-75A200CT (C12D) BP-1, BP-22, BP-24 THRU BP-51A200CT (FWC-12D) BP-7 THRU BP-11A200CT (RC-12D) GR-1 THRU GR-13A200CT (RC-12G) FC-1 THRU FC-3A200CT (RC-12H) GR-14 THRU GR-19A200CT (RK-12K) FE-1 THRU FE-15B200C (C-12F) BP-64 THRU BP-71B200C (UC-12M) BV-1 THRU BV-12B200CT (FW) FG-1 AND FG-2THIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE REPLACEMENT OF THE FUEL PANEL GSWITCHES ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-3168-1 SEXTERNAL POWER SWITCH MODULE - SPARES ATA :C90, E90, H90, 100, A100, B100, 200, 200C,200T, 200CT, A200, A200C, A200CT, B200,B200C, B200T, B200CTTHIS KIT PROVIDES PARTS AND INFORMATION FOR THE SPARES REPLACEMENT OF THE 101-361045-1 OR-5 OVERVOLTAGE MODULE ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : N/A

101-3169-1 SFUEL QUANTITY INDICATOR REPL INSTL ATA : 28A200, B200C AND A200CT (RC12H)AIRCRAFTTHIS KIT WILL PROVIDES PARTS & INFORMATION NECESSARY TO REPLACE 100-384189-3 FUEL QUANTITYINDICATOR WITH A REPLACEMENT INDICATOR FOR ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS TO REPLACE ONE(1)FUEL QUANTITY INDICATOR ONLY.NOTENOTENOTENOTE:::: FOR MODEL A90-1 & A90-4 (RU-21H) AIRCRAFT WITH 91-380028-13 INDICATOR SEE KIT

101-3169-3 S.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8 HRSMEN : 1 (MAN)

101-3170-1 SANTENNA MARKER BEACON ATA :B90, C90, E90, F90, H90, 100, A100, B100,200, A200, 200C, A200C, 200T, 200CT, B200,B200C, B200T, B200CTTHIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION FOR SPARES REPLACEMENT OF100-384120 MARK BEACON ANTENNA WITH A 101-384179 MARKER BEACON ANTENNA.

NOTENOTENOTENOTE:::: FOR MODELS 1900, 1900C AND 1900C-1 SEE KIT 114-3017-1 S.WT. CHANGE : N/AEST. MAN/HRS: : 10 TO 12MEN : N/A

101-3174-1 SINDICATOR PILOT AIRSPEED ATA :B300 (350) FL-17 THRU FL-102THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE REMOTE MOUNTED OVERSPEED WARNINGSWITCH AND PILOTS AIRSPEED INDICATOR WITH INDICATOR WITH INTERNAL WARNING SWITCH.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : N/A


KIT CATALOG

101-3175-1 SLIGHT, LANDING GEAR POSITION INDICATOR ATA :B200, B200T, B200C, B200CTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE LANDING GEAR POSITIONINDICATOR LIGHT ASSEMBLY P/N 308-607-0843-004 (P/N LF KORRY) WITH A (EATON) INDICATOR LIGHTASSEMBLY ON INSTRUMENT PANEL.

NOTENOTENOTENOTE:::: FOR C90A AIRCRAFT SEE KIT 90-3111-1 S.NOTENOTENOTENOTE:::: FOR MODELS 300, B300 (350) AND B300C (FA, FF, FL AND FM SERIES) SEE 101-3176-1 S.


101-3176-1 SLIGHT, LANDING GEAR POSITION INDICATOR ATA :300, B300 (350), B300C FA, FF, FL AND FMTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE LANDING GEAR POSITIONINDICATOR LIGHT ASSEMBLY P/N 308-607-0843-004 (P/N OF KORRY) WITH A (EATON) INDICATOR LIGHTASSEMBLY ON INSTRUMENT PANEL.

NOTENOTENOTENOTE:::: FOR MODEL B200, B200T, B200C AND B200CT AIRCRAFT SEE KIT 101-3175-1 S.NOTENOTENOTENOTE:::: FOR MODEL C90A AIRCRAFT SEE KIT 90-3111-1 S.


101-3180-1AIRSPEED LIMITATIONS IAS KNOTS ATA :300 (FAA) FF-1 THRU FF-19THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INDICATE AIRSPEED LIMITATIONS ANDWHAT IS REQUIRED TO ALLOW NEW MAXIMUM IAS AIRSPEEDS.

NOTENOTENOTENOTE:::: KIT 101-5084-3 MUST HAVE BEEN INSTALLED ON AIRCRAFT, WHICH INCLUDES THIS KITFOR A REPLACEMENT 101-3180-1 KIT TO BE SOLD SEPARATELY.


101-3181-1 SENGINE AND FATIGUE MONITORING SYSTEM ATA :300 (FAA) FF-1 THRU FF-19THIS DRAWING PROVIDES A LIST OF KITS NEEDED TO ADD ON-BOARD ENGINE AND FATIGUE TRENDMONITORING SYSTEM ON INSERVICE AIRCRAFT.WT. CHANGE : WT: + 44 LBS MOMENT: + 10.560 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-3181-3 SENGINE AND FATIGUE MONITORING SYSTEM ATA :300 (FAA) FF-1 THRU FF-19THIS DRAWING PROVIDES A LIST OF KITS NEEDED TO ADD ON-BOARD ENGINE AND FATIGUE TRENDMONITORING SYSTEM ON INSERVICE AIRCRAFT.WT. CHANGE : WT: + 44 LBS MOMENT: + 10.560 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3186-1 SCIRCUIT BREAKER FUEL CONTROL PANEL ATA :300 (FAA) FF-1 THRU FF-19THIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE INSTALLATION OF CIRCUIT BREAKERSUSED IN CONJUNCTION WITH THE FLIGHT DATA RECORDER ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ONLY INITIALLY AVAILABLE AS PART OF 101-3181 KIT INSTALLATION, PROOF OF 101-3181KIT REQUIRED BEFORE CONSIDERATION OF INDIVIDUAL SALE OF THIS KIT WILL BECONSIDERED.


101-3189-1 SWIRING MODIFICATION COMPLY WITH DUTCH REGULATIONS ATA :B300 (350) FL-80 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE INSTALLATION OF WIRING CHANGES INORDER TO COMPLY WITH DUTCH REGULATIONS FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 100 TO 120MEN : 2 (MEN)

101-3190-1 SANNUNCIATOR LEGENDS MODIFICATION, (DUTCH CERTIFICATION) ATA :B300 (350) FL-80 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REVISE ANNUNCIATOR LEGENDS INORDER TO COMPLY WITH DUTCH REGULATION FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : N/A

101-3191-1 SBATTERY BUS CHANGE (HOLLAND) ATA :B300 (350) FL-80 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE REPLACEMENT OF (K135) RELAY AND(CB154) CIRCUIT BREAKER ON INSERVICE AIRCRAFT FOR CERTIFICATION FOR REGISTRATION INHOLLAND.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 10MEN : N/A


KIT CATALOG

101-3194-1BRACKET CONNECTOR, STRAIN GAGE ATA :300 (FAA) FF-1 THRU FF-19THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED FOR INSTALLATION OF STRAIN GAGES ONAIRCRAFT.

NOTENOTENOTENOTE:::: GAGES ARE NOT PART OF THIS KIT, WHICH ONLY FURNISHES BRACKETS, DUST CAPSAND REQUIRED PLACARDS.

NOTENOTENOTENOTE:::: PRO-SEAL 890 SEALER IS REQUIRED FOR USE BUT NOT PART OF KIT.NOTENOTENOTENOTE:::: ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: EDGE FILL; 87005 QT., ADHESIVE EC2216,

EC2216 A/B QT, OR EC2216A/B 2OZ., AND ADHESIVE 14-31 QT., IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: 207200-1 CONNECTOR REPLACEMENT, EFFECTED SERIAL NUMBERS: BB-385 THRUBB-1406, BL-132 THRU BL-137, FA-169, FA-173 THRU FA-218, FE-18, FE-25 THRU FE-60,LJ-787 THRU LJ-1283, LW-289 AND AFTER.

NOTENOTENOTENOTE:::: 207201-1 CONNECTOR REPLACEMENT, EFFECTED SERIAL NUMBERS: BB-1312, BB-1318,THRU BB-1396, BL-137, FA-169, FA-173, THRU FA-218, FE-1 THRU FE-19, FL-18, FL-25, FL-60,LJ-787 THRU LJ-1273, LW-289 AND AFTER.

NOTENOTENOTENOTE:::: PROOF OF INSTALLATION OF 101-3181 KIT ON AIRCRAFT MUST BE FURNISHED BEFORETHIS KIT CAN BE ORDERED FOR SPARES REPLACEMENT OF SYSTEM DETAILS IN THISKIT FORM.


101-3196-1STRAIN GAGE ACCESS COVER ATA :300 (FAA) FF-1 THRU FF-19THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRAIN GAGE ACCESS COVERS ON FAAAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3202-1BULKHEAD CONNECTOR CHANGE (SPARE FOR 207201-1 AND 207200-1) ATA :C90, C90A, A200, A200C, B200, B200C, 300,B300,THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE AMP FEEDTHRU CONNECTORS, ANDASSOCIATED PLUS, WITH MIL-SPEC CONNECTORS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : N/A


KIT CATALOG

101-3208-1WIRE HARNESS, ENGINE FIRE DETECTOR ATA :B200 BB-1439, BB-1444 THRU BB-1512B200C BL-139, BL-140B200C (C-12F) BW-1 THRU BW-3B200C (C-12R) BW-4 AND BW-5B200T BT-35 THRU BT-38THIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACING THE WIRE ON THE ENGINE FIREDETECTOR, IN ENGINE COMPARTMENT INSERVICE AIRCRAFT:WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3210-1ELT REMOTE SWITCH ATA :200 BB-1463300 FA-222 THRU FA-230B200 BB-1431 THRU BB-1509B200C BL-138 THRU BL-140B200T BT-34 THRU BT-38B300 FL-60 THRU FL-126B300C FM-4 THRU FM-8B300C (CA) FN-1C90A LJ-1305 THRU LJ-1403THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REMOTE (COCKPIT) SWITCH ON INSERVICEEQUIPPED WITH AN ARTEX ELT-110-4-002 OR A 101-343290-17 (ELT-110-4-002 TRANSMITTER WITH A BACDECAL) EMERGENCY LOCATOR TRANSMITTER.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT: APPROPRIATE FLIGHT MANUAL SUPPLEMENT,ALODINE 1200, EA9309NA, AND MIL-S-8802. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.



KIT CATALOG

101-3214-1ELT AND REMOTE SWITCH ATA :100 B-1 THRU B-89, B-93200 BB-2, BB-6 THRU BB-853, BB-872, BB-873,

BB-892, BB-912, BB-893, BB-1463200C BL-1 THRU BL-36200CT BN-1200T BT-1 THRU BT-22, BT-28300 FA-1 THRU FA-230300 (FAA) FF-1 THRU FF-1965-90 LJ-1 THRU LJ-75, LJ-77 THRU LJ-11365-A90 LJ-76, LJ-114 THRU LJ-317A100 B-90 THRU B-92, B-94, B-100 THRU B-247B100 BE-1 THRU BE-137B200 BB-734, BB-793, BB-829, BB-854 THRU

BB-870, BB-874 THRU BB-891, BB-894,BB-896 THRU BB-911, BB-913 THRUBB-1462, BB-1464 THRU BB-1509

B200C BL-37 THRU BL-72, BL-113 THRU BL-117,BL-124 THRU BL-140

B200T BT-23 THRU BT-27, BT-29 THRU BT-38B300 FL-1 THRU FL-126B300C FM-1 THRU FM-8B300C (CA) FN-1B90 LJ-318 THRU LJ-501C90 LJ-502 THRU LJ-1062C90A LJ-1063 THRU LJ-1403E90 LW-1 THRU LW-347F90 LA-2 THRU LA-201,

LA-203, LA-204F90-1 LA-202, LA-205 THRU LA-236THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ARTEX ELT-110-4-002 EMERGENCYLOCATOR TRANSMITTER AND A REMOTE (COCKPIT) SWITCH ON INSERVICE AIRCRAFT EQUIPPED WITH ACOMMUNICATIONS COMPONENTS CORP. TR-70-09, TR-70-13 OR TR-70-17, A NARCO ELT-10, A D

NOTENOTENOTENOTE:::: THE INSTALLATION OF THIS KIT IS NOT COMPLETE UNTIL THE APPROPRIATE FLIGHTSUPPLEMENT HAS BEEN ADDED TO THE EXISTING FLIGHT MANUAL. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: ALODINE 1200 COATING, EA9309NA ADHESIVE, MIL-S-8802 SEALER REQUIRED, BUT NOTFURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY



KIT CATALOG

101-3215-1ELT AND REMOTE SWITCH ATA :A100 (U-21F) B-95 THRU B-99A100-1 BB-3 THRU BB-5A200C (UC-12B) BJ-1 THRU BJ-66B200C (C-12F) BL-73 THRU BL-112, BL-118 THRU BL-123B200C (C-12F) BP-64 THRU BP-71B200C (C-12R) BW-1 THRU BW-3B200C (RC-12F) BU-11, BU-12B200C (RC-12M) BV-11, BV-12B200C (UC-12F) BU-1 THRU BU-10B200C (UC-12M BV-1 THRU BV-10THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ARTEX ELT-110-4-002 EMERGENCYLOCATOR TRANSMITTER AND A REMOTE (COCKPIT) SWITCH ON INSERVICE AIRCRAFT PREVIOUSLYEQUIPPED WITH A COMMUNICATIONS COMPONENTS CORP. TR-70-09, TR-70-13, OR TR-70-17, A NARCO

NOTENOTENOTENOTE:::: THE INSTALLATION OF THIS KIT IS NOT COMPLETE UNTIL THE APPROPRIATE FLIGHTMANUAL SUPPLEMENT HAS BEEN ADDED TO THE EXISTING FLIGHT MANUAL, IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: ALODINE 1200 COATING, EA9309NA ADHESIVE, & MIL-S-8802 SEALER REQUIRED, BUT NOTFURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


101-3215-3ELT AND REMOTESWITCH KIT ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-3227-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN VHS FORMAT.

NOTENOTENOTENOTE:::: ALODINE 600X60GR PROTECTIVE COATING REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


101-3227-3ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN PAL FORMAT.

NOTENOTENOTENOTE:::: ALODINE 600X60GR PROTECTIVE COATING REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3238-1KIT - PITOT HEAT INDICATOR ATA : 34B200 BB-734, BB-793, BB-829, BB-854 THRU

BB-870, BB-874 THRU BB-891, BB-894,BB-896 THRU BB-911, BB-913 THRU BB-990,BB-992 AND AFTER

B200C BL-37 AND AFTERB200CT BN-2 AND AFTERB200T BT-23 THRU BT-27, BT-29 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR PITOT HEAT INDICATOR INSTALLATION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUALAND PILOT'S OPERATING HANDBOOK REVISIONS (OR SUPPLEMENTS) HAVE BEENINCORPORATED. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4-6MEN : 1 (MAN)

101-3259-1WINDSHIELD SCREW 12000 HOUR ATA : 56100, A100, B100200, 200C, 200T, 200CT, B200, B200C,B200T, B200CT300, 300C, B30065-8865-90, 65-A90, B90, C90, C90A, E90THIS KIT PROVIDES SCREWS TO REPLACE EXISTING SCREWS AT THE 12,000 HOUR REPLACEMENTSCHEDULE ON IN-SERVICE AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-3266-1ALTIMETER INSTALLATION ATA : 34B200 BB-1449 THRU BB-1801 AND BL-143 &

AFTER EXCLUDING AIRCRAFT WITH TAKE-OFF GROSS WEIGHT IN EXCESS OF 12,500LBS.

"OPTIONAL" SB NO. 34-3506THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE COPILOT NON ENCODING OR ENCODINGALTIMETER WITH AN ISS (INNOVATIVE SOLUTIONS & SUPPORT) ENCODING ALTIMETER (9D-80130-31) ONIN-SERVICE AIRCRAFT EQUIPPED WITH EFIS-84 FLIGHT INSTRUMENT SYSTEM, ADC-85 A

NOTENOTENOTENOTE:::: "PR1440" SEALER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION (OR SUPPLEMENT) HAS BEENINCORPORATED. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: WT: +22; MOMENT: +1,655 LB-IN.FOR AIRCRAFT EQUIPPED WITH A COPILOT ENCODING ALTIMETERWT: +20; MOMENT: +1,506 LB-IN.FOR AIRCRAFT EQUIPPED WITH A COPILOT NON ENCODING ALTIMETEREST. MAN/HRS: 16 HRS. (1 MAN)

WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-3266-3ALTIMETER INSTALLATION ATA : 34B200 BB-1449 THRU BB-1801 AND BL-143 AND

AFTER EXCLUDING AIRCRAFT WITH TAKE-OFF GROSS WEIGHT IN EXCESS OF 12,500LBS.

"OPTIONAL" SB NO. 34-3506THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE COPILOT NON ENCODING OR ENCODINGALTIMETER WITH AN IS&S (INNOVATIVE SOLUTIONS & SUPPORT) ENCODING ALTIMETER (9D-80130-31) ONIN-SERVICE AIRCRAFT EQUIPPED WITH EFIS-85 FLIGHT INSTRUMENT SYSTEM, ADC-85

NOTENOTENOTENOTE:::: "PR1440" SEALER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION (OR SUPPLEMENT) HAS BEENINCORPORATED. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: WT: +22; MOMENT: +1,655 LB-IN.FOR AIRCRAFT EQUIPPED WITH A COPILOT ENCODING ALTIMETERWT: +20; MOMENT: +1,506 LB-IN.FOR AIRCRAFT EQUIPPED WITH A COPILOT NON ENCODING ALTIMETEREST. MAN/HRS: 16 HRS (1 MAN)

WT. CHANGE : SEE NOTESEST. MAN/HRS: : 16MEN : 1 (MAN)


KIT CATALOG

101-3284-0001TRANSPONDER INSTL, FLIGHT ID-INFO ONLY ATA :B200 BB-1149 & BB-1458 THRU BB-1833, BL-139

THRU BL-147, BN-5 THRU BN-9, & BT-39THRU BT-46

B300 FL-75 THRU FL-380 & FM-4 THRU FM-11,EXCEPT SPECIAL MISSION AIRCRAFTINCLUDED IN THESE SERIALS.

C90A LJ-1306, LJ-1316, LJ-1318 & LJ-1320 &AFTER;

THIS KIT PROVIDES INFORMATION ONLY TO REPLACE THE EXISTING TDR-94 OR TDR-94D MODE STRANSPONDER INSTALLATION WITH ONE WHICH HAS ELEMENTARY FLIGHT ID ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3284-0003TRANSPONDER INSTL,FLIGHT ID-INFO ONLY ATA : C90A LJ-1306, LJ-1316, LJ-1318, LJ-1320, LJ-1726,

LJ-1728 THRU LJ-1753 & LJ-1755C90GT LJ-1727, LJ-1754 & LJ-1756 & AFTERTHIS KIT PROVIDES INFORMATION ONLY TO REPLACE THE EXISTING TDR-94 TRANSPONDERINSTALLATION WITH A TDR-94D WHICH HAS ELEMENTARY FLIGHT ID AND DIVERSITY ON IN-SERVICEAIRCRAFT.WT. CHANGE : TO BE DETERMINED BY INSTALLEREST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3401-1APPROACH MODE UNS-IM WITH FACTORY INSTALLED UNS-IM ATA :B200 BB-1500 THRU BB-1524THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE UNS-IM INSTALLATION TO ALLOW GPSNON-PRECISION APPROACHES WITH AUTOPILOT COUPLED ON AIRCRAFT WITH FACTORY INSTALLEDUNS-IM.

NOTENOTENOTENOTE:::: NOT SUPPLIED WITH KIT: COLLINS OR UNIV. NAV. UNITS. YOU WILL HAVE TO RETURNAPC-65H AP COMPUTER TO COLLINS RADIO MOD CENTER TO UPDATE TO 622-9724-130AND FOR IMPROVED SOFTWARE RC LIMITS AND ALT PRESELC REF COLLINS SERVICEBULLETIN NO. APC65H22-75. NEED TO RETURN UNS-IM COMPUTER TO UNIVERSAL NAVMOD CENTER TO UPDATE STATUS TO 1013-42-011 AND SCN 22.X.


101-3402-3ELT INSTL, DUAL MODE INFO ONLY ATA : 25B300 FL-273 ONLY.THIS KIT PROVIDES INFORMATION ONLY FOR INSTALLATION OF THE ARTEX ELT 110-406 & DUAL MODEROD ANTENNA (110-323) FOR MODELWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-3405-1ELT INSTL, DUAL MODE INFO ONLY ATA : 25B200, B200C, & B200T BT-39 & AFTER, BB1510 AND AFTER, BL-141

AND AFTER.THIS KIT PROVIDES INFORMATION ONLY FOR INSTALLATION OF THE ARTEX ELT C406-2 AND DUAL MODEROD ANTENNA (110-323) FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3407-1GROUND COM RELAY REPL INFO ONLY ATA : 23B200 BB-1731 THRU BB-1821B200C BL-141 THRU BL-147B300 FL-312 THRU FL-366C90A LJ-1612 THRU LJ-1691COMMUNIQUE' #2004-02. 07/12/04THIS KIT PROVIDES INFORMATION ONLY FOR REPLACING THE GROUND COMM AUDIO CONTROL RELAYSFOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)

101-3409-0001STANDBY BATTERY RELAY MODIFICATION ATA :B200, PROLINE 21 EQUIPPED BB-1769, BB-1834, BB-1843 THRU BB-1924B200C BL-148 & BL-149B200CT BN-10 & AFTERB200T BT-47 & AFTERB300 FL-329, FL-381, & FL-383 THRU FL-466B300C FM-12 & AFTER, ENDING SERIALS TO BE

ESTABLISHED BY THE EFFECTIVITY OFECR014769

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE EMERGENCY BATTERYELECTRONIC CIRCUIT BREAKER INSTALLATION TO PREVENT BATTERY DRAIN WHEN NOT POWERED, ONPROLINE 21 EQUIPPED IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: HEAT SHRINK TUBING REQUIRED BUT NOT SUPPLIED WITH KIT. PROCURE FROM ANYCOMPANY AUTHORIZED OUTLET.



KIT CATALOG

101-3410-0001ESIS LIGHTING VOLTAGE MOD-INFO ONLY ATA :B200 BB-1834, BB-1843 THRU BB-1862; B300 S/N:

FL-381, FL-383 THRU FL-395THIS KIT PROVIDES INFORMATION ONLY NECESSARY TO MODIFY THE EMERGENCY STANDBYINSTRUMENT SYSTEM (ESIS) TO ACCEPT AN ESIS USING +28VDC LIGHTING (-0401) IN LIEU OF +5VDCLIGHTING (-0201) ON PROLINE 21 EQUIPPED IN-SERVICE AIRCRAFT.


101-3505-0001TRANSPONDER WITH ENHANCED SURVEILLANCE INSTL ATA :B200 BB-1834, BB-1843 THRU BB-1897, BB-1899

AND AFTERB200C BL-148 & AFTERB300 FL-381, FL-383 & AFTERB300C FM-12 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL THE TRANSPONDER WITHENHANCED SURVEILLANCE OPTION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "NAS1097AD3""NAS1097AD4" RIVETS, "MIL-S-8802" SEALANT AND "M27500-22TG2T14"WIRE-SHLD TWIST PAIR REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : 7.5 LB MOMENT: +2,283 LB-IN (B200/B200C), WT: 7.5 LB MOMENT: +2,537 LB-IN (B300/B300C)EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4003-1 PCSEATS, AFT COMPARTMENT FOLDING ATA :200 BB-2 THRU BB-309, BB-311 THRU BB-342,

BB-344 THRU BB-382, BB-384 THRU BB-413200T BT-1 THRU BT-4THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO REMOVABLE FOLDING SEATS IN THE AFTBAGGAGE COMPARTMENT. (INCLUDES PROVISIONS FOR OXYGEN)WT. CHANGE : WT: 47 LBS @ 330 ARMEST. MAN/HRS: : 60MEN : N/A

101-4003-11 PCSEATS, AFT COMPARTMENT FOLDING ATA :200, B200 BB-383, BB-415, BB-416, BB-418 THRU

BB-448, BB-450 AND AFTER200T, B200T BT-5 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ONE REMOVABLE FOLDING SEAT ON THERIGHT SIDE OF THE AFT BAGGAGE COMPARTMENT.WT. CHANGE : WT: 30 LBS @ 329 ARMEST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

101-4003-13 PCSEATS, AFT COMPARTMENT FOLDING ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO REMOVABLE FOLDING SEATS IN THE AFTBAGGAGE COMPARTMENT. (INCLUDES PROVISIONS FOR OXYGEN)WT. CHANGE : WT: 47 LBS @ 330 ARMEST. MAN/HRS: : 60MEN : N/A

101-4003-15 PCSEATS, AFT COMPARTMENT FOLDING ATA :200 BB-2 THRU BB-309, BB-311 THRU BB-342,

BB-344 THRU BB-382, BB-384 THRU BB-412200T BT-1 THRU BT-4THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ONE REMOVABLE FOLDING SEAT ON THELEFT SIDE OF THE AFT BAGGAGE COMPARTMENT.WT. CHANGE : WT: 47 LBS @ 330 ARMEST. MAN/HRS: : 60MEN : N/A

101-4003-17 PCSEATS, AFT COMPARTMENT FOLDING ATA :300 FA-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO REMOVABLE FOLDING SEATS IN THE AFTBAGGAGE COMPARTMENT.WT. CHANGE : WT: 47 LBS @ 330 ARMEST. MAN/HRS: : 60MEN : N/A

101-4003-19 PCFOLD UP SEAT AFT C(COMM KT) ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-4003-3 PCSEATS, AFT COMPARTMENT FOLDING ATA :200, B200 BB-383, BB-415, BB-416, BB-418 THRU

BB-448, BB-450 THRU BB-733, BB-735 THRUBB-792, BB-794 THRU BB-828, BB-830 THRUBB-855, BB-871 THRU BB-873, BB-892,BB-893, BB-895, BB-912

200T BT-5 THRU BT-22, BT-28THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO REMOVABLE FOLDING SEATS IN THE AFTBAGGAGE COMPARTMENT. (INCLUDES PROVISIONS FOR OXYGEN)WT. CHANGE : WT: 47 LBS @ 330 ARMEST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

101-4003-5 PCSEATS, AFT COMPARTMENT FOLDING ATA :200 AND B200 BB-383, BB-415, BB-416, BB-418 THRU

BB-448, BB-450 THRU BB-733, BB-735 THRUBB-792, BB-794 THRU BB-828, BB-830 THRUBB-855, BB-871 THRU BB-873, BB-892,BB-893, BB-895, BB-912

200T BT-5 THRU BT-22, BT-28THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ONE REMOVABLE FOLDING SEAT ON THELEFT SIDE OF THE AFT BAGGAGE COMPARTMENT.WT. CHANGE : WT: 30 LBS @ 329 ARMEST. MAN/HRS: : 60MEN : N/A

101-4003-7 PCSEATS, AFT COMPARTMENT FOLDING ATA :B200 BB-734, BB-793, BB-829, BB-854 THRU


B200T BT-23 THRU BT-27, BT-29 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO REMOVABLE FOLDING SEATS IN AFTBAGGAGE COMPARTMENT.WT. CHANGE : WT: 47 LBS @ 330 ARMEST. MAN/HRS: : 60MEN : N/A

101-4003-9 PCSEATS, AFT COMPARTMENT FOLDING ATA :B200 BB-734, BB-793, BB-829, BB-854 THRU


B200T BT-23 THRU BT-27, BT-29 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ONE REMOVABLE FOLDING SEAT ON THELEFT SIDE OF THE AFT BAGGAGE COMPARTMENT.WT. CHANGE : WT: 30 LBS @ 329 ARMEST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

101-4010-1 SDUAL SUPPORT CABLE AIRSTAIR DOOR ATA :90, A90, B90, E90, F90, 100, A100, B100, 200,B200

BB-6 THRU BB-309, BB-311 THRU BB-342,BB-344 THRU BB-382, BB-384 THRU BB-414,BB-417, BB-449

A200 (C-12A) BC-51 THRU BC-61A200 (C-12A) BC-51 THRU BC-61A200 (C-12C) BC-62 THRU BC-75C90 LJ-502 THRU LJ-985, LJ-987 THRU LJ-995,

LJ-997 THRU LJ-1010DUAL SUPPORT CABLE, AIR STAIR DOOR (REF: SERVICE INSTRUCTION NO. 1036) KIT, (ADDS ADDITIONALAIRCRAFT SERIAL NUMBERS KIT AUTHORIZED FOR USAGE).

NOTENOTENOTENOTE:::: KIT FURNISHES COMPLETE CABLE ASSEMBLY, UPPER HALF: 1440-20. LOWER: 1440-21.NOTENOTENOTENOTE:::: FOR MODEL 300 SEE KIT 100-4042-1 S AND FOR CARGO DOOR AIRCRAFT SEE 101-4062-1

S. THE REST OF THE SERIAL NUMBER APPLICABILITY REMAINS THE SAME.NOTENOTENOTENOTE:::: FOR QUICK DISCONNECT FORWARD CABLE LIKE ON B300 AND C90B, ORDER P/N

130-430058-1 LINK AND 100-430046-37 UPPER CABLE ASSEMBLY IN ADDITION TO KIT. LINKREPLACED IS 100-430049 AND CABLE REPLACED IS 1440-20. CONTACT PRODUCTSUPPORT IF INFORMATION FOR INSTALLATION IS NEEDED. (SEE -3 S AND -5 S KITSALSO.)


101-4010-3 SAIRSTAIR DOOR DUAL SUPPORT CABLE ATA :200, B200 BB-310, BB-343, BB-415, BB-416, BB-418

THRU BB-448, BB-450 AND AFTER200T, B200T BT-5 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DUAL SUPPORT CABLE ON THE FORWARDSIDE OF THE AIRSTAIR DOOR.WT. CHANGE : WT: 7 LBS @ 279 ARMEST. MAN/HRS: : 24 TO 30MEN : N/A

101-4010-5 SAIRSTAIR DOOR DUAL SUPPORT CABLE ATA :C90, C90A LJ-986, LJ-996, LJ-1011 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DUAL SUPPORT CABLE ON THE FORWARDSIDE OF THE AIRSTAIR DOOR.WT. CHANGE : WT: 7 LBS @ 229 ARMEST. MAN/HRS: : 24 TO 30MEN : N/A


KIT CATALOG

101-4014-3 PSTROBE LIGHT ROCK SHIELD ATA :200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT BN-1 AND AFTER200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STROBE LIGHT SHIELD ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4015-1 SAIR CONDITIONER SOLENOID VALVE ATA :200, B200 BB-2 THRU BB-744200C BL-1 THRU BL-13200T BT-1 THRU BT-16, BT-18THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE SPARES REPLACEMENT FOR THE3302-00-11 SOLENOID VALVE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4016-1 PWINDSHIELD WASHER ATA :200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERF90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WINDSHIELD WASHER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4019-1 SVENTRAL FIN - SPARES ATA :200, B200 BB-2 THRU BB-829200C BL-1 THRU BL-30200C BL-1 THRU BL-30200CT BN-1200T BT-1 THRU BT-19THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A P/N 101-440018-83 FIN ASSEMBLY AS ASPARES REPLACEMENT FOR THE 101-440018-11 AND P/N 101-440018-77 ASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-4019-3 SVENTRAL FIN - SPARES ATA :90, A90, B90, C90 LJ-1 THRU LJ-974E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A P/N 50-440051-83 FIN ASSEMBLY AS ASPARES REPLACEMENT FOR THE 50-440051-7, -27, AND -73 ASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4019-7 SVENTRAL FIN - SPARES ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-126THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A P/N 99-420023-61 FIN ASSEMBLY AS ASPARES REPLACEMENT FOR 99-440023-9 AND -29 ASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4019-9 SVENTRAL FIN INSTL ATA : 53WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-4024-3 SWING BOLT, LOWER FORWARD ATA :100, A100 B-1 THRU B-247 WITH KIT 100-4007-1 S

INSTALLED90, A90, B90, C90, C90A LJ-1 THRU LJ-1084 WITH KIT 90-4077-1 S

INSTALLED,LJ-1086 AND LJ-1087 WITH KIT 90-4077-1 SINSTALLED

B100 BE-1 THRU BE-137 WITH KIT 100-4007-1 SINSTALLED

E90 LW-1 THRU LW-347 WITH KIT 90-4077-1 SINSTALLED

F90 LA-2 THRU LA-225SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)


KIT CATALOG

101-4024-5 SWING BOLT, LOWER FORWARD ATA :100, A100 B-1 THRU B-247 WITHOUT KIT 100-4007-1 S

INSTALLED100, A100 B-1 THRU B-247 WITHOUT KIT 100-4007-1 S

INSTALLED90, A90, B90, C90, C90A LJ-68 THRU LJ-1084 WITHOUT KIT 90-4077-1

S INSTALLED,LJ-1086 AND LJ-1087 WITHOUT KIT90-4077-1 S INSTALLED

B100 BE-1 THRU BE-137 WITHOUT KIT 100-4007-1S INSTALLED

E90 LW-1 THRU LW-347 WITHOUT KIT 90-4077-1S INSTALLED

SB NO. 1235 AND NO. 2248 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)

101-4024-7 SWING BOLT, LOWER FORWARD ATA :90 LJ-1 THRU LJ-67 WITHOUT KIT 90-4077-1 S

INSTALLEDSB NO. 1235 AND NO. 2248 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)

101-4025-1 SWING BOLT, UPPER FORWARD ATA :200, B200 BB-2 THRU BB-1157, BB-1159 THRU

BB-1166, BB-1168 THRU BB-1192200C, B200C BL-1 THRU BL-72200CT, B200CT BN-1 THRU BN-4200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)


KIT CATALOG

101-4025-3 SWING BOLT, UPPER FORWARD ATA :F90 LA-2 THRU LA-225SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)

101-4025-5 SWING BOLT, UPPER FORWARD ATA :A100 B-122 THRU B-247A100 B-122 THRU B-247B100 BE-1 THRU BE-137C90, C90A LJ-568 THRU LJ-1084, LJ-1086E90 LW-5 THRU LW-347SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)

101-4025-7 SWING BOLT, UPPER FORWARD ATA :100 AND A100 B-1 THRU B-12190, A90, B90, C90 LJ-1 THRU LJ-567E90 LW-1 THRU LW-4SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : N/A

101-4026-1 SWING BOLT, AFT UPPER OR LOWER ATA :100, A100 B-1 THRU B-24790, A90, B90, C90, C90A LJ-1 THRU LJ-1084, LJ-1086, LJ-1087B100 BE-1 THRU BE-137E90 LW-1 THRU LW-347SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT. ONE BOLTPER KIT. 4 KITS PER AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)


KIT CATALOG

101-4026-3 SWING BOLT, AFT UPPER OR LOWER ATA :200, B200 BB-2 THRU BB-1157, BB-1159 THRU

BB-1166, BB-1168 THRU BB-1192200C, B200C BL-1 THRU BL-72200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30300 FA-1 & AFTERB300 FL-1 & AFTERB300C FM-1 & AFTERF90 LA-2 THRU LA-225SB NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT. ONE BOLTPER KIT. 4 EA PER AIRCRAFT

WT. CHANGE : N/AEST. MAN/HRS: : 9 TO 12MEN : 2 (MEN)

101-4026-5WING BOLT INSTL, AFT ATA :65-90, 65-A90, B90, C90, E90, 99, 99A, A99A,B99, C99, 100, A100, B100, H90(T44A),A90-1 RU-21A, U-21A, RU-21D, U-21G, JU-21AA90-1 RU-21H GRVA90-2 RU-21BA90-3 RU-21CA90-4 RU-21H GRVA90-4 RU-21H GRVTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BOTH INCONEL WING ATTACH BOLTS ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4026-7WING BOLT INSTL, AFT ATA :F90, 200, 200C, 200T, 200CT, B200, B200C,B200T, B200CT, A200, A200C, A200CT, 300,B300, & B300CTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BOTH INCONEL WING ATTACH BOLTS ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-4030-1 SRUDDER PEDAL LEVER - SPARES ATA :200, B200 BB-114 THRU BB-1220200C, B200C BL-1 THRU BL-117200CT, B200CT BN-1 THRU BN-4200T, B200T BT-24 THRU BT-30A100 B-226 THRU B-247B100 BE-31 THRU BE-137C90A, C90A LJ-677 THRU LJ-1110E90 LW-165 THRU LW-347F90 LA-2 THRU LA-237THIS KIT IS THE SPARES REPLACEMENT FOR 101-524599-1, 101-524281-1 OR 101-524759-1 LH RUDDERPEDAL LEVERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4030-2 SRUDDER PEDAL LEVER - SPARES ATA :200, B200 BB-114 THRU BB-1220200C, B200C BL-1 THRU BL-117200CT, B200CT BN-1 THRU BN-4200T, B200T BT-24 THRU BT-30A100 B-226 THRU B-247B100 BE-31 THRU BE-137C90, C90A LJ-677 THRU LJ-1110E90 LW-165 THRU LW-347F90 LA-2 THRU LA-237THIS KIT IS THE SPARES REPLACEMENT FOR 101-524599-2, 101-524281-2 OR 101-524759-2 RH RUDDERPEDAL LEVERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4032-1 SWING CENTER SECTION, UPPER SKIN ATA :200, B200 BB-614 THRU BB-1138, BB-1140 THRU

BB-1157, BB-1159 THRU BB-1166, BB-1168THRU BB-1178, BB-1180 THRU BB-1188,BB-1190 THRU BB-1192

200C, B200C BL-7 THRU BL-66, BL-68 THRU BL-71200CT, B200CT BN-1 THRU BN-4200T, B200T BT-20 THRU BT-26, BT-28, BT-30300 FA-1 THRU FA-16THIS KIT PROVIDES PARTS AND INFORMATION FOR REBONDING THE LEFT WING CENTER SECTIONHONEYCOMB WING PANEL SKIN.WT. CHANGE : WT: 5 LBS @ 205 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-4032-3 SWING CENTER SECTION, UPPER SKIN ATA :200, B200 BB-614 THRU BB-1138, BB-1140 THRU

BB-1157, BB-1159 THRU BB-1166, BB-1168THRU BB-1178, BB-1180 THRU BB-1188,BB-1190 THRU BB-1192

200C, B200C BL-7 THRU BL-66, BL-68 THRU BL-71200CT, B200CT BN-1 THRU BN-4200T, B200T BT-20 THRU BT-26, BT-28, BT-30300 FA-1 THRU FA-16THIS KIT PROVIDES PARTS AND INFORMATION FOR REBONDING THE RIGHT WING CENTER SECTIONHONEYCOMB WING PANEL SKIN.WT. CHANGE : WT: 5 LBS @ 205 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4034-1 SAIRSTAIR DOOR REINFORCEMENT ATA :200C, B200C BL-1 THRU BL-112, BL-118 THRU BL-128200CT, B200CT BN-1 THRU BN-4THIS KIT PROVIDES PARTS AND INFORMATION FOR THE INSTALLATION OF THE CARGO AIRSTAIR DOORLOWER CLOSURE REINFORCEMENT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4037-1 PJACK PAD REINFORCEMENT, WING AND FUSELAGE ATA :300 FA-1 THRU FA-87THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL JACK PAD SUPPORT STRUCTURES ON THEWING REAR SPAR AND THE FUSELAGE NOSE TO COMPLY WITH REQUIREMENTS OF CAA CERTIFICATION.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4038-1 PFLAP CONTROL ATA :300 FA-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLAP LIMIT SWITCH ASSEMBLY AND FLAPCONTROL SWITCH ASSEMBLY ON THE INBOARD RH FLAP AND PEDESTAL RESPECTIVELY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-4039-1 SBATTERY RELAY COVER ATA :300 FA-1 THRU FA-89SB NO. 2143 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RELAY COVER FOR PROTECTION OFELECTRICAL COMPONENTS AGAINST WATER LEAKS.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : N/A

101-4040-1 SFUEL FILTER ACCESS DOOR ATA :300 FA-1 THRU FA-12THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ACCESS DOOR TO THE FUEL FILTER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4042-1 SAIRSTAIR DOOR DUAL SUPPORT ATA :300 FA-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DUAL SUPPORT CABLE ON THE FORWARDSIDE OF THE AIRSTAIR DOOR.

NOTENOTENOTENOTE:::: FOR CARGO DOOR AIRCRAFT SEE KIT 101-4062-1 S.NOTENOTENOTENOTE:::: FOR OTHER MODELS SEE KITS 101-4010-1 S, -3 S AND -5 S.

WT. CHANGE : WT: + 4.4 LBS; MOMENT: + 1231 IN.-LBSEST. MAN/HRS: : 12 TO 16MEN : N/A

101-4043-1 SDEFROSTER INSTL,COCKPIT&CABIN WINDOW ATA : 30300 FA-2 THRU FA-206300 (FAA) FF-1 THRU FF-19SI NO. 2273, REV. 1WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-4043-11 SDEFROSTER, COCKPIT AND CABIN WINDOW ATA :300 FA SERIESPENDING SB NO. 2273, REV. 2THIS KIT PROVIDES PARTS AND INFORMATION MINUS THE 101-420081-9 AND -10 WINDOWS NECESSARYTO INSTALL A DEFROSTER INSTALLATION FOR COCKPIT SIDE WINDOWS WITH BLEED AIR REGULATORALREADY INSTALLED BY 101-4043-1 S KIT PER "OPTIONAL" SB NO. 2223 OR FACTORY EQUI

NOTENOTENOTENOTE:::: SEE KIT 101-9067-3 S WHICH OFFERS AN OPTIONAL IMPROVEMENT TO THIS KIT.WT. CHANGE : WT: + 1.1; ARM: + 188; MOMENT: +260 IN.-LBSEST. MAN/HRS: : 42MEN : 2 (MEN)


KIT CATALOG

101-4043-13 SDEFROSTER, COCKPIT AND CABIN WINDOW ATA :300 FA SERIESTHIS KIT PROVIDES PARTS AND INFORMATION, MINUS THE 101-420081-9 AND -10 WINDOWS, NECESSARYTO INSTALL A DEFROSTER INSTALLATION FOR THE COCKPIT SIDE WINDOWS. REQUIRED BLEED AIRREGULATOR SYSTEM IS INCLUDED IN THIS KIT.WT. CHANGE : WT: + 3.8 LB.; ARM: + 2-2 IN.; MOMENT: +768 IN.-LBSEST. MAN/HRS: : 90MEN : 2 (MEN)

101-4043-3 SDEFROSTER, COCKPIT AND CABIN ATA :300 FA-131 THRU FA-168, FA-170 THRU FA-176,

FA-179 THRU FA-183, FA-185 THRU FA-189"MANDATORY" SB NO. 2273, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DEFROSTER INSTALLATIONFOR COCKPIT SIDE WINDOWS WITH BLEED AIR REGULATOR ALREADY INSTALLED BY 101-4043-1 S KIT ORFACTORY EQUIPPED ON AIRCRAFT AND ANY AIRCRAFT WITH -1 S KIT INSTALLED PER "OPT

NOTENOTENOTENOTE:::: THIS KIT INCLUDES 101-420081-9 AND -10 COATED WINDOW.NOTENOTENOTENOTE:::: SEE KIT 101-9067-3 S, WHICH MAKE AN OPTIONAL IMPROVEMENT TO THIS KIT.NOTENOTENOTENOTE:::: BLACK RUBBER WINDOW SEAL CAN BE REUSED SO IS NOT FURNISHED WITH KIT. IF

FOUND DAMAGED OR DAMAGED IN REMOVING THEN REPLACE WITH NEW SEAL. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 1.1 ARM; + 188 MOMENT: + 206 IN.-LBS;EST. MAN/HRS: : 42MEN : N/A

101-4043-5 SDEFROSTER, COCKPIT AND CABIN ATA :300 FA-2 THRU FA-130 WHICH HAVE NOT

INCORPORATED "OPTIONAL" SERVICEBULLETIN NO. 2223 AND KIT 101-4043-1 S,OR A PREVIOUS INSTALLATION

"MANDATORY" SB NO. 2273, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DEFROSTER INSTALLATIONFOR COCKPIT SIDE WINDOWS INCLUDING A BLEED AIR REGULATOR SYSTEM. THIS KIT INCLUDES101-420081-9 AND -10 COATED WINDOWS.

NOTENOTENOTENOTE:::: BLACK RUBBER WINDOW SEAL CAN BE REUSED SO IS NOT FURNISHED WITH KIT. BUT IFFOUND DAMAGED OR DAMAGED IN REMOVAL THEN NEED TO REPLACE.

NOTENOTENOTENOTE:::: SEE KIT 101-9067-3 S WHICH MAKES AN OPTIONAL IMPROVEMENT TO THIS KIT.WT. CHANGE : WT: + 3.8 ARM; + 202 MOMENT: +768 IN.-LBSEST. MAN/HRS: : 90MEN : 2 (MEN)


KIT CATALOG

101-4043-7 SDEFROSTER, COCKPIT AND CABIN ATA :300 FA-1 THRU FA-130"OPTIONAL" SB NO. 2223, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DEFROSTER INSTALLATIONFOR CABIN WINDOWS INCLUDING OPTIONAL VESTIBLE WINDOW ON AIRCRAFT WITH BLEED AIR SYSTEMALREADY INSTALLED BY 101-4043-5 S KIT IN ACCORDANCE WITH SB NO. 2273.

NOTENOTENOTENOTE:::: KIT IS WITHOUT BLEED AIR REGULATOR OR COATED WINDOWS.NOTENOTENOTENOTE:::: SEE KIT NO. 101-9067-3 S WHICH OFFERS AN OPTIONAL IMPROVEMENT TO THIS KIT.

WT. CHANGE : WT: + 2.3; ARM: + 212; MOMENT: +488 IN.-LBSEST. MAN/HRS: : 24MEN : 2 (MEN)

101-4043-9 SDEFROSTER ATA :300 FF-1 THRU FF-19SB NO. 2273, REV. 1THIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL DEFROSTER FOR COCKPIT SIDE WINDOWSINCLUDING A BLEED AIR REGULATOR.WT. CHANGE : N/AEST. MAN/HRS: : 90MEN : N/A

101-4045-1 SUPPER WING SKIN ATA :200, 200C, 200CT, B200, B200C, B200T,B200CT, 300, 300CSB NO. 2040, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR REMOVAL AND REPLACEMENT OFPARTIAL LEFT CENTER SECTION UPPER WING SKIN PANEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 180MEN : N/A

101-4045-3 SUPPER WING SKIN ATA :200, 200C, 200CT, B200, B200C, B200T,B200CT, 300THIS KIT CONSISTS OF PARTS AND INFORMATION FOR REMOVAL AND REPLACEMENT OF PARTIAL LEFTCENTER SECTION UPPER WING SKIN PANEL WITH NOMEX CORE. KIT 101-4052-1 S WILL BE REQUIRED TOOBTAIN RESTRICTED ARTICLES REQUIRED FOR INSTALLATION OF THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : 180MEN : 1 (MAN)


KIT CATALOG

101-4045-4 SUPPER WING SKIN ATA :200, 200C, 200CT, B200, B200C, B200T,B200CT, 300, 300CTHIS KIT PROVIDES PARTS AND INFORMATION FOR REMOVAL AND REPLACEMENT PARTIAL RIGHTCENTER SECTION UPPER WING SKIN PANEL WITH NOMEX CORE. PURCHASE OF 101-4052-1 SRESTRICTED ARTICLE KIT IS REQUIRED FOR INSTALLATION OF THIS KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4046-1 PCSEATS FOLD UP, AFT COMPARTMENT ATA :300 FA-1 AND AFTERB300 FL-1 AND AFTER (SEE NOTE NO. 1)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL DUAL (SIDE BY SIDE) SEATS INAFT BAGGAGE COMPARTMENT ON INSERVICE AIRCRAFT. KIT CONTAINS 2 SEATS.

NOTENOTENOTENOTE:::: WHEN THIS KIT IS INSTALLED ON FA-2 THRU FA-111 COMPLIANCE WITH "MANDATORY"SERVICE BULLETIN NO. 2331 IS REQUIRED. SEE -3 PC FOR LEFT SIDE SEAT ONLY AND -5PC FOR RIGHT SIDE SEAT ONLY.

NOTENOTENOTENOTE:::: EFFECTIVE FL-114 AND AFTER THE COCKPIT VOICE RECORDER IS STANDARDEQUIPMENT.

NOTENOTENOTENOTE:::: WHEN EITHER THE -1, -3 OR -5 PC KIT INSTALLATIONS IS INSTALLED ON AIRCRAFT, THE130-530074 HIGH DENSITY SEAT INSTALLATION, APPROVED COCKPIT VOICE RECORDERAND FLIGHT DATE RECORDER MUST BE INSTALLED ON AIRCRAFT.

NOTENOTENOTENOTE:::: FOR MODEL 200 SEE 101-4003 KITS.WT. CHANGE : SEE KIT DRAWING ON MODEL FOR SPECIFIC CHANGE INFORMATION.EST. MAN/HRS: : 60MEN : N/A

101-4046-3 PCFOLD UP - AFT COMPARTMENT SEAT, LEFT SIDE ONLY ATA :300 FA-1 AND AFTERB300 FL-1 AND AFTER (SEE NOTE NO. 1)FOR OTHER OPTIONS SEE -5 PC (R-S) AND-1 PC FOR DUAL SEATSWT. CHANGE : N/AEST. MAN/HRS: : 60MEN : N/A

101-4046-5 PCFOLD UP - AFT COMPARTMENT SEAT, RIGHT SIDE ONLY ATA :300 FA-1 AND AFTERB300 FL-1 AND AFTER (SEE NOTE NO. 1).FOR OTHER OPTIONS SEE -5 PC R-S AND -1 PC FOR DUAL SEATSWT. CHANGE : SEE KIT DRAWING ON MODEL FOR SPECIFIC WEIGHT CHANGE INFORMATION.EST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

101-4048-1 SRIVET SEALING - UPPER WING PANEL ATA :200, 200C, 200T, 200CT, B200, B200C,B200T, B200CTSB NO. 2040, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR SEALING RIVETS IN THE LEFT ANDRIGHT HAND UPPER INBOARD SKIN PANEL.

NOTENOTENOTENOTE:::: MC236 SEALER REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.


101-4049-1 SCENTER SECTION LEADING EDGE ATA :300 FA-1 THRU FA-134300 (FAA) FF-1, FF-2A200CT (C-12D) BP-46 THRU BP-51A200CT (C-12F) BP-52 THRU BP-63A200CT (RC-12K) FE-1 THRU FE-6B200 BB-1158 THRU BB-1167, BB-1193 THRU

BB-1280B200C BL-124 THRU BL-129B200C (C12F) BL-73 THRU BL-112, BL-118 THRU BL-123B200C (C12F) BP-64B200C (RC-12F) BU-11, BU-12B200C (UC-12F) BU-1 THRU BU-10B200C (UC-12M) BV-1B200T BT-31SB NO. 2295 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REMOVE AND REPLACE SKIN PANELS ON TOP SIDEOF WING CENTER SECTION AT MAIN SPAR. ALSO REMOVE AND REPLACE LEADING EDGE SKINS ONBOTTOM SIDE WING CENTER SECTION AT MAIN SPAR FOR RH AND LH SIDE.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : 1 (MAN)

101-4049-3 SCENTER SECTION LEADING EDGE ATA :B200, B200C, B200T, 300, FAA (300)SB NO. 2295 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REMOVE AND REPLACE LEADING EDGE SKINS ONBOTTOM SIDE OF WING CENTER SECTION AT MAIN SPAR FOR RH AND LH SIDES.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : N/A


KIT CATALOG

101-4050-1 SSPAR BUSHING (1ST OVERSIZE) ATA :300 FA-1 THRU FA-190300 (FAA) FF-1 THRU FF-19B200 BB-1157, BB-1193 THRU BB-1334B200C (C12F) BL-73 THRU BL-132B200CT BN-1 THRU BN-4B200T BT-31 THRU BT-33C90A LJ-1085, LJ-1088 THRU LJ-1206F90 LA-226 THRU LA-237THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE THE LOWER MAIN SPAR CAP FITTINGBUSHINGS, USING THE “FORCEMATE” METHOD AS USED ON NEW AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 48MEN : N/A

101-4050-3SPAR BUSHING (2ND OVERSIZE) ATA :300 FA-1 THRU FA-190300 (FAA) FF-1 THRU FF-19B200 BB-1157, BB-1193 THRU BB-1334B200C (FAA) BL-73 THRU BL-132B200CT BN-1 THRU BN-4B200T BT-31 THRU BT-33C90A LJ-1085, LJ-1088 THRU LJ-1206F90 LA-226 THRU LA-237THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE THE LOWER MAIN SPAR CAP FITTINGBUSHINGS USING THE “FORCEMATE” METHOD OF INSTALLATION.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : N/A

101-4052-1 SFUEL BLADDER MOD., ADHESIVE AND SEALANTS ATA :THIS KIT PROVIDES FOR FASTENER PADS, SEALANT, SOLVENT, SCRIM CLOTH AND PRIMER FOR ONEUPPER WING PANEL INSTALLATION. REQUIRED FOR USE WITH KIT 101-4045.

NOTENOTENOTENOTE:::: THIS KIT IS REQUIRED FOR USE WITH KITS 101-4045-3 S AND -4 S.NOTENOTENOTENOTE:::: METALSET A4 ADHESIVE FILLER AND EA9309NA ADHESIVE REQUIRED BUT NOT

FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



KIT CATALOG

101-4053-1 PBAGGAGE POD FAIRING EXTENSION MODIFICATION ATA :B200 BB-1296, BB-1302, BB-1304, BB-1305,

BB-1309, BB-1314, BB-1338 THRU BB-1343ANTENNA CARGO POD KIT 101-3134-1 P REQUIRED FOR INSTALLATION WITH THIS MODIFICATION.THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE BAGGAGE POD AND REPLACE FORWARDAND AFT BAGGAGE POD FAIRING.WT. CHANGE : TO COMPLIANCE WITH FAR 23.25/CAR 3.74EST. MAN/HRS: : 48MEN : N/A

101-4060-1 SWINDSHIELD BIRD GUARD, CREW ENCLOSURE (U.K. CERTIFICATION) ATA :B300 FL-1 AND AFTERB300C FM-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A BIRD GUARD INSTALLATION ONTHE CREW WINDSHIELD ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS FOR U.K. CERTIFICATION OF THE MODEL 350 (B300) AND (B300C) SERIESAIRCRAFT, BUT MAY BE INSTALLED.

WT. CHANGE : WT: + 6.1 LBS; MOMENT: + 683 IN.-LBSEST. MAN/HRS: : 28 TO 32MEN : N/A

101-4061-1 SSTIFFENER, AFT PRESSURE BULKHEAD (U.K. CERTIFICATION) ATA :B300 FL-17 AND AFTER AS REQUIRED BY WORK

ORDERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STIFFENING ANGLES ON THE AFTPRESSURE BULKHEAD ON INSERVICE AIRCRAFT AS REQUIRED BY WORK ORDER FOR CERTIFICATION INTHE UNITED KINGDOM.WT. CHANGE : WT: 5 LBS; @ 382EST. MAN/HRS: : 23 TO 40MEN : N/A


KIT CATALOG

101-4062-1 SCARGO DOOR AIRSTAIR HAND RAIL ATA :200C, B200C BL-1 THRU BL-72, BL-124 THRU BL-139200C, B200C (C-12F) BL-73 THRU BL-112, BL-118 THRU BL-123,200CT, B200CT BN-1 THRU BN-4A200C (UC-12B) BJ-1 THRU BJ-66A200CT BP-64 THRU BP-74A200CT (C-12D) BP-1, BP-22, BP-24 THRU BP-51A200CT (C-12F) BP-52 THRU BP-63A200CT (RC-12D) GR-1 THRU GR-13A200CT (RC-12G) FC-1 THRU FC-3A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 AND AFTERB200C (RC-12F) BU-11, BU-13B200C (RC-12M) BV-11 AND BV-12B200C (UC-12F) BU-1 THRU BU-10B200C (UC-12M) BV-1 THRU BV-10B200CT (FW) FG-1, FG-2B200CT (FWC-12D) BP-7 THRU BP-11B300C FM-1 THRU FM-4THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A FORWARD HANDRAIL ONCARGO, AIRSTAIR DOOR.

NOTENOTENOTENOTE:::: RASI WILL HAVE THE SPECIAL TOOLS TO SUPPORT MILITARY AIRCRAFT INSTALLATION.NOTENOTENOTENOTE:::: EA9394 ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR

SHOP STOCK, YOU CAN PROCURE LOCALLY.NOTENOTENOTENOTE:::: COMMERCIAL AND AIRLINER KING AIR OPERATORS WILL HAVE TO CONTACT PRODUCT

SUPPORT TO MAKE ARRANGEMENTS FOR SHIPMENT OF 3 SPECIAL LOANER TOOLSTHAT ARE REQUIRED FOR INSTALLATION OF KIT BEFORE SCHEDULING AIRCRAFT INTOANY M-SHOP.

WT. CHANGE : (A200C, B200C) WT; + 3 LBS; MOMENT: + 828 (B300CT) WT: + 3 LBS; MOMENT: + 930EST. MAN/HRS: : 10MEN : N/A


KIT CATALOG

101-4063-1 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :200/B200 BB-2, BB-6 THRU BB-1462200C/B200C BL-1 THRU BL-72200C/B200C BL-124 THRU BL-138200CT/B200CT BN-1 THRU BN-4200T/B200T BT-1 THRU BT-38A100-1 BB-3 THRU BB-5A200 BC-1 THRU BC-75, BD-1 THRU BD-30A200C BJ-1 THRU BJ-66A200CT BP-1 THRU BP-63, GR-1 THRU GR-13, FC-1

THRU FC-3B200C BV-1 THRU BV-12B200C BL-73 THRU BL-112, BL-118 THRU BL-123B200C BU-1 THRU BU-12B200CT FG-1 THRU FG-2, BP-64 THRU BP-71"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 5 , # 6, OR # 7 LH SIDE AT FS 347.75.

NOTENOTENOTENOTE:::: OPERATORS OF AIRPLANES WITH EXISTING EXTERNAL DOUBLER INSTALLATIONS MAYREPLACE THE EXTERNAL DOUBLERS WITH THE INTERNAL STRINGER REINFORCEMENTKITS. SEE PART III OF SERVICE BULLETIN FOR INSTRUCTIONS ON REMOVING THEEXTERNAL DOUBLERS.

NOTENOTENOTENOTE:::: CONTACT PRODUCT SUPPORT FOR AIRCRAFT WITH SPECIAL APU. CARGO DOORINSTALLED UNDER AN STC OR SCIENTIFIC EQUIPMENT INSTALLATIONS WILL REQUIREALTERNATE METHODS OF COMPLIANCE. CONTACT PRODUCT SUPPORT FOR FURTHERINFORMATION REGARDING SPECIAL INSTALLATIONS.

WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)


KIT CATALOG


THRU FC-3B200C BU-1 THRU BU-12B200C BL-73 THRU BL-112, BL-118 THRU BL-123B200C BV-1 THRU BV-12B200CT FG-1 THRU FG-2, BP-64 THRU BP-71"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 5, # 6, # 7 OR # 11 RH SIDE AT FS 347.75.

NOTENOTENOTENOTE:::: OPERATORS OF AIRPLANES WITH EXISTING EXTERNAL DOUBLER INSTALLATIONS MAYREPLACE THE EXTERNAL DOUBLERS WITH THE INTERNAL STRINGER REINFORCEMENTKITS. SEE PART III OF SERVICE BULLETIN FOR INSTRUCTIONS ON REMOVING THEEXTERNAL DOUBLERS SERIAL NUMBER.

NOTENOTENOTENOTE:::: CONTACT PRODUCT SUPPORT FOR AIRPLANES WITH SPECIAL APU. CARGO DOORINSTALLED UNDER AN STC OR SCIENTIFIC EQUIPMENT INSTALLATIONS WILL REQUIREALTERNATE METHODS OF COMPLIANCE. CONTACT PRODUCT SUPPORT FOR FURTHERINFORMATION REGARDING SPECIAL INSTALLATIONS.



KIT CATALOG


THRU FC-3B200C BU-1 THRU BU-12B200C BL-73 THRU BL-112, BL-118 THRU BL-123B200C BV-1 THRU BV-12B200CT FG-1 THRU FG-2, BP-64 THRU BP-71"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 8, # 9 OR # 10 LH SIDE AT FS 347.75.


NOTENOTENOTENOTE:::: OPERATORS OF AIRPLANES WITH EXISTING EXTERNAL DOUBLER INSTALLATIONS MAYREPLACE THE EXTERNAL DOUBLERS WITH THE INTERNAL STRINGER REINFORCEMENTKITS. SEE PART III OF SERVICE BULLETIN FOR INSTRUCTIONS ON REMOVING THEEXTERNAL DOUBLERS SERIAL NUMBER IF NOT LISTED.



KIT CATALOG


THRU FC-3B200C BV-1 THRU BV-12B200C BU-1 THRU BU-12B200C BL-73 THRU BL-112, BL-118 THRU BL-123B200CT FG-1 THRU FG-2, BP-64 THRU BP-71"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 8, # 9 OR # 10 RH SIDE AT FS 347.75.

NOTENOTENOTENOTE:::: CONTACT PRODUCT SUPPORT FOR ENDING AIRCRAFT SERIAL NUMBER IF NOT LISTED.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)


KIT CATALOG


THRU FC-3B200C BU-1 THRU BU-12B200C BV-1 THRU BV-12B200C BL-73 THRU BL-112, BL-118 THRU BL-123B200CT FG-1 THRU FG-2, BP-64 THRU BP-71"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 11 LH SIDE AT FS 347.75.


NOTENOTENOTENOTE:::: OPERATORS OF AIRPLANES WITH EXISTING EXTERNAL DOUBLER INSTALLATIONS MAYREPLACE THE EXTERNAL DOUBLERS WITH THE INTERNAL STRINGER REINFORCEMENTKITS. SEE PART III FOR INSTRUCTIONS ON REMOVING THE EXTERNAL DOUBLERS.


101-4064-1 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-228B300 (350) FL-1 THRU FL-103B300C FN-1B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ON STRINGER #5, # 6 OR # 7 LH SIDE AT FS 347.75.





KIT CATALOG

101-4064-2 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-228B300 (350) FL-1 THRU FL-103B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8B300C (CS) FN-1"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 5, # 6, # 7 OR # 11 RH SIDE AT FS 347.75.




101-4064-3 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-228B300 (350) FL-1 THRU FL-103B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8B300C (CM) FN-1"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGERS # 8, # 9 OR # 10 LH SIDE AT FS 347.75.





KIT CATALOG

101-4064-4 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-228B300 (350) FL-1 THRU FL-103B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8B300C (CS) FN-1"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENT ON STRINGER # 8, OR #9 RH SIDE AT FS 347.75.




101-4064-5 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-228B300 (350) FL-1 THRU FL-103B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8B300C (CS) FN-1"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 11 LH SIDE AT FS 347.75.





KIT CATALOG

101-4064-7 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-228B300 (350) FL-1 THRU FL-103B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8B300C (CS) FN-1"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 10 RH SIDE AT FS 347.75.




101-4064-9STRINGER REINFORCEMENT, AFT FUSELAGE ATA :300 FA-1 THRU FA-230B300 FL-1 THRU FL-110B300C FM-1 THRU FM-8B300C FM-1 THRU FM-8B300C (CS) FN-1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT IN THE EVENTOF A RIVET SPACING PROBLEM FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MS20470E4-, MS20426E4-, NAS1097AD4-, MS20470AD4- & MS20426AD4- RIVETS ANDEA9309NA ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS FOR 300 SERIES WT: .3 LBS; MOMENT: 115 IN.-LBS FOR B300 SERIESEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-4065-1 SDOOR AIRSTAIR REINFORCEMENT ATA :A200CT (C-12D) BP-46 THRU BP-51A200CT (C-12F) BP-52 THRU BP-63A200CT (RC-12K) FE-26 THRU FE-29A200CT (RC-12K) FE-1 THRU FE-24B200C BL-129 THRU BL-138B200C (C-12F) BP-64 THRU BP-71B200C (RC-12M) BV-11, BV-12B200C (UC-12F) BU-1 THRU BU-10B200C (UC-12M) BV-1 THRU BV-10B200CT (FW) FG-1, FG-2B200CT (RC-12F) BU-11, BU-12B300C FM-1 THRU FM-4THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR THE INSTALLATION OF THE CARGO-AIRSTAIR DOOR LOWER CLOSURE REINFORCEMENT.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR INSTALLATION OF THIS KIT, BUT ARENOT FURNISHED WITH THE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY: P/N "EA9309 QT" SEALER, "MEK" CLEANING SOLVENT AND "CAB-O"SILICA OR GLASS SPHERES.


101-4066-1 SSPAR CAP LOWER MAIN, CENTER SECTION ATA :300 FA-1 THRU FA-219300 (FAA) FF-1 THRU FF-19A200CT BP-46 THRU BP-63A200CT FE-1 AND AFTERB200 BB-1158, BB-1167, BB-1193 THRU BB-1413B200C BL-124 THRU BL-137B200C BU-1 THRU BU-12, BV-1 THRU BV-12B200C BL-73 THRU BL-112, BL-118 THRU BL-123,

BP-64 THRU BP-71B200CT FG-1, FG-2B200T BT-31 THRU BT-34THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE A CENTER SECTIONLOWER MAIN SPAR CAP.

NOTENOTENOTENOTE:::: ADHESIVE P/N: "EA9309NA" OR "EA9309 QT" WILL BE REQUIRED TO INSTALL THIS BUT ISNOT PART OF KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.

WT. CHANGE : DETERMINE PER SECTION IV OF INSTALLATION INSTRUCTIONSEST. MAN/HRS: : 1600MEN : 1 (MAN)


KIT CATALOG

101-4066-3 SSPAR CAP LOWER MAIN, CENTER SECTION ATA :300 FA-220 AND AFTER300 (FAA) FF-20 AND AFTERB200 BB-1414 AND AFTERB200C BL-138 AND AFTERB200C BP-72 AND AFTERB200C BU-13 AND AFTERB200C BV-13 AND AFTERB200CT FG-3 AND AFTERB200CT BN-5 AND AFTERB200T BT-35 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERB300C (CS) FN-1 AND AFTERTHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE A CENTER SECTIONLOWER MAIN SPAR CAP.

NOTENOTENOTENOTE:::: ADHESIVE P/N: "EA9309NA" OR "EA9309 QT" WILL BE REQUIRED FOR INSTALLATION OFTHIS KIT BUT IS NOT PART OF KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.

WT. CHANGE : DETERMINE PER SECTION IV OF INSTALLATION INSTRUCTIONSEST. MAN/HRS: : 1600MEN : 1 (MAN)

101-4068-1 SSTRINGER REINFORCEMENT, AFT FUSELAGE, LH SIDE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 5, # 6 OR # 7 LH SIDE AT AFT PRESSURE BULKHEAD FOR SPECIAL MISSION AIRCRAFTEQUIPPED WITH OBSERVERS BUBBLE WINDOWS.

NOTENOTENOTENOTE:::: FOR REPAIR OF # 11 STRINGER ALSO REFER TO KIT 101-4064 DRAWING.NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLY

REFER TO KIT 101-4064 DRAWING FOR REPAIR KITS FOR THE NON-BUBBLE SIDE.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLATION (PER STRINGER PER SIDE)EST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)


KIT CATALOG

101-4068-10 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ON STRINGER #8, # 9 OR # 10 RH SIDE AT AFT PRESSURE BULKHEAD FOR INSERVICE SPECIAL MISSION AIRCRAFTEQUIPPED WITH OBSERVERS BUBBLE WINDOW IN THE AFT BAGGAGE COMPARTMENT.

NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLYREFER TO KIT 101-4064 KITS FOR REPAIR KITS FOR THE NON-BUBBLE SIDE.

NOTENOTENOTENOTE:::: FOR REPAIR OF # 11 STRINGER ALSO REFER TO 101-4064 KITS AND "MANDATORY"SERVICE BULLETIN NO. 2472.

WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLATION (PER STRINGER PER SIDE)EST. MAN/HRS: : FOR ACCESS: 10 TO 15

MAN/HRS: TO INSTALLATION: 10MEN : 2 MEN PER KIT (MEN)

101-4068-2 SSTRINGER REINFORCEMENT, AFT FUSELAGE, RH SIDE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 5, # 6 OR # 7 RH SIDE AT AFT PRESSURE BULKHEAD FOR SPECIAL MISSION AIRCRAFTEQUIPPED WITH OBSERVERS BUBBLE WINDOWS.

NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLYREFER TO KIT 101-4064 DRAWING FOR REPAIR KIT FOR THE NON-BUBBLE SIDE.

NOTENOTENOTENOTE:::: FOR REPAIR OF # 11 STRINGER ALSO REFER TO KIT 101-4064 DRAWING.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLATION (PER STRINGER PER SIDE)EST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)


KIT CATALOG

101-4068-3 SSTRINGER REINFORCEMENT, AFT FUSELAGE, LH SIDE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 8, # 9 OR # 10 LH SIDE AT AFT PRESSURE BULKHEAD FOR SPECIAL MISSION AIRCRAFTEQUIPPED WITH OBSERVERS BUBBLE WINDOWS.

NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLYREFER TO KIT 101-4064 DRAWING FOR REPAIR KITS FOR THE NON-BUBBLE SIDE.


101-4068-4 SSTRINGER REINFORCEMENT, AFT FUSELAGE, RH SIDE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 8 OR # 9 RH SIDE AT AFT PRESSURE BULKHEAD FOR SPECIAL MISSION AIRCRAFT EQUIPPEDWITH OBSERVERS BUBBLE WINDOWS.

NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLYREFER TO KIT 101-4064 DRAWING FOR REPAIR KITS FOR THE NON-BUBBLE SIDE.


101-4068-5 SSTRINGER REINFORCEMENT, AFT FUSELAGE, RH SIDE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STRINGER REINFORCEMENT ONSTRINGER # 10 ONLY, RH AT AFT PRESSURE BULKHEAD FOR SPECIAL MISSION AIRCRAFT EQUIPPEDWITH OBSERVERS BUBBLE WINDOWS.

NOTENOTENOTENOTE:::: FOR REPAIR OF # 11 STRINGER ALSO REFER TO KIT 101-4064 DRAWING.NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLY

REFER TO KIT 101-4064 DRAWING FOR REPAIR KITS FOR THE NON-BUBBLE SIDE.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLATION (PER STRINGER PER SIDE)EST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)


KIT CATALOG

101-4068-7 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :200T BT-1 THRU BT-22, BT-28,B200C BL-137 AND AFTERB200C BL-137 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ON STRINGER # 5, #6 OR # 7 LH SIDE AT AFT PRESSURE BULKHEAD FOR INSERVICE SPECIAL MISSION AIRCRAFT EQUIPPEDWITH OBSERVERS BUBBLE WINDOW IN THE AFT BAGGAGE COMPARTMENT.


NOTENOTENOTENOTE:::: FOR REPAIR OF #11 STRINGER ALSO REFER TO 101-4064-KITS AND "MANDATORY"SERVICE BULLETIN NO. 2472.



101-4068-8 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ON STRINGER #5, # 6 OR # 7 RH SIDE AT AFT PRESSURE BULKHEAD FOR INSERVICE SPECIAL MISSION AIRCRAFTEQUIPPED WITH OBSERVERS BUBBLE WINDOW IN THE AFT BAGGAGE COMPARTMENT.

NOTENOTENOTENOTE:::: FOR AIRCRAFT EQUIPPED WITH OBSERVERS BUBBLE WINDOW ON ONE SIDE ONLYREFER TO 101-4064 KITS FOR REPAIR KITS FOR THE NON-BUBBLE SIDE.





KIT CATALOG

101-4068-9 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :200T BT-1 THRU BT-22, BT-28B200C BL-37 AND AFTERB200C BL-37 AND AFTERB200CT BN-2 THRU BN-4B200T BT-23 THRU BT-38, EXCEPT BT-28THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ON STRINGER #8, # 9 OR # 10 LH SIDE AT AFT PRESSURE BULKHEAD FOR INSERVICE SPECIAL MISSION AIRCRAFTEQUIPPED WITH OBSERVERS BUBBLE WINDOW IN THE AFT BAGGAGE COMPARTMENT.





101-4069-1 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 THRU FE-31"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENTS ON STRINGER ON # 7ON LH SIDE ONLY AT FS 347.45 FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: .3 LBS MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 10 (PER KIT)

TO GAIN ACCESS FOR INSTALLATION KIT OR KITS: 10 TO 15MEN : 1 MAN PER KIT (MEN)

101-4069-2 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 THRU FE-31"MANDATORY" SB NO.2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENTS ON STRINGER # 7 ONRH SIDE ONLY AT FS 347.45 FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 10 (PER KIT)

TO GAIN ACCESS FOR INSTALLATION KIT OR KITS: 10 TO 15MEN : N/A


KIT CATALOG

101-4069-3 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 THRU FE-31"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENTS ON STRINGER # 8, # 9OR # 10 ON LH SIDE ONLY AT FS 347.45 FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 10 (PER KIT)

TO GAIN ACCESS FOR INSTALLATION KIT(S): 10 TO 15MEN : 2 (MEN)

101-4069-4 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 THRU FE-31"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENTS ON STRINGER # 8, # 9OR # 10 ON RH SIDE ONLY AT FS 347.45.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 10 (PER KIT)

TO GAIN ACCESS FOR INSTALLATION KIT(S): 10 TO 15MEN : 2

1 (MEN)

101-4069-5 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 THRU FE-31"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENTS ON STRINGER # 5 LHSIDE ONLY AT FS 347.75.WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLATION (PER STRINGER PER SIDE)EST. MAN/HRS: : 10 (PER KIT)


1 (MEN)


KIT CATALOG

101-4069-6 SSTRINGER REINFORCEMENT, AFT FUSELAGE ATA :A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 THRU FE-31THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STRINGER REINFORCEMENT ON STRINGER #5 RH SIDE ONLY AT FS 347.75.

NOTENOTENOTENOTE:::: (REF: "MANDATORY" SERVICE BULLETIN NO. 2472 REV. 1)WT. CHANGE : WT: .3 LBS; MOMENT: 104 IN.-LBS PER KIT INSTALLED (PER STRINGER PER SIDE)EST. MAN/HRS: : 10 (PER KIT)


1 (MEN)

101-4070-1 SSTRINGERS, LH SIDE REINFORCEMENT, AFT FUSELAGE ATA :300 (FAA) FF-1 THRU FF-19"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENT ON STRINGERS # 5, # 7,# 8, # 9 AND # 10 ON LH SIDE ONLY AT AFT PRESSURE BULKHEAD FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: +2.0 LBS; MOMENT: +696 IN.-LBS PER LH KIT INSTALLEDEST. MAN/HRS: : 50

TO GAIN ACCESS FOR INSTALLATION KIT: 10 TO 15MEN : 2

1 (MEN)

101-4070-3 SSTRINGERS, RH SIDE REINFORCEMENT, AFT FUSELAGE ATA :300 (FAA) FF-1 THRU FF-19"MANDATORY" SB NO. 2472, REV. 1THIS KIT PROVIDES THE PARTS AND INFORMATION TO INSTALL REINFORCEMENT ON STRINGERS # 5THRU # 11 ON RH SIDE ONLY AT AFT PRESSURE BULKHEAD FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: +2.0 LBS; MOMENT: +696 IN.-LBS PER RH KIT INSTALLEDEST. MAN/HRS: : 70

TO GAIN ACCESS FOR INSTALLATION KIT: 10 TO 15MEN : 2

1 (MEN)

101-4071-1BAGGAGE PLACARD MODEL B300 CIS ATA :B300 FL-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A PLACARD DENOTING WEIGHTLIMITATIONS FOR THE AFT BAGGAGE COMPARTMENT. THIS KIT IS TO BE USED WITH AIRCRAFTMODIFICATION CIS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-4071-3BAGGAGE PLACARD MODEL B300 CIS ATA :B300 FL-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A PLACARD DENOTING WEIGHTLIMITATIONS FOR THE AFT BAGGAGE COMPARTMENT. THIS KIT IS TO BE USED WITH AIRCRAFTMODIFICATION CIS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4072-1FLAP RIB REPLACEMENT ATA :100, A100 B-1 THRU B-94, B-100 THRU B-247200, B200 BB-2, BB-6 THRU BB-1518200C, B200C BL-1 THRU BL-72, BL-124 THRU BL-140200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-38300 FA-1 THRU FA-230300 (FAA) FF-1 THRU FF-19A100 (U-21F) B-95 THRU B-99A100-1 BB-3 THRU BB-5A200 (C12C) BC-1 THRU BC-75, BD-1 THRU BD-30A200C (UC12B) BJ-1 THRU BJ-66A200CT (C12’S, FWC12D, RC12’S) BP-1 THRU BP-63, FE-1 THRU FE-36, FC-1

THRU FC-3, GR-1 THRU GR-19B100 BE-1 THRU BE-137B200C (UC12F, UD12M, RC12M, C12F) BU-1 THRU BU-10, BV-1 THRU BV-12, BP-64

THRU BP-71, BW-1 THRU BW-14, BL-73THRU BL-112, BL-118 THRU BL-123

B200CT (RC12F, FW) BU-11, BU-12,FG-1, GD-2

B300 FL-1 THRU FL-127C90, C90-1, C90A LJ-567 THRU LJ-1418E90 LW-1 THRU LW-347F90, F90-1 LA-1 THRU LA-237H90 T44A LL-1 THRU LL-61"OPTIONAL" SB NO. 2629, AUGUST, 1995THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION REQUIRED TO REPAIR AND ORREINFORCE THE LEADING EDGE OF THE OUTBOARD FLAP IN THE AREA OF THE ACTUATOR ATTACHBRACKET.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8MEN : N/A


KIT CATALOG

101-4074-1FLAP RIB REPLACEMENT, LH OR RH FIX ATA :B300 FL-1 THRU FL-127B300C FM-1 THRU FM-8B300C (CS) FN-1"OPTIONAL" SB NO. 2629, AUGUST, 1995THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION REQUIRED TO REPAIR AND ORREINFORCE THE LEADING EDGE OF THE OUTBOARD FLAP IN THE AREA OF THE ACTUATOR ATTACHBRACKET.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8MEN : N/A

101-4076-1DOUBLER, WING TO FUSELAGE ATA :300 FA-2 AND AFTER300 (FAA) FF-1 AND AFTERB200 BB-1158, BB-1167, BB-193 AND AFTERB200C BL-124 AND AFTERB200CT BN-5 AND AFTERB200T BT-31 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DOUBLER ON EACH SIDE OF THE BELLY OFTHE AIRCRAFT BETWEEN THE SPARS FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PR-1440 B-1/2 (PR1440B1/2), METALSET A-4 (METALSET A4), DEVCON-F (DEVCON F) ANDEA9309NA (EA9309 QT) NOT FURNISHED. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOUCAN PROCURE LOCALLY.

WT. CHANGE : WT: 7.0 LBS: MOMENT: 1456 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-4077-1SPAR ASSEMBLY FATIGUE INSPECTION, COLD WORKING ATA :300 FA-1 THORUGH FA-87A200CT (C-12D) BP-46 THRU BP-51A200CT (C-12F) BP-52 THRU BP-63A200CT (RC-12H) GR-14 THORUGH GR-19B200 BB-1158, BB-1167, BB-1193 THRU BB-1349B200 (C-12R) BW-1 THRU BW-24B200C (C-12F) BL-73 THRU BL-135B200C (FW-II) BV-11, BV-12B200C (UC-12F) BU-1 THRU BU-12B200C (UC-12M) BV-1 THRU BV-10B200CT (RC-12M) FG-1, FG-2B200T BT-31 THRU BT-33THIS KIT PROVIDES PARTS AND INFORMATION ON COLD WORKING FOR FATIGUE INSPECTION OF THEREAR SPAR ASSEMBLY ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NAS1097AD4 RIVET, MS20426AD4-7 RIVET, MS20426AD3-5 RIVET, PR1428 SEALANT,NAS1739B4 RIVET, MS20426AD4 RIVET, MS20470AD4-5 RIVET, MS20426AD6 RIVET, PR1440SEALANT, AND EA9309 QT ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


101-4077-3SPAR ASSEMBLY FATIGUE INSPECTION, COLD WORKING ATA :300 FA-88 THORUGH FA-230300 (FAA) FF-1 THORUGH FF-19A200CT (RC-12K) FE-1 TO FE-9A200CT (RC-12N) FE-10 THRU FE-24A200CT (RC-12P) FE-25 TO FE-31, FE-33 AND FE-35A200CT (RC-12Q) FE-32, FE-34 AND FE-36B200 BB-1350 AND AFTERB200C BL-136 AND AFTERB200C (C-12R) BW-1 THRU BW-29B200CT BN-5 AND AFTERB200T BT-34 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERB300C (CS) FN-1THIS KIT PROVIDES INFORMATION ON COLD WORKING FOR FATIGUE INSPECTION OF THE REAR SPARASSEMBLY ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NAS1097AD4 RIVET, MS20426AD4-7 RIVET, MS20426AD3-5 RIVET, PR1428 SEALANT,NAS1739B4 RIVET, MS20426AD4 RIVET, MS20470AD4-5 RIVET, MS20426AD6 RIVET, PR1440SEALANT, AND EA9309 QT ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

101-4078-1SKIN CRACK, LOWER CENTER SECTION - INFORMATION ONLY ATA :100, A100 B-1 THRU B-94, B-100 THRU B-24765-90, A90, B90, C90, C90A LJ-1 THRU LJ-1490A100 (U21F) B-95 THRU B-99B100 BE-1 THRU BE-137E90 LW-1 THRU LW-347H90(T44A) LL-1 THRU LL-61THIS KIT PROVIDES INFORMATION NECESSARY TO FIX A SKIN CRACK BELOW THE MAIN SPAR ONINSERVICE AIRCRAFT. INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA9309NA EPOXY ADHESIVE AND SCRIM CLOTH REQUIRED, BUT IS NOT FURNISHEDWITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


101-4080-1PLACARD - OPERATING INSTRUCTIONS, AIRSTAIR DOOR ATA :65-90, 65-A90, B90, C90, C90A, E90, F90,F90-1, 100, A100, B100, 200, 200T, B200,B200T, 300, B300THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL AN AIRSTAIR DOOR OPERATINGINSTRUCTIONS PLACARD ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4081-1SKIN ASSY,TRAILNG EDGE LOW INFO ONLY ATA : 57300, B300, B300CA100-1A200, A200CT, 200, B200, 200CT, B200C,B200CT, B200TWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-4083-1ATTACH BOLT, WING, LOWER FORWARD ATA : 57200C/B200C BL-73 & AFTER200CT/B200CT BN-5 & AFTER200T/B200T BT-31 & AFTER300 FA-1 & AFTER, FF-1 THRU FF-19B200 BB-1158, BB-1167, BB-1193 & AFTERB300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1 & AFTERC90A LJ-1085, LJ-1088 AND AFTERF90 LA-226 THRU LA-236THIS KIT PROVIDES REPLACEMENT PARTS AND INFORMATION FOR ONLY THE LOWER FORWARD WINGATTACH BOLT & HARDWARE AT THE 5 YEAR SERVICE REPLACEMENT INTERVAL, AND AT ANY TIME THEWING IS REMOVED FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4083-3ATTACH BOLT, WING, LOWER FORWARD ATA : 57200 & B200 BB-1 THRU BB-1157, BB-1159 THRU

BB-1166, BB-1168 THRU BB-1192200C/B200C BL-1 THRU BL-72200CT/B200CT BN-1 THRU BN-4200T/B200T BT-1 THRU BT-30.THIS KIT PROVIDES REPLACEMENT PARTS AND INFORMATION FOR ONLY THE LOWER FORWARD WINGATTACH BOLT AND HARDWARE AT THE 5 YEAR SERVICE REPLACEMENT INTERVAL, AND AT ANY TIMETHE WING IS REMOVED FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4084-1CABIN AIRSTAIR,LATCH BOLTS ATA : 52ALL MODELS 200, 200T, B200, B200T, 300,AND B300.(NON-CARGO DOOR).THIS KIT PROVIDES THE CABIN AIRSTAIR DOOR LATCH BOLTS REQUIRED FOR REPLACEMENT INACCORDANCE WITH THE CHAPTER 4 MAINTENANCE MANUAL LIMIT OF 6000 HOURS FOR ALL IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3-4 HOURS.MEN : 1 (MAN)


KIT CATALOG

101-4085-1CABIN AIRSTAIR,UPPER HOOK MECH ATA : 52ALL MODEL 200, 200T, B200, B200T, 300, &B300 (NON-CARGO DOOR).THIS KIT PROVIDES THE CABIN AIRSTAIR DOOR UPPER HOOK MECHANISM COMPONENTS REQUIREDFOR REPLACEMENT IN ACCORDANCE WITH THE CHAPTER 4 MAINTENANCE MANUAL LIMIT OF 12000HOURS FOR ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4091-0001CABLE, AIRSTAIR/CARGO DOOR 8,000 CYCLES REPLACEMNT ATA :200C AND 200CT ALL MODELS KING AIR CARGO DOOR

AIRCRAFTA200C AND A200CTB200C AND B200CTB300CTHIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACING AIRSTAIR DOOR CABLES ANDASSOCIATED HARDWARE IN ACCORDANCE WITH THE CHAPTER 4 MAINTENANCE MANUAL LIMIT OF 8,000CYCLES FOR ALL IN-SERVICE AIRCRAFT.


101-4091-0003CABLE, AIRSTAIR/CARGO DOOR 8,000 CYCLES REPLACEMNT ATA :200C AND 200CT ALL MODELS - KING AIR CARGO DOOR

AIRCRAFTA200C AND A200CTB200C AND B200CTB300CTHIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACING CARGO DOOR CABLES AND ASSOCIATEDHARDWARE IN ACCORDANCE WITH THE CHAPTER 4 MAINTENANCE MANUAL LIMIT OF 8,000 CYCLES FORALL IN-SERVICE AIRCRAFT.



KIT CATALOG

101-4310-1PLACARD INSTALLATION, EMERGENCY EXIT ATA : 52(RC-12M) BV-11 & BV-12100, A100 B-1 THRU B-94 & B-100 THRU B-247200 & B200 BB-2, & BB-6 THRU BB-1604200C & B200C BL-1 THRU BL-72 & BL-124 THRU BL-140200CT & B200CT BN-1 THRU BN-4200T & B200T BT-1 THRU BT-3899, 99A, A99A, B99, C99 U-1 THRU U-239A100(U-21F) B-95 THRU B-99A100-1(U-21J) BB-3 THRU BB-5A200(C-12A,C-12C) BD-1 THRU BD-30, BC-1 THRU BC-75A200C(UC-12B) BJ-1 THRU BJ-66;A200CT(C-12D) BP-1, BP-22 & BP-24 THRU BP-51A200CT(CT-12F) BP-52 THRU BP-63A200CT(FWC-12D) BP-7 THRU BP-11A200CT(RC-12D) GR-1 THRU GR-13A200CT(RC-12G) FC-1 THRU FC-3A200CT(RC-12H) GR-14 THRU GR-19A200CT(RC-12K) FE-1 THRU FE-9A200CT(RC-12N) FE-10 THRU FE-24A200CT(RC-12P) FE-25 THRU FE-31, FE-33 & FE-35A200CT(RC-12Q) FE-32, FE-34 & FE-36B100 BE-1 THRU BE-137B200C(C-12F) BL-73 THRU BL-112 & BL-118 THRU BL-123,

BP-64 THRU BP-71B200C(UC-12F) BU-1 THRU BU-10B200C(UC-12M) BV-1 THRU BV-10B200CT(FW-11) FG-1 AND FG-2B200CT(RC-12F) BU-11 & BU-12"MANDATORY" SB NO. 52-3096THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL AN AIRSTAIR DOOR OPERATINGINSTRUCTIONS PLACARD ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4310-3PLACARD INSTALLATION, EMERGENCY EXIT ATA :300, B300, B300C, B300C(CS)THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL EXTERIOR PLACARDS (DECALS)ON THE EMERGENCY EXIT HATCH ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-4410-STIFFNER, AFT SHELF ATA : 53WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-4410-1STIFFENER, AFT SHELF ATA : 53B200 BB-1312, BB-1318 THROUGH BB-1763B200C BL-131 THROUGH BL-142B200T BT-33 THROUGH BT-43.THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL SUPPORT BRACKETS ON THELOWER AFT AVIONIC SHELF ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLE

EST. MAN/HRS:EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5006-1 SOXYGEN BOTTLE 76 CU. FT. ATA :200 BB-2 THRU BB-37SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL 76 CU. FT. OXYGEN BOTTLE ON AIRCRAFTWITHOUT 101-5007 KIT. IF USED MUST ALSO USE 101-5008-1 KIT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : N/A

101-5006-7 SINSTALLATION OF 76 CU. FT. OXYGEN BOTTLE ATA :200 BB-38 THRU BB-54, BB-7 THRU BB-37SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL 76 CU. FT. OXYGEN BOTTLE ON AIRCRAFTWITHOUT 101-5007 KIT AND AIRCRAFT WITH 101-5007 KIT INSTALLED. IF USED MUST ALSO USE 101-5008-1KIT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : N/A

101-5007-1 SOXYGEN SYSTEM AUTOMATIC DEPLOYMENT ATA :200 BB-14, BB-21, BB-23, BB-27, BB-32SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL AN AUTOMATIC DEPLOYMENTOXYGEN SYSTEM AND TO RELOCATE EXISTING TEMPERATURE SENSOR TO THE FORWARD CABIN.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : N/A


KIT CATALOG

101-5007-11 SOXYGEN SYSTEM AUTOMATIC DEPLOYMENT ATA :200 BB-20, BB-25, BB-37SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL AN AUTOMATIC DEPLOYMENTOXYGEN SYSTEM AND TO RELOCATE THE EXISTING TEMPERATURE SENSOR TO THE FORWARD CABIN.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : N/A


101-5007-3 SOXYGEN SYSTEM AUTOMATIC DEPLOYMENT ATA :200 BB-6 THRU BB-11, BB-13, BB-15 THRU

BB-19, BB-22, BB-24, BB-26, BB-28 THRUBB-31, BB-34, BB-36

SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL AN AUTOMATIC DEPLOYMENTOXYGEN SYSTEM AND TO RELOCATE EXISTING TEMPERATURE SENSOR TO THE FORWARD CABIN.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : N/A

101-5007-7 SOXYGEN SYSTEM AUTOMATIC DEPLOYMENT ATA :200 BB-40, BB-43, BB-45, BB-48, BB-50, BB-51,

BB-53SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL AN AUTOMATIC DEPLOYMENTOXYGEN SYSTEM AND TO RELOCATE EXISTING TEMPERATURE SENSOR TO THE FORWARD CABIN.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : N/A


KIT CATALOG


101-5008-1 SMASK INSTALLATION, CREW DILUTER DEMAND ATA :200 BB-2 THRU BB-53SI NO. 0776-341 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL QUICK DONNING DILUTERDEMAND CREW MASKS. MUST BE USED WITH KIT 101-5006 WHICH INSTALLS A HIGH FLOW REGULATORAND A 76 CU. FT. OXYGEN BOTTLE.WT. CHANGE : N/AEST. MAN/HRS: : 32MEN : N/A

101-5034-1 SMIRROR INSTALLATION, RH AFT PARTITION ATA :200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERA100 B-91 THRU B-93, B-94 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A VANITY ON THE RH AFT PARTITION.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : N/A

101-5035-1 SAIR CONDITIONING PLUMBING AND PRESSURE SWITCH ATA :200 BB-2, BB-6 THRU BB-33, BB-35 THRU

BB-122, BB-124 THRU BB-344200T BT-1 THRU BT-3SI NO. 0968 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LARGER DIAMETER HIGH PRESSURE LINEAND A NEW PRESSURE SWITCH TO THE AIR CONDITIONER SYSTEM. THIS KIT IS APPLICABLE TOAIRPLANES THAT HAVE COMPLIED WITH SERVICE INSTRUCTION NO. 0820-410 REVISION I OR SUBWT. CHANGE : N/AEST. MAN/HRS: : 14MEN : N/A


KIT CATALOG

101-5035-3 SAIR CONDITIONING PLUMBING AND PRESSURE SWITCH ATA :200 BB-2, BB-6 THRU BB-33, BB-35 THRU BB-120SI NO. 0968 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LARGER DIAMETER HIGH PRESSURE LINEAND A NEW PRESSURE SWITCH TO THE AIR CONDITIONER SYSTEM. THIS KIT IS APPLICABLE TOAIRPLANES THAT HAVE NOT COMPLIED WITH SERVICE INSTRUCTION NO. 0820-410 REVISION I ORWT. CHANGE : N/AEST. MAN/HRS: : 14MEN : N/A

101-5035-5 SAIR CONDITIONING PLUMBING AND PRESSURE SWITCH ATA :200THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PRESSURE SWITCH IN THE EARLY 200’STHAT DO NOT ALREADY HAVE THE SWITCH INSTALLED. WITH THIS SWITCH AND THE PRESSURE RELIEFVALVE INSTALLED, REFRIGERANT KITS 101-5163 FOR R134A RETROFIT OR 101-5169 FOR F

NOTENOTENOTENOTE:::: TUBE ASSEMBLY, 101-555143-5, IS REQUIRED FOR INSTALLATION, BUT WILL BE SUPPLIEDWITH KIT 101-5163, 101-5149 OR 101-5069.


101-5037-1 SELECTRIC BONDING, STATIC ELIMINATION ATA :200 BB-2 THRU BB-391200T BT-1 THRU BT-3SI NO. 1003 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL STATIC ELIMINATION BOND JUMPERS ON THEENGINE COWLINGS AND LANDING GEAR DOORS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : N/A

101-5037-3 SDRAIN TUBE, FUSELAGE, IMPROVED ATA :200 BB-2 THRU BB-366, BB-369 THRU BB-375,

BB-377 THRU BB-413200T BT-1 THRU BT-4SI NO. 1003 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED DRAIN TUBE AFT OF THE AFTPRESSURE BULKHEAD.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : N/A


KIT CATALOG

101-5037-5 SELECTRIC BONDING, STATIC ELIMINATION ATA :200 BB-2 THRU BB-341200T BT-1 THRU BT-4SI NO. 1003 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL CONDUCTIVE STRIPS ON THE DORSAL FINAND FUSELAGE AREAS.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : N/A

101-5039-1 PCHARTHOLDER, BEECHCRAFT CONTROL WHEEL, 720 SERIES ATA :100, A100 B-1 THRU B-247200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTER300 FA-1 AND AFTER300C FE-1 AND AFTERB100 BE-1 THRU BE-137C90, C90A LJ-502 AND AFTERE90 LW-1 THRU LW-347F90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CHART HOLDER WHICH ALLOWS ADEQUATENIGHT TIME LIGHTING OF MAPS AND CHARTS WITHOUT INTERFERING WITH THE PILOT’S NIGHT VISION.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 3 FOR ADDITIONAL INFORMATION.WT. CHANGE : N/AEST. MAN/HRS: : .5 TO 1.5MEN : N/A

101-5040-1 PCARGO RESTRAINT SYSTEM ATA :200C, 200CTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A CARGO RESTRAINT SYSTEMON INSERVICE AIRCRAFT. A COPY OF THIS KIT DRAWING MUST BE INSERTED IN THE AIRCRAFTS FLIGHTMANUAL ALONG WITH A CURRENT REVISION OF FLIGHT MANUAL SUPPLEMENT NO. 131536.WT. CHANGE : N/A (INSTALLATION AID)EST. MAN/HRS: : 2MEN : N/A


KIT CATALOG

101-5041-1 SSTRESS FREE WINDSHIELD ATA :KING AIR 65-90, 65-A90, B90, C90, C90A,E90, F90, F90A, 100, A100, B100SUPER KING AIR 200, 200C, 200T, 200CT,B200, B200C, B200T, B200CTSUPER KING AIR 300, 300C, B300, B300CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON INSERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR BOTH WINDSHIELDS.

NOTENOTENOTENOTE:::: PR1440B1/2 6 OZ. K SEALER (6 EACH PER KIT), EC1300L 1/2 PT AND A400 ADHESIVE (2EACH PER KIT) REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY, OR FROM RAPID.


101-5041-3 SSTRESS FREE WINDSHIELD ATA :KING AIR 100, A100, B100KING AIR 200, 200C, 200T, 200CT, B200,B200C, B200T, B200CTKING AIR 300, 300C, B300, B300CKING AIR 65-90, 65-A90, B90, C90, C90A,E90, F90, F90ATHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON INSERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR ONE WINDSHIELD.

NOTENOTENOTENOTE:::: PR1440B1/2 6 OZ. K SEALER (3 EACH PER KIT), EC1300L 1/2 PT AND A400 ADHESIVE (1EACH PER KIT) REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY, OR FROM RAPID.



101-5045-1 SWINDOW, CABIN, FROST FREE ATA :100, A100 B-1 THRU B-247200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTERB100 BE-1 THRU BE-137THIS KIT PROVIDES PARTS AND INFORMATION TO MAKE THE 11 CABIN WINDOWS FROST FREE ON THEINSERVICE AIRCRAFT:

NOTENOTENOTENOTE:::: THIS KIT DOES NOT COVER AFT TEARDROP WINDOWS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 10MEN : N/A


KIT CATALOG

101-5045-3 SWINDOW, CABIN, FROST FREE ATA :90, A90, B90, C90 LJ-1 THRU LJ-568 THAT HAVE BEEN

MODIFIED BY KIT INSTALLATION 90-4065 POR 90-4065-1 P

C90, C90A LJ-569 AND AFTERE90 LW-1 THRU LW-347E90 LW-1 THRU LW-347F90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO MAKE THE 8 CABIN WINDOWS FROST FREE.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT COVER ANY AFT TEARDROP WINDOWS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 7 TO 9MEN : N/A

101-5046-1 SAIR CONDITIONER SERVICE PORT ATA :200 BB-2 THRU BB-556200C BL-1 THRU BL-4200T BT-1 THRU BT-9SI NO. 1079 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL REFRIGERANT SERVICE PORTS IN THE NOSEWHEEL WELL AND UNDER THE CABIN FLOORBOARDS TO FACILITATE SERVICING THE AIR CONDITIONERWITH THE ENGINES RUNNING.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : N/A

101-5048-5 SCONTAINER INSTL OXMASK (COMM KIT) ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5051-1 SFUEL QUANTITY PROBE INSTL ATA : 28200, A100, B100, C90, E90 & F90 ALL

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARE INBD LEADING EDGE FUEL PROBEON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT CONSISTS OF KIT DRAWING, FUEL PROBE & CONNECTOR. THERE IS NO GASKETWITH THIS KIT. YOU MUST ORDER ANY GASKETS SEPERATELY.



KIT CATALOG

101-5051-3 SFUEL QUANTITY PROBE INSTL ATA : 28

200, A100, B100, C90, E90 & F90 ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARE INBD BOX TANK FUEL PROBE ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT CONSISTS OF KIT DRAWING, FUEL PROBE AND CONNECTOR. ANY GASKET ORGASKETS THAT MAY BE REQUIRED TO BE REPLACED WHEN WORKING IN THIS AREAMUST BE ORDERED SEPARATELY.


101-5051-5 SFUEL QUANTITY PROBE INSTL ATA : 28200THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARE AUX. TANK FUEL PROBE ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NOTE: THE HOLE IS DIFFERENT ON THE -151 AND THE -167. THE KIT 101-5051-5 S CANBE USED IN PLACE OF THE 100-380006-167.PER SPARES ENG 2/28/01


101-5062-1 SVENT BLOWER INSTALLATION ATA : 21200, A200, B200, 200C, A200C, B200C, 200T,B200T, 200CT, A200CT, B200CTCOMMUNIQUE NO. 51THIS KIT PROVIDES PARTS & INFORMATION TO INSTALL A SPARES REPLACEMENT VENT BLOWER ANDSPEED CONTROLLER FOR THE 101-384026-5, 101-384026-7, OR 101-384100-1 VENT BLOWER FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: RATE OF AIR FLOW REPLACEMENT BLOWER IS 500CFM @ 4 INCHES,(MAIN RATING). THISIS A VARIABLE SPEED BLOWER.

WT. CHANGE : WT: +5.15 ARM: 67.5 MOMENT: +212.64EST. MAN/HRS: : 6 TO 8 HRSMEN : 1 (MAN)


KIT CATALOG

101-5065-1 SFLOW CONTROL VALVE(COMM KIT) ATA : 21200, 200C, 200T, 200CT, A200, A200C,A200CT, B200, B200C, & B200CTWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5068-1 PBAGGAGE LIMITATION(COMM KIT) ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5068-3 PBAGGAGE LIMITATION,AFT COMPARTMENT ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5068-5 PBAGGAGE LIMITATIONAFT COMPT ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5082-1 SFUEL SYSTEM SPLICEINSTL (KIT) ATA : 28WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5083-1 SAIR INLET REINF (KIT) ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5084-1 PEXPORT ICAO ANNEX 8 INSTLN ATA : 4300 FA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO MAKE CONVERSION TO MEET THE AIRWORTHINESSREQUIREMENTS OF ICAO AS PRESCRIBED BY "ANNEX 8" OF THE CONVENTION ON INTERNATIONAL CIVILAVIATION ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 HRSMEN : N/A


KIT CATALOG

101-5086-1HYDRAULIC BRAKE RESERVOIR INSTAL ATA : 32 A200CT C-12D, RC-12D, FWC-12D, AND RC-12GA100 U-21J.A200 C-12A AND C-12CA200C UC-12BB200C C-12FTHIS KIT SUPPLIES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE EXISTING HYDRAULICBRAKE RESERVOIR WITH A RESERVOIR HAVING A MOISTURE DRAIN VALVE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EF ITEMS REQUIRED BUT NOT FURNISHED WITH KIT: EC3911 PRIMER, EA9309 ADHESIVE,AND EC1792 ADHESIVE.


101-5088-1 SBRAKE DEICECLAMP INSTAL KIT ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5092-1 SREINF INSTL, SEATBELT ATTACHMENT ATA : 25"MANDATORY" SB NO. 2121WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5093-7 PREDUCED GROSS WEIGHT MODEL 300 ATA : 4WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5095-1 PSPEED WARNING INST ATA : 34WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5101-1 SBARRIER INSTL NOSE COMPARTMENT ATA : 30"OPTIONAL" SB NO. 2234

NOTENOTENOTENOTE:::: TOTAL 3900 AIRCRAFTWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-5106-1 SSERVO COVER INSTL ATA : 22WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5107-1 SSERVO COVER INSTLSPERRY SPZ 4000 ATA : 22WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5109-1 SOVERBOARD PRESSURIZATION DUMP SYSTEM ATA : 21"OPTIONAL" SB NO. 2285WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5119-1 STABLE IMPROVEMENTB200 ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5136-1 SFOREIGN CERTPLACARD INSTL ATA : 4WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5137-1 SCLOCK INSTL CONTROL WHEEL ATA : 25KIT-CLOCK INSTALLATION CONTROL WHEEL--THIS KIT PROVIDES PARTS & INFORMATION NECESSARY TOINSTALL A DAVTRON DIGITAL CHRONOMETER CONTROL WHEEL CLOCK ON ALL IN-SERVICE KING AIRMODEL AIRCRAFT

NOTENOTENOTENOTE:::: CLOCK COMES WITH BEECHCRAFT CONTROL WHEEL FACE PLATE ATTACHED.NOTENOTENOTENOTE:::: EFFECTS 3000+ AIRCRAFT

2 PER AIRCRAFT10 X 12 BAG

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5 TO 1.1 HOURSMEN : 1 (MAN)


KIT CATALOG

101-5138-1 SFOREIGN CERTIFICATION FIRE EXTINGUISHER INSTALLATION ATA : 4B300 FL-17 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FIRE EXTINGUISHER TO COMPLY WITHFOREIGN CERTIFICATION ON IN-SERVICE AIRCRAFTWT. CHANGE : WT: +.7 LB MOMENT: +64 LB-INEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

101-5141-1 SSEAT BELT INSTL U.K. ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5145-1 SSPEAKER INSTALLCABIN ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5146-1 SAILERON TRIMPULLEY ATA : 27WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5149-1 SA/C RELIEF VALVE INSTALL ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5149-3 SA/C RELIEF VALVE INSTALL ATA : 21

NOTENOTENOTENOTE:::: 389 TOTAL AIRCRAFTPENDING "M"S.B.#2681***S.B. CANCELLED, CONTACT TECH SUPPORT WITH QUESTIONS



KIT CATALOG


NOTENOTENOTENOTE:::: TOTAL 262 AIRCRAFTPENDING "M" S.B.#2681***S.B. CANCELLED, CONTACT TECH SUPPORT WITH QUESTIONS


101-5149-7 SA/C RELIEF VALVE INSTALL ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


NOTENOTENOTENOTE:::: S.B. CANCELLED, CONTACT TECH SUPPORT WITH QUESTIONSTS29557 7/16/03


101-5151-1 SFOREIGN CERTPLACARD INSTL ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-5160-5R134A REFRIG CHANGE,AIR CONDITION ATA : 21200 BB-2, BB-6 THRU BB-185, BB-187 THRU

BB-202, BB-204 THRU BB-269, BB-271 THRUBB-407, BB-409 THRU BB-468, BB-470 THRUBB-488, BB-490 THRU BB-509, BB-511 THRUBB-529, BB-531 THRU BB-550, BB-552 THRUBB-562, BB-564 THRU BB-572, BB-574 THRUBB-590, BB-592 THRU BB-608, BB-610 THRUBB-626, BB-628 THRU BB-646, BB-648 THRUBB-664, BB-666 THRU BB-694, BB-696 THRUBB-733, BB-735 THRU BB-792, BB-794 THRUBB-797, BB-799 THRU BB-822, BB-824 THRUBB-828, BB-830 THRU BB-853, BB-872,BB-873, BB-892 BB-893, & BB-912

200C BL-1 THRU BL-23, BL-25 THRU BL-36200CT BN-1200T B200T S/N: BT-1 THRU BT-22 & BT-28300 FA-1 THRU FA-230, FF-1 THRU FF-19B200 BB-734, BB-793, BB-829, BB-854 THRU

BB-870, BB-874 THRU BB-891, BB-894,BB-896 THRU BB-911, BB-913 THRU BB-990,BB-992 THRU BB-1051, BB-1053 THRUBB-1092, BB-1094, BB-1095, BB-1099 THRUBB-1104, BB-1106 THRU BB-1116, BB-1118THRU BB-1184, BB-1186 THRU BB-1263,BB-1265 THRU BB-1288, BB-1909 THRUBB-1300, BB-1302 THRU BB-1425, BB-1427THRU BB-1447, BB-1449, BB-1450, BB-1452,BB-1453, BB-1455, BB-1456, BB-1458 THRUBB-1514

B200C BL-37 THRU BL-57, BL-61 THRU BL-78,BL-124 THRU BL-140

B200CT BN-2 THRU BN-4B200T BT-23 THRU BT-27, BT-29 THRU BT-38THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT FROM R-12 TO R-134AREFRIGERANT IN THE AIR CONDITIONING SYSTEMS ON IN-SERVICE AIRCRAFT EQUIPPED WITH ORWITHOUT THE AFT EVAPORATOR OPTION.

NOTENOTENOTENOTE:::: "838" TEDLAR FILM TAPE, "RL100S" & "R134A" REFRIGERANT OIL, "AC FLUSH" FLUSHFLUID, "22-1428" & "22-1429" QUICK SEAL CAP REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE LOCALLY.



KIT CATALOG

101-5164-1REFRIGERANT CHANGE, A/C-FORWARD EVAPORATOR ONLY ATA :300 FA-1 & AFTER300C FB-1 & AFTERB200 BB-1244 & AFTERB200 (1300) BB-1296,BB-1296,BB-1302,BB-1305,BB-1309,

BB-1314,BB-1338 THRUBB-1343,BB-1376,BB-1383,BB-1384

B200 W/101-5149 KT INSTALLED BB-734,BB-793,BB-829,BB-854 THRUBB-870,BB-874 THRU BB-891,BB-894,BB-896THRU BB-911,BB-913 THRU BB-990,BB-992THRU BB-1116,BB-1118 THRU BB-12

B200C(UC12F) BU-1 THRU BU-12B200C(UC-12M) BV-1-BV-12B200CT(W 101-5149 KT INSTL) BN-2 THRU BN-4B200T BT-31 & AFTERB200T W/101-5149 KT INSTL BL-73 THRU BL-78THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT FROM R-12 TO R-134AREFRIGERANT IN THE AIR CONDITIONING SYSTEMS WITH FORWARD EVAPORATOR ONLY ON IN-SERVICEMODELS.

NOTENOTENOTENOTE:::: IF NEW COMPRESSOR REQ'D,ORDER 101-9078-1 KT & THIS KT.NOTENOTENOTENOTE:::: EARLIER B200S PRIOR TO BB-1243 W/O 101-5149 KT INSTLN & ETC SEE 101-5164-3.NOTENOTENOTENOTE:::: FOR ACFT WITH AFT EVAPORATORS SEE 101-5163-1,-3,-5 OR-7 FOR ACFT S/N.

NOTENOTENOTENOTE:::: "R134A" REFRIGERANT, "RL100H" OR "POE100" OIL (1 QT), & FLUSH FLUID REQUIRED BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


101-5164-3REFRIGERANT CHANGE, A/C-FORWARD EVAPORATOR ONLY ATA :B200 W/O 101-5149 BB-734,BB-793,BB-829,BB-854 THRU

BB-870,BB-874 THRU BB-891,BB-894,BB-896THRU BB-911,BB-913 THRU BB-990,BB-992THRU BB-1116,BB-1118 THRU BB-1243

B200C (C-12F) W/O 101-5149 BL-73 THRU BL-78B200C W/O 101-5149 BL-37 THRU BL-57,BL-61 THRU BL-72B200CT W/O 101-5149 BN-2 THRU BN-4B200T W/O 101-5149 BT-23 THRU BT-27,BT-29 & BT-30THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT FROM R-12 TO R-134AREFRIGERANT IN THE AIR CONDITIONING SYSTEMS WITH FORWARD EVAPORATOR ONLY ON IN-SERVICEMODELS WITHOUT KIT 101-5149 INSTALLED.

NOTENOTENOTENOTE:::: IF NEW COMPRESSOR REQ'D ORDER 101-9078-1 KT IN CONJUNCTION W/THIS KIT.NOTENOTENOTENOTE:::: FOR ACFT WITH AFT EVAPORATOR ALSO SEE 101-5163-1,-3,-5 OR-7 FOR ACFT S/N.NOTENOTENOTENOTE:::: FOR ACFT WITH AFT EVAPORATOR ALSO SEE 101-5163-1,-3,-5 OR-7 FOR ACFT S/N.



KIT CATALOG

101-5166-1FIRE EXTINGUISHER KIT ATA : 26 65-90 LJ-1 THRU LJ-113 65A50-4(U21E) BB-3 THRU BB-5 65-A90 LJ-114 THRU LJ-317 65-A90-2 LS-1 THRU LS-3 65-A90-3 LT-1 THRU LT-2100/A100 B-1 & AFTER200/B200(1300) BB-91 & AFTER200C/B200C BL-1 THRU BL-133, BV-1 THRU BV-12 & BU-1

THRU BU-12200CT/B200CT BN-1 THRU BN-4200T/B200T BT-1 THRU BT-32300/300 FA-2 THRU FA-195 & FF-1 THRU FF-19A100-1 BB-1,BB-2,BB-3A200(C12) BC-1 THRU BC-75A200(C12C) BD-1 THRU BD-30A200C BJ-1 THRU BJ-66A200CT BP-1 THRU BP-71B100 BE-1 & AFTERB90 & C90 LJ-318 THRU LJ-1062C90A LJ-1063 THRU LJ-1210E90 LW-1 & AFTERF90 LA-1 & AFTERH90(T44A) LL-1 THRU LL-61THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A REPLACEMENT FIREEXTINGUISHER ASSEMBLY IN BEECH AIRCRAFT KING AIR SERIES MODELS WITH 2-10, FR-2 1/2, FR2 3/4,344T FIRE EXTINGUISHERS INSTALLED AS STANDARD, STANDARD OPTION, OR MODIFICATIONINSTALLATIONS SUCH AS 36-5017-1 S OR -3 S KITS.WT. CHANGE : AS NOTED KT DRWG & TYPE INSTLNEST. MAN/HRS: : 3 TO 4 HRSMEN : 1 (MAN)


KIT CATALOG

101-5170-1COMPRESSOR, AIR CONDITIONING ATA :(C-12F) BP-52 THRU BP-63(FWC-12D) GR-1 THRU GR-13(RC-12G) FC-1 THRU FC-3(RC-12H) GR-14 THRU GR-19(UC-12F) BU-1 THRU BU-12200 & B200 BB-1 THRU BB-1438, BB-1440 THRU BB-1443200C & B200C BL-1 THRU BL-72 & BL-124 THRU BL-138200CT & B200CT BN-1 THRU BN-4200T & B200T BT-1 THRU BT-34300 FA-1 THRU FA-23099, A99, B99, C99 U-1 THRU U-239A100-1(U-21J) BB-3 THRU BB-5A200(C-12C) BC-1 THRU BC-75, BD-1 THRU BD-30A200C(UC-12B) BJ-1 THRU BJ-66A200CT(C-12D) BP-1, BP-22, BP-24 THRU BP-51B200C(C-12F) BL-73 THRU BL-112, BL-118 THRU BL-123B200CT(FWC-12II FG-1 & FG-2THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL COMPRESSORS FOR AIRCRAFT WITH AHEAVY DUTY COMPRESSOR AND R-12 REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5170-3COMPRESSOR, AIR CONDITIONING ATA :(C-12F) BP-52 THRU BP-63(FWC-12D) GR-1 THRU GR-13(RC-12G) FC-1 THRU FC-3(RC-12H) GR-14 THRU GR-19(UC-12F) BU-1 THRU BU-12200 & B200 BB-1 THRU BB-1438, BB-1440 THRU BB-1443200C & B200C BL-1 THRU BL-72, BL-124 THRU BL-138200CT & B200CT BN-1 THRU BN-4200T & B200T BT-1 THRU BT-34300 FA-1 THRU FA-23099, A99, B99, C99 U-1 THRU U-239A100-1(U-21J) BB-3 THRU BB-5A200(C-12C) BC-1 THRU BC-75 & BD-1 THRU BD-30A200C(UC-12B) BJ-1 THRU BJ-66A200CT(C-12D) BP-1, BP-22 BP-24 THRU BP-51B200C(C-12F) BL-73 THRU BL-112, BL-118 THRU BL-123B200CT(FWC-12II) FG-1 & FG-2THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL COMPRESSORS FOR AIRCRAFT WITH AHEAVY DUTY COMPRESSOR AND R-134A REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-5170-5COMPRESSOR, AIR CONDITIONING ATA : 300 FA-1 THRU FA-230(C-12F) BP-52 THRU BP-63(FWC-12D) GR-1 THRU GR-13(RC-12G) FC-1 THRU FC-3(RC-12H) GR-14 THRU GR-19(UC-12F) BU-1 THRU BU-12200 & B200 BB-1 THRU BB-1438, BB-1440 THRU BB-1443200C & B200C BL-1 THRU BL-72, BL-124 THRU BL-138200CT & B200CT BN-1 THRU BN-4200T & B200T BT-1 THRU BT-349, A99, B99, C99 U-1 THRU U-239A100-1(U-21J) BB-3 THRU BB-5A200(C-12C) BC-1 THRU BC-75 & BD-1 THRU BD-30A200C(UC-12B) BJ-1 THRU BJ-66A200CT(C-12D) BP-1, BP-22 BP-24 THRU BP-51B200C(C-12F) BL-73 THRU BL-112, BL-118 THRU BL-123B200CT(FWC-12II) FG-1 & FG-2THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL COMPRESSORS FOR AIRCRAFT WITH AHEAVY DUTY COMPRESSOR AND FR-12 REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5171-1COMPRESSOR SERVICE FITTING CHANGE ATA :200,200C,200T,200CT,B200,B200C,B200T,B200CT,A200(C-12C),A200C(UC-12B)A200CT(C-12D)(C-12F)(FWC-12D)(RC-12H),B200C(C-12F)(UC-12F),B200CT(FWC-12II),,B200C(UC-12M(C-12F),A200CT(RC-12K)(RC-12M)(RC-12P)B200C(C-12R)300,B300,B300C,B300C(CS)THE PURPOSE OF THESE KITS ARE TO PROVIDE A NEW COMPRESSOR FITTINGS INSTL WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPECOMPRESSORS. (FOR R-12 SERVICE PORTS).



KIT CATALOG

101-5171-3COMPRESSOR SERVICE FITTING CHANGE ATA :200,200C,200T,200CT,B200,B200C,B200T,B200CT,A200(C-12C),A200C(UC-12B)A200CT(C-12D)(C-12F)(FWC-12D)(RC-12H),B200C(C-12F)(UC-12F),B200CT(FWC-12II),B200C(UC-12M(C-12F),A200CT(RC-12K)(RC-12M)(RC-12P)B200C(C-12R)300,B300,B300C,B300C(CS)THE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPECOMPRESSORS. (FOR FR-12 SERVICE PORTS).


101-5171-5COMPRESSOR SERVICE FITTING CHANGE ATA :200,200C,200T,200CT,B200,B200C,B200T,B200CT,A200(C-12C),A200C(UC-12B)A200CT(C-12D)(C-12F)(FWC-12D)(RC-12H),B200C(C-12F)(UC-12F),B200CT(FWC-12II),B200C(UC-12M(C-12F),A200CT(RC-12K)(RC-12M)(RC-12P)B200C(C-12R)300,B300,B300C,B300C(CS)THE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPECOMPRESSORS. (FOR R-134A SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5171-7COMPRESSOR SERVICE FITTING CHANGE ATA :200,200C,200T,200CT,B200,B200C,B200T,B200CT,A200(C-12C),A200C(UC-12B)A200CT(C-12D)(C-12F)(FWC-12D)(RC-12H),B200C(C-12F)(UC-12F),B200CT(FWC-12II),B200C(UC-12M(C-12F),A200CT(RC-12K)(RC-12M)(RC-12P)B200C(C-12R)300,B300,B300C,B300C(CS)THE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPECOMPRESSORS. (FOR R-12 SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-5171-9COMPRESSOR SERVICE FITTING CHANGE ATA :200,200C,200T,200CT,B200,B200C,B200T,B200CT,A200(C-12C),A200C(UC-12B)A200CT(C-12D)(C-12F)(FWC-12D)(RC-12H),B200C(C-12F)(UC-12F),B200CT(FWC-12II),B200C(UC-12M(C-12F),A200CT(RC-12K)(RC-12M)(RC-12P)B200C(C-12R)300,B300,B300C,B300C(CS)THE PURPOSE OF THIS KIT IS TO PROVIDE A STEP PORT COMPRESSOR FITTINGS FOR USE WITH SPAREREPLACEMENT LIGHT WEIGHT, GM-TYPE COMPRESSORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5172-1HUMPSEAL INSTALLATION, WINDSHIELD ATA :ALL KING AIRS AND 1900 EXCEPT FORSOME OLDER 1900 MODELS WHICH DONOT USE THE LATEST WINDSHIELDDESIGN.TO INSTALL PPG KIT (DHS-001-1) ON THE LEFT WINDSHIELD FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: IF AIRCRAFT HAS INSTALLED KITS OR WINDSHIELDS IT IS ACCEPTABLE TO INSTALL PPGKITS. 129-5025-1 AND -2 WITH 114-384020-3 AND -4 WINDSHIELD. 114-5043-1 S AND -2 SWITH 101-384025-15, -16, -17, AND -18 WINDSHIELD. 90-3100-1 P AND -2 P WITH50-420069-29, -30, -31, -32, -33, AND -34 WINDSHIELD. INSTALL PPG KITS (DHS-001-1) TOREPAIR EXISTING GRAY OR BLACK HUMPSEALS, TO ADD BLACK HUMPSEALS TOWINDSHIELDS THAT DO NOT HAVE HUMPSEALS, OR TO REPLACE GRAY HUMPSEALSWITH BLACK HUMPSEALS FOR THE WINDSHIELD ASSEMBLIES INDICATED.

NOTENOTENOTENOTE:::: "PR14525B1/2 2.5 OZ" BLACK SEALER REQUIRED BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

101-5178-1CREW MASK REPLACEMENT, OXYGEN ATA : 35200C; 200T BT-7 AND AFTER200CT; A200C; A200CT; 200 AND B200 BB-310,BB-343,BB-383,BB-415,

BB-416,BB-418 THROUGH BB-448,BB-450THROUGH BB-1438,BB-1440 THROUGHBB-1443

300 FA-1300CA100 B-240 AND AFTERB100 BE-36 AND AFTERB200C BL-37 THROUGH BL-138B200C(C-12F)B200CT BN-1 THROUGH BN-4THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OXYGEN MASK STORAGE CUP ASSYS ANDCREW OXYGEN MASKS AS SPARE REPLACEMENTS FOR EXISTING DILUTER DEMAND OXYGEN MASKSWITH MICROPHONES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT REQUIRES EITHER -7, -9, -11 OR -13 TO COMPLETE THE INSTL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5178-11CREW MASK REPLACEMENT, OXYGEN ATA : 35THIS KIT PROVIDES SCOTT/EROS BRAND CREW MASKS (WITH COMFORT CONTROL) AND HOLDING CUPSTO COMPLETE THE -1 KIT.


101-5178-13CREW MASK REPLACEMENT, OXYGEN ATA : 35THIS KIT PROVIDES SCOTT/EROS BRAND CREW MASKS (WITHOUT COMFORT CONTROL) AND HOLDINGCUPS TO COMPLETE THE -1 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-5178-3CREW MASK REPLACEMENT, OXYGEN ATA : 35300 FA-2 AND AFTERB200 BB-1439, BB-1444 AND AFTERB200C BL-139 AND AFTERB200CT BN-5 AND AFTERB200T BT-35 AND AFTERB300; B300C; B300C (CS) ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL CREW OXYGEN MASK STORAGE CONTAINER,CREW OXYGEN MASK OUTLETS, AND CREW OXYGEN MASKS AS SPARE REPLACEMENTS FOR EXISTINGDILUTER DEMAND OXYGEN MASKS WITH MICROPHONES AND CONTAINER ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SUPPLIES PURITAN-BENNETT OR SCOTT/EROS CREW OXYGEN MASKS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5178-7CREW MASK REPLACEMENT, OXYGEN ATA : 35THIS KIT PROVIDES PURITAN/BENNETT BRAND CREW MASKS (WITH COMFORT CONTROL) AND HOLDINGCUPS TO COMPLETE THE -1 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5178-9CREW MASK REPLACEMENT, OXYGEN ATA : 35THIS KIT PROVIDES PURITAN/BENNETT BRAND CREW MASKS (WITHOUT COMFORT CONTROL) ANDHOLDING CUPS TO COMPLETE THE -1 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5196-0001BOOST REGULATOR ATA : 27WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-5301-1EMERGENCY LIGHTING INSTL, JAR OPS ATA : 33B200 BB-1444 & AFTERB200GT BY-1 & AFTERB200T BT-35 & AFTERTHIS KIT CONTAINS PARTS AND INFORMATION TO INSTALL EMERGENCY LIGHTING ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "MS20601B4W2" RIVETS REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED FLIGHT MANUAL REVISION/SUPPLEMENT HAS BEEN INCORPORATED. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.


101-5301-3EMERGENCY LIGHTING INSTL, JAR OPS ATA : 33B200C BL-141 & AFTERB200CGT BZ-1 & AFTERTHIS KIT CONTAINS PARTS AND INFORMATION TO INSTALL EMERGENCY LIGHTING ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: MS20601B4W2" RIVETS REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED FLIGHT MANUAL REVISION/SUPPLEMENT HAS BEEN INCORPORATED. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.


101-5307-1FLOOR INSTL, CARGO ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-6003-0001EMPENNAGE INSPECTION PANELS ATA : 55F90 LA-1 THRU LA-236"R"S.B. 55-3835THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ACCESS PANELS ONTO THE VERTICAL ANDHORIZONTAL STABILIZERS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MS20426AD4" RIVET & "EA9309NA" ADHESIVE REQUIRED BUT NOT SUPPLIED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : WT. +3.6 LB MOMENT: +1591 IN-LBEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-6003-0003EMPENNAGE INSPECTION PANELS ATA : 55200 & B200; 200T & B200T; 200C & B200C; &200CT & B200CT

BB-2 AND AFTER; BT-1 & AFTER; BL-1 &AFTER; BN-1 & AFTER UP TO THEEFFECTIVITY OF ECR14112. ( 2,175 A/C ASOF 5/07)

"R"S.B.55-3835THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ACCESS PANELS ONTO THE VERTICAL ANDHORIZONTAL STABILIZERS FOR IN-SERVICE AIRCRAFT.


WT. CHANGE : WT: +3.6 MOMENT: +1772 IN-LBEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-6003-0005EMPENNAGE INSPECTION PANELS ATA : 55

300 & 300(FAA) FA-1 THRU FA-230, & FF-1 THRU FF-19. 249"R"S.B.55-3835THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ACCESS PANELS ONTO THE VERTICAL ANDHORIZONTAL STABILIZERS FOR IN-SERVICE AIRCRAFT.



101-6003-0007EMPENNAGE INSPECTION PANELS ATA : 55B300, B300C & B300C(CS) FL-1 & AFTER; FM-1 & AFTER UP TO THE

EFFECTIVITY OF ECR14112; & FN-1 ONLY.535

"R"S.B.55-3835ZHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ACCESS PANELS ONTO THE VERTICAL ANDHORIZONTAL STABILIZERS FOR IN-SERVICE AIRCRAFT.


WT. CHANGE : WT. +3.6 LB MOMENT: +1895 IN-LB.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG


C-12C(A200); UC-12B(A200C); C-12D(A200CT); C-12F(A200CT); C-12F(B200C);FWC-12D

BC-1 THRU BC-75;BD-1 THRU BD-30;BJ-1THRU BJ-66;BP-1 & BP-22 & BP-24 THRUBP-51,BP-52 THRU BP-63,BP-64 THRUBP-71,BP-7 THRU BP-11;BU-1 THRU BU-10,BU-11 AND BU-12;BV-1 THRU BV-10,BV-11THRU BV-12;BW-1 THRU BW-29;FC-1 THRUFC-3;FG-1 & FG-2; & GR-1 THRU GR-13





A200CT(RC-12H);A200CT(RC-12K)(RC-12N)(RC-12Q)

GR-14 THRU GR-19;FE-1 THRU FE-36



WT. CHANGE : WT: +3.1 LB MOMENT: +1488 IN-LBEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-8005-11 SBRAKE DEICER INSTL ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG





101-8011-1 SBRAKE DEICE HOSEINSTAL KIT ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-8013-3 SMLG DOOR RETRACT MECHANISM IMPRO ATA : 32200 S/N:BB-2 THROUGH BB-73,BB-76 ANDBB-106 THROUGH BB-672200C S/N:BL-1 THROUGH BL-8200T S/N:BT-1 THROUGH BT-15.SI NO. 1114 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED SWIVEL AND LINK ASSEMBLYFOR THE HIGH FLOTATION LANDING GEAR ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 1 KIT PER AIRCRAFT-4 MAIN GEAR DOOR LINK ASSEMBLIESNOTENOTENOTENOTE:::: "LPS NO 3" LUBRICANT REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE

SEPERATELY FROM RAPID OR YOUR LOCAL SUPPLIER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : N/A


KIT CATALOG

101-8013-5 SMLG DOOR RETRACT MECHANISM IMPRO ATA : 32200 ,B200 BB-673 THROUGH BB-741200C BL-9 THROUGH BL-12200T BT-16 AND BT-18SI NO. 1114 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED SWIVEL AND LINK ASSEMBLYFOR THE HIGH FLOTATION LANDING GEAR ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 1 KIT PER AIRCRAFT-4 MAIN GEAR DOOR LINK ASSEMBLIESWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : N/A

101-8018-1HYDRAULIC LANDING GEAR INSTL KIT ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-8018-3HYDRAULIC LANDING GEAR INSTALATION KIT ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-8025-1 SDE ICE INSTL, WHEEL BRAKE ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-8027-1 PALUM NOSE WHEEL INSTL ATA : 32WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-8031-1 PHIGH FLOTATION LANDING GEAR ATA : 32

NOTENOTENOTENOTE:::: 4/20/04 KEEP 1 O/O OR O/H AT ALL TIMES PER HANK LEWIS. DTWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-8032-1 SMAIN WHEEL ASSEM REPLACEMENT ATA : 32A100-1, 200, 200C, 200CT, A200, A200C,A200CT, B200, B200C, B200CT, B200C(C-12F), & B200CT (FW)THIS KIT IS A SPARES REPLACEMENT FOR 10-8002-5 WHEEL ASSEMBLY THAT IS EQUIPPED WITH TYSON13685XL BEARINGS & 13621XL CUPS ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-8034-1SUPPORT ASSEMBLY ACTUATOR BEARING ATA : 32A200CT, B200C, B200T, B200CT, 300, B300 &B300C"MANDATORY" SB NO. 2658WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9005-1 PENG.FIRE EXTINGUISHER*RA ATA : 26THIS KIT IS FOR AIRCRAFT PRIOR TO BB-1204, WITH MECHANICAL GEAR USE -1, IF MODIFIED TO GEAR BYRAC KIT 101-8018 USE -3 KIT

NOTENOTENOTENOTE:::: REQUIRES 2 EA FIRE CONTAINERS 30301102 & SQUIBBS 13083-514 X 14 X 36

NOTENOTENOTENOTE:::: REVISION "A" TO KIT DRWG MADE NECESSARY CHANGES TO KIT TO USE KIT ONCURRENT PRODUCTION ACFT AS REQUESTED BY WARREN HILLWIG PH#316-676-6253LETTER. FOR BB1158, BB1167,BB1193, & BB1204 & AFTER, BL124 & AFTER, BT31 & AFTERAND FOR AIRCRAFT WITH KIT 101-8018 (HYDRAULIC L/G INSTALLED) SEE KIT 101-9005-3.

NOTENOTENOTENOTE:::: THIS IS AN EXPLOSIVE DEVICE AND CAN NOT SHIP TO DOMESTIC PEOPLE WHO ARE NOTATF LICENSE TO HANDLE EXPLOSIVE AND BOTH RAC AND RAPID HAVE A CONFIRMATIONCERTIFIED LICENSE ON HAND IN SHIPPING.ONLY MILITARY AND EXPORT SHIPMENT CAN BE MADE, AND IF THEY AREGOING THROUGH A FORWARDER, CERTIFIED PROOF OF THAT FORWARDER'S AFTLICENSE FOR HANDLING EXPLOSIVES MUST BE ON FILE WITH RAC AND RAPID. FOREXAMPLE, YOU CAN NOT SHIP TO FREIGHT FORWARDER, CONCORDIA IN GRAPEVINEUNLESS RAC/RAPID HAVE AN ATF LICENSE ON FILE FOR CONCORDIA!!


101-9005-3KIT, FIRE EXTINGUISHER ATA : 26

NOTENOTENOTENOTE:::: REQUIRES 2 EA FIRE CONTAINERS 30301102 & SQUIBBS 13083-5WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9012-1 SOIL VENT EXHAUST INSTL (COML KIT) ATA : 79WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9015-1 SFUEL VENT PLUMB ATA : 79WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9015-3 SFUEL VENT PLUMBING ATA : 79WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9015-5 SFUEL VENT PLUMB ATA : 79WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9016-1 SWASH RING INSTALLATION, ENGINE PT6A-41 & -42 ATA : 71200 BB-2 THRU BB-733, BB-735 THRU BB-792,

BB-794 THRU BB-828, BB-830 THRU BB-873,BB-893, BB-895, BB-912, BB-991

200C BL-1 THRU BL-36200CT BN-1200T BT-1 THRU BT-22THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE WASH RING FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT REQUIRED PER AIRCRAFTWT. CHANGE : +10.9 LBS. MOMENT: +1417 LBS-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-9016-3WASH RING INSTALLATION, ENGINE PT6A-41 & -42 ATA :

B200 BB-1439, BB-1444 & AFTERB200C BL-132 & AFTERB200CT BN-5 & AFTERB200T BT-31 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE WASH RING FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT

WT. CHANGE : +10.9 LBS. MOMENT: +1417 LBS-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-9016-5WASH RING INSTALLATION, ENGINE PT6A-41 & -42 ATA :B200T BT-23 THRU BT-30.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE WASH RING FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFTWT. CHANGE : WT: +10.9 LBS MOMENT: +1417 LBS-IN.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-9022-1PROP AUTOFEATHER & SYNCHROPHASER ATA : 61WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9025-1 SSYNCHROPHASER TARGPROP INSTL (KIT) ATA : 61100 PRIOR TO B-94 AIRCRAFT EQUIPPED WITH

TYPE I SYNCHROPHASER200 PRIOR TO BB-792 AIRCRAFT EQUIPPED

WITH TYPE I SYNCHROPHASER200C PRIOR TO BL-18 AIRCRAFT EQUIPPED

WITH TYPE I SYNCHROPHASER200T PRIOR TO BT-19 EXCLUDING BT-17

AIRCRAFT EQUIPPED WITH TYPE ISYNCHROPHASER

A100 PRIOR TO B-248 AIRCRAFT EQUIPPEDWITH TYPE I SYNCHROPHASER

C90 PRIOR TO LJ-942 AIRCRAFT EQUIPPEDWITH TYPE I SYNCHROPHASER

E90 PRIOR TO LW-342 AIRCRAFT EQUIPPEDWITH TYPE I SYNCHROPHASER

F90 PRIOR TO LA-100 AIRCRAFT EQUIPPEDWITH TYPE I SYNCHROPHASER

THIS KIT PROVIDES PARTS & INFORMATION NECESSARY TO INSTALL SYNCHROPHASER TARGETS ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

101-9027-1 SPROP MOUNT BOLT INSTALLATION ATA : 61WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9030-1 SFUEL PURGE TANK IN(COMM KIT) ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9037-3 SFUEL FLOW DIVI& DAMP VALVE ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9038-1 SSYNCHROPHASER TARGET INSTL ATA : 61WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9039-1 SHOT LIP DUCT STIFFINSTL ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9042-1 SMID COWLING GUIDE& AFT LATCH REIN ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9044-1 SS D4 STACK ATA : 78WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9047-1 SMID COWLING LATCHINSTL ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9048-1 SEXHAUST STACK INSTALLATION ATA : 78SB NO. 2372MATERIAL DETERMINATION IS MANDATORY, S/S BY # 101-9048-17WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9048-11EXHAUST STACK INSTALLATION ATA : 78WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9048-13EXHAUST STACK INSTALLATION ATA : 78200, B200, 200C, B200C, 200T, B200T,200CT, B200CT, A100, A200, A200CTMATERIAL DETERMINATION IS "MANDATORY", S/S BY 101-9048-17WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9048-17EXHAUST STACK INSTALLATION ATA : 78WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9048-19EXHAUST STACK INSTALLATION ATA : 78"MANDATORY" S/S FROM 101-9048-15WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9048-9EXHAUST STACK INSTALLATION ATA : 78MATERIAL DETERMINATION IS "MANDATORY" S/S BY 101-9048-17WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9049-1 SINLET DUCT REPLACEMENT KIT ATA : 54300"OPTIONAL" SB NO. 2299WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9050-1 SCOWLING STIFFENERINSTALL ATA : 54300 SERIESSB NO. 2315KIT PROVIDES PARTS AND INFORMATION TO INSTALL UPPER FORWARD COWLING DOUBLER ON IN-SERVICE KING AIR 200 SERIES AIRCRAFT LISTED ABOVE.

NOTENOTENOTENOTE:::: FOR MODEL300SERIES ACFT, SEE 101-9075-1 S & -3 S KITS,WHICH USES BRACKETS TOBEEF-UP COWLINGS.

WT. CHANGE : N/AEST. MAN/HRS: : 3 TO 5MEN : N/A

101-9052-1 SCOWLING DOOR LEDGE REPLACEMENT ATA : 54300 FA-2 THRU FA-211 AND FF-1 THRU FF-19THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HOOK LATCHES ON COWLING DOORS OF INSERVICE MODEL 300 AIRCRAFTWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9059-1 SEXHAUST STACK CONSTANT AREA ATA : 78WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9060-1 SAMBIENT AIR DUCTINSTL BLEED AIR ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9061-1 SAIR INLET DUCTSLEEVE INSTL ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9063-1 SHOT LIP FLEX HOSEREPL ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9066-1 SDEICE BOOT REINFORCEMENT INFO ONLY ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9067-1 SPNEUMATIC AIRINSTAL ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9067-3 SPNEUMATIC AIRINSTAL ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9068-1 SFIRE RESISTHOSE ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9074-1 SEXHAUST PIPEASSEM REPL ATA : 78WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9075-1 SCOWL BRACKET ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9075-3 SCOWL BRACKET ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9077-1DETECTOR INSTL, FIRE AND OVERHEAT ATA : 26B200 & 200 PRIOR TO BB871,BB872 THRU BB1438, AND

BB1440 THRU BB1443B200C & 200C PRIOR TO BL73, AND BL124 THRU BL138B200CT & 200CT UP TO AND INCLUDING BN4B200T & 200T UP TO AND INCLUDING BT34"OPTIONAL" SB NO. 2596, AUGUST,1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A CONTINUOUS LOOP FIREDETECTION SYSTEM ON IN-SERVICE MODEL B200 & 200 AIRCRAFT LISTED.

NOTENOTENOTENOTE:::: THIS KIT MODIFIES AIRCRAFT WITH A FIRE EXTINGUISHING SYSTEM INSTALLED.THIS KIT EXCLUDES AIRCRAFT CAA CERTIFIED FOR THE UNITED KINGDOM.

NOTENOTENOTENOTE:::: MS20995C20" SAFETY WIRE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.NOTE: THIS INSTALLATION IS NOT COMPLETE UNTIL THE AIRCRAFT FLIGHT MANUALSUPPLEMENT HAS BEEN INCORPORATED INTO THE PILOT'S OPERATING HANDBOOK.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

101-9077-3DETECTOR INSTL, FIRE AND OVERHEAT ATA : 26B200 & 200 PRIOR TO BB871, BB872 THRU BB1438,

AND BB1440 THRU BB1443B200C & 200C PRIOR TI BL73, AND BL124 THRU BL138B200CT & 200CT UP TO AND INCLUDING BN4B200T & 200T UP TO AND INCLUDING BT34"OPTIONAL" SB NO. 2596, AUGUST,1995KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A CONTINUOUS LOOP FIREDETECTION SYSTEM ON IN-SERVICE MODEL B200 & 200 AIRCRAFT LISTED.THIS KIT MODIFIES AIRCRAFT "WITHOUT" A FIRE EXTINGUISHING SYSTEM INSTALLED.THIS KIT EXCLUDES AIRCRAFT CAA CE

NOTENOTENOTENOTE:::: NOTE: "MS20995C20" SAFETY WIRE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.NOTE: THIS INSTALLATION IS NOT COMPLETE UNTIL THE AIRCRAFT FLIGHT MANUALSUPPLEMENT HAS BEEN INCORPORATED INTO THE PILOT'S OPERATING HANDBOOK.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : REF KIT DRWGEST. MAN/HRS: : 40MEN : 2 (MEN)

101-9078-1COMPRESSOR AIR CONDITIONING ATA : 21B200, B200C, B200T, B300 & A200CTCONTACT TECH SUPPORT WITH QUESTIONSWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9078-3A/C COMPRESSORINSTL KIT ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9078-5A/C COMPRESSORINSTL KIT ATA : 21


101-9081-1FUEL FLOAT VALVE, WING TIP ATA : 28WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

101-9081-5FUEL FLOAT VALVE,WING TIP ATA : 28WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9082-1TUBE BREAK WARN BLEED AIR INFO ONLY ATA : 26200, B200CT"OPTIONAL" SB NO. 2655WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9083-1REPR TUBE BREAKAGE WARNING INFO ONLY ATA : 26WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-9085-1EXHAUST STACKINSTL KIT ATA : 78(RC-12D) GR-1 THROUGH GR-13(RC-12G) FC-1 THROUGH FC-3(RC-12H) GR-14 THROUGH GR-19200 S/N: BB-2 THROUGH BB-912200C S/N: BL-1 THROUGH BL-36200CT S/N: BN-1, BL-24200T S/N: BT-1 THROUGH BT-28, BB-186THROUGH BB-1117A100-1 S/N: (U-21J) BB-3 THROUGH BB-5A200 S/N: BC-1 THROUGH BC-75, BD-1THROUGH BD-30, BJ-1 THROUGH BJ-66A200CT S/N: BP-1 THROUGH BP-51B200 S/N: BB-734 THROUGHBB-1523 AND AFTERB200C S/N: BL-37 THROUGH BL-112, BL-118THROUGH BL-128B200CT S/N: BN-2 THROUGH BN-4, BL-58THROUGH BL-60B200T S/N: BT-23, BB-1052, BT-29THROUGH BT-31"OPTIONAL" SB NO.2372THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LH & RH D4 14.50 STYLE EXHAUST STACKS ONIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: INSTALL THIS KIT ONLY IF KIT 101-9048 HAS ALREADY BEEN INSTALLED.WT. CHANGE : 19 LBS. MOMENT: 1919 LB-IN.EST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

101-9085-3EXHAUST STACKINSTL KIT ATA : 78 (RC-12H) GR-14 THROUGH GR-19(RC-12D) GR-1 THROUGH GR-13(RC-12G) FC-1 THROUGH FC-3200 BB-2 THROUGH BB-912200C BL-1 THROUGH BL-36200CT BN-1, BL-24200T BT-1 THROUGH BT-28, BB-186 THROUGH

BB-1117A100-1 (U-21J) BB-3 THROUGH BB-5.A200 BC-1 THROUGH BC-75, BD-1 THROUGH

BD-30, BJ-1 THROUGH BJ-66A200CT BP-1 THROUGH BP-51B200 BB-734 THROUGH BB-1523 AND AFTERB200C BL-37 THROUGH BL-112, BL-118 THROUGH

BL-128B200CT BN-2 THROUGH

BN-4, BL-58 THROUGH BL-60B200T BT-23, BB-1052, BT-29 THROUGH BT-31"OPTIONAL" SB NO.2372THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL RH D4 14.50 STYLE EXHAUST STACKS ON IN-SERVICE AIRCRAFT

NOTENOTENOTENOTE:::: INSTALL THIS KIT ONLY IF KIT 101-9048 HAS ALREADY BEEN INSTALLEDNOTENOTENOTENOTE:::: , , , , , , , ,, , , , ,

WT. CHANGE : 9.5 LBS. MOMENT: 959.5 LB-INEST. MAN/HRS: : 5MEN : 1 (MAN)


KIT CATALOG

101-9085-5EXHAUST STACK INSTL KIT ATA : 78 (RC-12H) GR-14 THROUGH GR-19(RC-12D) GR-1 THROUGH GR-13(RC-12G) FC-1 THROUGH FC-3200 BB-2 THROUGH BB-912200C BL-1 THROUGH BL-36200CT BN-1, BL-24200T BT-1 THROUGH BT-28, BB-186 THROUGH

BB-1117A100-1 (U-21J) BB-3 THROUGH BB-5.A200 BC-1 THROUGH BC-75, BD-1 THROUGH

BD-30, BJ-1 THROUGH BJ-66A200CT BP-1 THROUGH BP-51B200 BB-734 THROUGH BB-1523 AND AFTERB200C BL-37 THROUGH BL-112, BL-118 THROUGH

BL-128B200CT BN-2 THROUGH

BN-4, BL-58 THROUGH BL-60B200T BT-23, BB-1052, BT-29 THROUGH BT-31"OPTIONAL" SB NO.2372THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LH D4 14.50 STYLE EXHAUST STACKS ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: INSTALL THIS KIT ONLY IF KIT 101-9048 HAS ALREADY BEEN INSTALLED.WT. CHANGE : 9.5 LBS. MOMENT: 959.5 LB-INEST. MAN/HRS: : 5MEN : 5 (MEN)

101-9088-0001ENGINE IGNITION EXCITER BOX INSTALLATION ATA :B200 EQUIPPED WITH PT6A-42 ENGINES, PRIOR

TO S/N BB-1806THIS KIT CONTAINS INFORMATION AND HARDWARE TO INSTALL A NEW ENGINE IGNITION EXCITER BOXON EITHER THE LH OR RH ENGINE. THE IGNITION EXCITER BOX IS NOT A PART OF THIS KIT, BUT ISDEFINED IN P&W SB NO. 3390R1.

NOTENOTENOTENOTE:::: 2 PER AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-9108-0001ENGINE IGNITION EXCITER BOX INSTALLATION ATA :B200 EQUIPPED WITH PT6A-42 ENGINES, PRIOR

TO S/N BB-1806THIS KIT CONTAINS INFORMATION AND HARDWARE TO INSTALL A NEW ENGINE IGNITION EXCITER BOXON EITHER THE LH OR RH ENGINE. THE IGNITION EXCITER BOX IS NOT A PART OF THIS KIT, BUT ISDEFINED IN P&W SB NO. 3390R1.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

109-4011-1RIGHT AILERON SUBSPAR ATA : 27100 & A100 B-1 THRU B-9499 SERIES U-1 THRU U-239A100(U-21F) B-95 THRU B-99B100 BE-1 THRU BE-137, B-100 THRU B-247B90 LJ-318 THRU LJ-501C90 LJ-502 THRU LJ-1062C90A LJ-1063 THRU LJ-1562E90 LW-1 THRU LW-347F90 LA-1 THRU LA-236H90(T-44A) LL-1 THRU LL-61THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PARTIAL SUB SPAR FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "CR3245-04-01", "CR2248-4-2", "MS20470B3-4", "MS20470AD3-4", "MS20426B3-4" RIVETSREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM RAPID ORYOUR LOCAL SUPPLIER.


109-9000-5TANK INSTL FUEL PURGE ATA : 71E90 LW-334 THRU LW-347F90 LA-57 THRU LA-201, LA-203 & LA-204"MANDATORY" SB NO. 71-3185THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL PURGE SYSTEM FORIMPROVED RELIABILITY ON IN-SERVICE AIRCRAFT

NOTENOTENOTENOTE:::: "ALODINE","MIL-P-23377" PRIMER,"EC-2084" SEALANT & "1300L" SEALANT REQUIRED BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET


109-9011-1TANK INSTL ATA : 71C90A LJ-1063 THRU LJ-1516"MANDATORY" SB NO. 71-3185THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL PURGE SYSTEM FORIMPROVED RELIABILITY ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 8 (MEN)


KIT CATALOG

109-9012-1TANK INSTL, FUEL PURGE ATA : 71C90 LJ-901 THRU LJ-1062"MANDATORY" SB NO. 71-3185THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL PURGE SYSTEM FORIMPROVED RELIABILITY ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "ALODINE" & "MIL-P-23377" PRIMER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


109-9013-1TANK INSTL, FUEL PURGE ATA : 71F90 LA-202, LA-205 THRU LA-236"MANDATORY" SB NO. 71-3185THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL PURGE SYSTEM FORIMPROVED RELIABILITY ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEIGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

117-9000-1 SAIR CONDITIONER COMPRESSOR INSTALLATION, SPARES ATA :A200CTB200B300THIS KIT GIVES PARTS AND INFORMATION TO INSTALL A NEW STEP PORT LIGHT WEIGHT COMPRESSORAS SPARES FOR R12 REFRIGERATION SYSTEM AS INSTALLED ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MAY NEED TO ORDER 117-9000-5 WHEN ORDERING -1 S KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

117-9000-3AIR CONDITIONER COMPRESSOR INSTALLATION, SPARES ATA :A200CTB200B300THIS KIT GIVES PARTS AND INFORMATION TO INSTALL A NEW STEP PORT LIGHT WEIGHT COMPRESSORAS SPARES FOR FR12 OR R134A REFRIGERANT SYSTEM INSTALLED PER KIT 101-5160, 101-5163, 101-5169,130-5009, AND 130-5022.

NOTENOTENOTENOTE:::: MAY NEED TO ORDER 117-9000-5 WHEN ORDERING THIS -3 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

117-9000-5AIR CONDITIONER COMPRESSOR INSTALLATION, SPARES ATA :A200CTB200B200THIS KIT GIVES PARTS AND INFORMATION TO INSTALL STEP PORT FITTINGS INTO THE R134A OR FR12COMPRESSORS, 101-555211-3 OR -7 OR R12 COMPRESSORS, 101-555211-5 OR -9 WHICH THE EARLIERCOMPRESSOR DID NOT HAVE. THESE ARE BASIC FITTINGS WITH NO FILL PORTS. SEE SERVICE KIT101-5171 IF FILL PORTS ARE DESIRED.

NOTENOTENOTENOTE:::: MAY NEED TO ORDER THIS 117-9000-5 WHEN ORDERING -1 S OR -3 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-1200-1LEADING EDGE IMPROVEMENT ATA : 57300 FA-1 THROUGH FA-230B300 FL-1 THROUGH FL-207B300C FM-1 THROUGH FM-9B300C(CS) FN-1"M"S.B.24-3245 ISSUED 4/99THIS KIT PROVIDES INFORMATION AND PARTS FOR THE IMPROVEMENT OF LEADING EDGE INLET DUCTFOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: :"MEK" CLEANER,GLASS CLOTH,"FLEXT" FLEX,"951" HARDNER,"EPON 828"ADHESIVE,"MS20426AD3-3" RIVET NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 HRS. (IF REPAIR IS REQUIRED: 10 HRS.)MEN : 2 (MEN)

130-3004-1 SFIELD PERFORMANCEIMPROVEMENT ATA : 22B300 (350) FL1 THRU FL110. (SINGLE SYS) (DUAL"C" -3

S KITB300C FM2 THRU FM8 (WITH SINGLE FLT

DIRECTORY SYSTEM).THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO MODIFY IN-SERVICE MODEL B300(350) AIRCRAFT EQUIPPED WITH SINGLE FLIGHT DIRECTOR SYSTEM TO IMPROVE THE OVERALL FIELDTAKE-OFF PERFORMANCE.

NOTENOTENOTENOTE:::: MUST CONTACT COLLINS AVIONICS,CEDAR RAPIDS, IA. LOCAL DIST. OR VENDOR ONMODIFICATION OF EQPMNT ON ACFT &/OR REPLACEMENT UNITS FOR SMT85B SERVOMOUNT,SVO85B SERVO & APC65J AUTOPILOT COMPUTER REQ'D FOR TAKEOFFIMPROVMENT.

NOTENOTENOTENOTE:::: KIT 130-3005-1 S IS FURNISHED WITH THIS KIT, YOU DO NOT HAVE TO ORDERSEPERATELY.

NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT P/N: 130-590031-75 WILL BE REQUIRED TO COMPLETETHIS KIT INSTALLATION. IT IS NOT PART OF THE KIT AND MUST BE ORDEREDSEPARATELY TO INSURE IT IS CURRENT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 102 HRS.(BOTH KITS)MEN : 2 (MEN)


KIT CATALOG

130-3004-3 SFIELD PERFORMANCEIMPROVEMENT ATA : 22 B300 (350) FOR SINGLE FLT SYSTEM "C" -1 S KIT, S/N:

FL-1 THRU FL-110 (WITH DUAL FLIGHTDIRECTOR SYSTEMS).MODEL B300C S/N:FM-1 & FN-1 (WITH DUAL FLIGHTDIRECTOR SYSTEMS).

THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO MODIFY IN-SERVICE MODEL B300(350) AIRCRAFT EQUIPPED WITH DUAL FLIGHT DIRECTOR SYSTEMS TO IMPROVE THE OVERALL FIELDTAKE-OFF PERFORMANCE OF THESE AIRCRAFT:

NOTENOTENOTENOTE:::: KIT 130-3005-3 S IS FURNISHED WITH THIS KIT, IT IS NOT NECESSARY TO ORDER ITSEPERATELY

NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT P/N: 130-590031-75 IS REQUIRED TO COMPLETE INSTLNOF THIS KIT. IT IS NOT PART OF KIT AND MUST BE ORDEREDSAME TIME AS KIT TOINSURE IT IS CURRENT FROM YOUR LOCAL BEECH PTS CTR.

NOTENOTENOTENOTE:::: MUST CONTACT AVIONICS,CEDAR RAPIDS,IA. LOCAL DIST OR VR FOR MOD/OR ECH OFEQPMNT ON ACFT:SMT85B,SVO85B SERVO & APC65J A/P COMPTR4TAKEOFFIMPROVMNT.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 104 HRS.(BOTH KITS)MEN : 2 (MEN)

130-3008-1 PILOT HEATANNUNCIATION ATA : 31WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : N/A

130-3016-1CIRCUIT BREAKER RE-LOCATION ATA : 32300 FA-2 THROUGH FA-230300(FAA) FF-1 THROUGH FF-19B300 FL-1 THROUGH FL-207B300C FM-1 THROUGH FM-9B300C(CS) FN-1"MANDATORY" SB NO. 24-3245

NOTENOTENOTENOTE:::: 300 S/N: FA-2 THROUGH FA-230;300(FAA) S/N: FF-1 THROUGH FF-19;B300 S/N: FL-1THROUGH FL-207;B300C S/N: FM-1 THROUGH FM-9;B300C(CS) S/N: FN-1. 465 AIRCRAFTPOSSIBLE



KIT CATALOG

130-3017-1PITOT HEAT INDICATOR ATA : 30B300 FL-1 THRU FL-288B300C FM-1 THRU FM-10B300C (CS) FN-1THIS KIT PROVIDES PARTS AND INFORMATION FOR PITOT HEAT INDICATOR INSTALLATION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISIONS (OR SUPPLEMENTS) HAVE BEENINCORPORATED. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-3017-5PITOT HEAT INDICATOR ATA : 30B300 FL-289 AND AFTERB300C FM-11 AND AFTERB300C (CS) FN-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR PITOT HEAT INDICATOR INSTALLATION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISIONS (OR SUPPLEMENTS) HAVE BEENINCORPORATED. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-3018-1PITOT HEAT & STALL HEAT ANNUNCIATORS ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-3019-1NI CAD BATTERY ATA : 24B300 & B300C FL-215 AND AFTER, FM-10 AND AFTER AND

FN-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 101-381008-7 NI-CAD BATTERY IN PLACE OFLEAD ACID BATTERIES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION (OR SUPPLEMENT) HAS BEENINCORPORATED. MAY BE OBTAINED FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : -6 LBSMOMENT: -1166 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-3022-0001STALL WARNING MOD,MODEL B300 ATA : 27B300 FL-329, FL-381, FL-383 THRU FL-394 (12

AIRCRAFT)THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE 101-380005-35 LIFT COMPUTER WITH101-380005-39 LIFT COMPUTER ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-3025-0001COLD CATHODE LIGHTING PANEL-INFO ONLY ATA :300 FA-2 THRU FA-230 AND FF-1 THRU FF-19B300 FL-1 THRU FL-476B300C FM-1 THRU FM-12 & FN-1THIS KIT PROVIDES INFORMATION TO IMPROVE THE OPERATION OF THE CABIN INDIRECT LIGHTS WHENSWITCHING FROM BRIGHT TO DIM FOR IN-SERVICE AIRCRAFT.


130-3404-1ALTIMETER REPLACEMENT KIT ATA : 31WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-3405-1HF & ADF INSTL ATA : 23B300 FL-141, FL-152, FL-159, FL-169, FL-177 &

FL-179WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-3405-3HF & ADF INSTL ATA : 23B300 FL-141, FL-152, FL-159, FL-169, FL-177,

FL-179, FL-205 & FL-212WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

130-3407-1CVR INSTALLATION INFO ONLY ATA : 23B300 FL-30, FL-52, FL-62, FL-63, FL-65, FL-73,

FL-84, FL-87, FL-114 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY FOR INSTALLATION OF THE FAIRCHILD MODEL FA2100 CVR FORIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: WT. & BALANCE INFO: THE FA2100 WEIGHS 10.2 LBS. THE A100S WEIGHED 16.0 LBS AT ANARM OF 402.7 INCHES, FOR A -2335.9 LB-IN.MOMENT: THE A100A WEIGHED 22.3 LBS AT AN ARM OF 402.7 INCHES, FOR A -4873.2 LB-IN.

WT. CHANGE : SEE NOTESEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-3408-1ELT INSTALLATION,DUAL MODE INFO ONLY ATA : 25B300 FL-127 & AFTERB300C FM-9 & AFTERTHIS KIT PROVIDES INFORMATION ONLY FOR INSTALLATION OF THE ARTEX ELT C406-2 AND DUAL MODEROD ANTENNA (110-323) FOR IN-SERVICE AIRCRAFT. THIS KIT APPLIES TO FL-80 THRU FL-126, FM-5 THRUFM-8, AND FN-1, PROVIDED KIT 101-3210-1, ELT REMOTE SWITCH IS INSTAL

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED FLIGHT MANUAL REVISION (ORSUPPLEMENT) HAS BEEN INCORPORATED. MANUAL REVISIONS (OR SUPPLEMENTS)MAY BE OBTAINED FROM ANY COMPANY AUTHORIZED OUTLET.


130-3408-3ELT INSTALLATION,DUAL MODE INFO ONLY ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-3410-1FRENCH MOD ATA :B300 FL-301 AND AFTER AS APPROPRIATETHIS KIT PROVIDES INFORMATION & PARTS TO INSTALL THE EQUIPMENT REQUIRED TO CERTIFY A B300MODEL AIRCRAFT IN FRANCE.

NOTENOTENOTENOTE:::: "131681AA22-9""131681AA20-9""132088-22TG1T14""132088-22TG2T14"131681AA16-9""132088-22TG3T14""M27500-22-TE3T14""M27500-22-TE2T14"WIRE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: 130-3018-1 PITOT HEAT & STALL HEAT ANNUNCIATOR KIT INCLUDED WITH THIS KIT.WT. CHANGE : +72 LBS. MOMENT: +22142.0 IN-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-3411-1ALTIMETER INSTALLATION, RVSM ATA : 34B300 FL-1 THRU FL-351B300C FM-1 THRU FM-10"OPTIONAL" SB NO. 34-3507THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EXISTING COPILOT ALTIMETER (EITHERENCODING OR NON-ENCODING) P/N 10450-11950, 10450-11951, 101450-11952, OR 101450-11953 WITH AHIGH ACCURACY ENCODING ALTIMETER MANUFACTURED BY INNOVATIVE SOLUTIONS AN

NOTENOTENOTENOTE:::: IF REQUIRED, THE FOLLOWING EQUIPMENT MAY BE INSTALLED USING THE RAYTHEONAIRCRAFT FIELD SERVICE KITS LISTED. 130-3004, FIELD PERFORMANCE IMPROVEMENTKIT; 130-3005, FIELD PERFORMANCE, WIRING INSTALLATION KIT; 130-3006, RUDDERSERVO CABLE ALIGNMENT KIT. THESE KITS WILL INSTALL A COLLINS APC-65J AUTO-PILOT COMPUTER AND SVO-85B AUTO-PILOT SERVO ON AIRCRAFT FL-1 THRU FL-110AND FM-1 THRU FM-8. AIRCRAFT AFTER THESE S/N'S WERE DELIVERED FROM THEFACTORY WITH THIS EQUIPMENT. RAC MAY NOT HAVE FIELD SERVICE KITS TO INSTALLTHE ADC-85. SOME OTHER FAA APPROVED MEANS OF INSTALLING THIS EQUIPMENTMUST BE EMPLOYED PRIOR TO IMPLEMENTATION OF KIT 130-3411.

NOTENOTENOTENOTE:::: "PR-1440" SEALER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION (OR SUPPLEMENT OR LATER REVISION) HASBEEN INCORPORATED. MAY BE OBTAINED FROM ANY COMPANY AUTHORIZED OUTLET.


130-3412-0001AVIONICS UPGRADE ADC 85A ATA : 34WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-3413-0001AUDIO SWITCH PANEL REPLACEMENT ATA :B200 BB-1843 THRU BB-1856B300 FL-383 THRU FL-389 WHEN EQUIPPED

WITH SINGLE DME AND SINGLE ADFTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE 804-003 AND 805-003 SWITCH PANEL WITH804-001 AND 805-001 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-3413-0003AUDIO SWITCH PANEL REPLACEMENT ATA :B200 BB-1843 & AFTERB300 FL-383 & AFTER WHEN EQUIPPED WITH

SINGLE DME AND DUAL ADFTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE 804-002 AND 805-002 SWITCH PANEL WITH804-000 AND 805-000 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-3415-0001AVIONICS NOSE SHELF STRUCTURAL IMPROVEMENT ATA :B200 BB-1769, BB-1834 TO BB-1907B200C BL-148 AND BL-149B300 FL-329, FL-381, FL-383 THRU FL-393, FL-395

THRU FL-432, FL-434 & FL-435"R"S.B.# 34-3728THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO IMPROVE STIFFNESS OF THE LOWER NOSEAVIONICS SHELVES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA934NA" ADHESIVE & "132370AD3" RIVET REQUIRED, BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-3415-0003AVIONICS NOSE SHELF STRUCTURAL IMPROVEMENT ATA : 34B200 BB-1769, BB-1834 TO BB-1907B200C BL-148 AND BL-149B300 FL-329, FL-381, FL-383 THRU FL-393, FL-395

THRU FL-432, FL-434 & FL-435"R"SB #34-3728

NOTENOTENOTENOTE:::: "MS20426AD3" RIVET & "EA934NA" ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-3600-1EXTERNAL DC POWERSWITCH TRANSIENT ATA : 24B300 FL-1 THRU FL-323B300C FM-1 THRU FM-10 & FN-1C90A LJ-1288 THRU LJ-1633"RECOMMENDED" SB NO. 24-3363, 10/20/00THIS KIT CONTAINS PARTS AND INFORMATION TO ADD EXTERNAL DC POWER TRANSIENT SUPRESSIONFOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

130-4000-1 MBREAKIN & EXITMARKINGS INSTL ATA : 11WT. CHANGE :

IF BOTH KTS INSTALLED DOUBLE VALUE FOR WT.& MOMENTEST. MAN/HRS: : N/AMEN : 1 (MAN)


KIT CATALOG

130-4002-1ICE PROTECTION NOSE DOOR ATA : 30200, B200 BB-1 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTER300 FA-1 AND AFTERB200C (C-12F) BW-1 AND AFTERB200CGT BZ-1 AND AFTERB200GT BY-1 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERB300C (CS) FN-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ICE SHIELD ON THE L.H. NOSE AVIONICSDOOR FOR IN-SERVICE MODELS 200,B200,B200T,B200C,B200CT,B200CT (C-12F),300,B300,B300C & B300C(CS) AIRCRAFT:

NOTENOTENOTENOTE:::: REF A/R ITEMS NOT FURNISHED W/KIT BUT REQUIRED: "P900" EPOXY SURFACER W/CAT;"467-9" PINHOLE FILLER; "ALODINE 1000" COATING; "EA960F QT" ADHESIVE; SCRIM CLOTH"AF3306 "OR" AF3306-2"; "EA9309NA" OR "EA9309 QT" ADHESIVE; "CA41B" CATALYSTWHICH SHOULD BE P/O: "467-9" FILLER ABOVE; & "528-306" ANTI-STATIC BLACK PAINT W/"910-464" PAINT CATALYST(ALT A-S PNT: 528-104). IF OUT, ORDER LOCALLY.

WT. CHANGE : 1.6 LBS, MOMENT: 115 IN-LBS. FOR -1 OR -3 KIT IS INSTALLED.EST. MAN/HRS: : 8-10MEN : 1 (MAN)

130-4002-3ICE PROTECTION NOSE DOOR ATA : 30200, B200 BB-1 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTER300 FA-1 AND AFTERB200C (C-12F) BW-1 AND AFTERB200CGT BZ-1 AND AFTERB200GT BY-1 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERB300C (CS) FN-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ICE SHIELD ON THE R.H. NOSE AVIONICSDOOR IN IN-SERVICE MODELS.

NOTENOTENOTENOTE:::: REF A/R ITEMS NOT FURNISHED W/KIT BUT REQUIRED: "P900" EPOXY SURFACER W/CAT;"467-9" PINHOLE FILLER; "ALODINE 1000" COATING; "EA960F QT" ADHESIVE; SCRIM CLOTH"AF3306" OR "AF3306-2"; "EA9309NA" OR "EA9309 QT "ADHESIVE; "CA41B" CATALYSTWHICH SHOULD BE P/O: "467-9" FILLER ABOVE; & "528-306" ANTI-STATIC BLACK PAINT W/"910-464" PAINT CATALYST(ALT A-S PNT: 528-104). IF OUT, ORDER FROM BEECH PTS.

WT. CHANGE : 1.6 LBS, MOMENT: 115 IN-LBS. FOR -1 OR -3 KIT INSTALLATION.- IF BOTH KTS INSTALLED DOUBLE VALUEFOR WT.& MOMENT.

EST. MAN/HRS: : 8-10MEN : 1 (MAN)


KIT CATALOG

130-4008-1GRAVEL RUNWAY PROTECTION INSTL ATA :300 FA-1B300 FL-1 & AFTERB300C FM-1 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL GRAVEL GUARDS ON INBOARD FLAPS, BELLYANTI-COLLISION LIGHT AND BELLY ANTENNAS FOR NON SPECIAL MISSION IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR1440B2" AND "PR1440B1/2" SEALANTS REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE LOCALLY.

WT. CHANGE : +8 LBS. MOMENT: +2058 LB-INEST. MAN/HRS: : 24 TO 30 HRSMEN : 1 (MAN)

130-4009-1WINDSHIELD WASHERINSTALLATION ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-4011-0001WING BOLT COVER INSTALLATION KIT ATA : 57B300 FL-133 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL WING BOLT COVER INSTL FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309NA" EPOXY ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-4400-0001CENTRAL FIN INSTL,DUAL ATA :B300 FL-1 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DUAL VENTRAL FINS FOR IN-SERVICEAIRCRAFT

NOTENOTENOTENOTE:::: "EA9309NA" ADHESIVE,"METALSET A-4" FILLER, "EA960F" SURFACEFILLER,"MS20426AD3""MS20470AD4""MS20470AD5" RIVETS,"PR1440B1/2"SEALANT,"528-306" ANTI-STATIC PAINT, & "910-119" CATALYST FOR ANTI-STATIC PAINTREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : +26.0 LBS. MOMENT: +12,785 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-4400-0003CENTRAL FIN INSTL,DUAL ATA :B300 FL-1 & AFTER, WITH STC SA5151NM

INCORPORATED ON AIRCRAFTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DUAL VENTRAL FINS FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309NA" ADHESIVE,"METALSET A-4" FILLER, "EA960F" SURFACEFILLER,"MS20426AD3""MS20470AD4""MS20470AD5" RIVETS,"PR1440B1/2"SEALANT,"528-306" ANTI-STATIC PAINT, & "910-119" CATALYST FOR ANTI-STATIC PAINTREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : +26.0 LBS. MOMENT: +12,785 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-5009-1REFRIGERANTCHANGE AIR ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5009-3REFIGERANTCHANGE AIR ATA : 21B300 & B300CCONTACT TECH SUPPORT WITH QUESTIONSWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5009-5REFRIGERANT CHANGE, AIR ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5010-1INSTL, AFTHEAT DISTRIBUTIO ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5011-3ACTUATOR ASSY/INSTL ELEVATOR TRIM ATA : 27WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

130-5011-9ACTUATOR ASSY/INSTL ELEVATOR TRIM ATA : 27"MANDATORY" SB NO. 2620...PENDING REC.SB NO. 27-3472 12/6/01WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5012-1FIRE EXTINGUISHERINSTALL ATA : 26WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5014-1CIS REQUIREMENTS ATA : ??WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5015-1SEAT BELT COVER TUBE, CABIN CHAIR KIT (DO NOT OCCUPY) ATA : 25B300 & B300CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL SEAT BELT COVER TUBES OVEREXISTING SEAT BELTS ON CABIN SEATS.

NOTENOTENOTENOTE:::: USED FOR TAKING SEAT OUT OF OPERATION, FOR ONE PILOT OPERATIONS, SUCH AS:FERRYING THE AIRCRAFT OVERSEAS AND ETC. ONE KIT, CONTAINS 2 TUBES, MAKINGTWO CHAIRS UNOCCUPIABLE.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : N/AMEN : N/A

130-5016-5PLACARDS, CHINESETRANSLATION ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5017-1CREW CHAIR UPDATE ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5018-1AIR CONDITIONINGINSTL, B300 ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

130-5018-3AIR CONDITIONING INSTL ATA : 21B300WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5022-1FR12 REFRIGERANT CHANGE, AIR CONDITIONING ATA : 21B300 FL-1 & AFTERB300C FM-1 & AFTERB300C (CS) FN-1 & AFTERTHIS KIT PROVIDES PARTS AND INSTRUCTIONS REQUIRED TO CONVERT R-12 REFRIGERANT IN THE AIRCONDITIONING SYSTEM TO A FR-12 REFRIGERANT SYSTEM FOR ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "FR12" REFRIGERANT, "POE" OIL, "838" TAPE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANY OUTLET.


130-5023-1PLACARD MOROCCAN CERTIFICATIONS KIT ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5024-1FURNISHINGINSTL ATA : 25THIS KIT IS FOR USE AT RAC OR RAC SERVICE CENTERS ONLYWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5026-1PLACARDS, PORTUGUESE TRANSLATION ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5026-3PLACARDS, PORTUGUESE TRANSLATION ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

130-5028-1SPANISH TRANSLATION PLACARD KIT ATA : 11B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PLACARDS AND DECALS WITH SPANISHTRANSLATIONS ON IN-SERVICE AIRCRAFT WITH STANDARD INTERIORS.

NOTENOTENOTENOTE:::: "EC2084" SEALER & "608" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-5028-3SPANISH TRANSLATION PLACARD KIT ATA : 11 B300C(CS) FN-1 & AFTER300 FL-1 & AFTERB300C FM-1 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PLACARDS AND DECALS WITH SPANISHTRANSLATIONS ON IN-SERVICE AIRCRAFT WITH FOLD-UP SEAT OPTION.

NOTENOTENOTENOTE:::: "EC2084" SEALER & "608" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


130-5028-5SPANISH TRANSLATION PLACARD KIT ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-5028-7SPANISH TRANSLATION PLACARD KIT ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

130-5068-1CABIN SEAT SHOULDERHARNESS STOP/OAK ATA : 25200/B200 BB-75 & AFTER200C/B200C BL-1 & AFTER200CT/B200CT BN-1 & AFTER200T/B200T BT-1 & AFTER300 FA-1 THRU FA-230A100 B-229 THRU B-247B100 BE-13 THRU BE-137B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1C90/C90A LJ-693 & AFTERE90 LW-193 THRU LW-347F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO INSTALL A STOP AND INSTRUCTIONPLACARD RETAINER ON THE CABIN CHAIR RETRACTABLE SHOULDER HARNESS ON IN-SERVICEAIRCRAFT, IF SO EQUIPPED.

NOTENOTENOTENOTE:::: COLOR IS OAK. RECOMMENDED FOR FAWN WEBBING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-5068-11CABIN SEAT SHLDER HARNESS STOP/CLEAR ATA : 25200/B200 BB-75 & AFTER200C/B200C BL-1 & AFTER200CT/B200CT BN-1 & AFTER200T/B200T BT-1 & AFTER300 FA-1 THRU FA-230A100 B-229 THRU B-247B100 BE-13 THRU BE-137B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1C90/C90A LJ-693 & AFTERE90 LW-193 THRU LW-347F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO INSTALL A STOP AND INSTRUCTIONPLACARD RETAINER ON THE CABIN CHAIR RETRACTABLE SHOULDER HARNESS ON IN-SERVICEAIRCRAFT, IF SO EQUIPPED.

NOTENOTENOTENOTE:::: COLOR IS CLEAR. RECOMMENDED FOR ANY COLOR WEBBING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-5068-3CABIN SEAT SHLDR HARNES STOP/GRAPHIT ATA : 25200/B200 BB-75 & AFTER200C/B200C BL-1 & AFTER200CT/B200CT BN-1 & AFTER200T/B200T BT-1 & AFTER300 FA-1 THRU FA-230A100 B-229 THRU B-247B100 BE-13 THRU BE-137B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1C90/C90A LJ-693 & AFTERE90 LW-193 THRU LW-347F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO INSTALL A STOP AND INSTRUCTIONPLACARD RETAINER ON THE CABIN CHAIR RETRACTABLE SHOULDER HARNESS ON IN-SERVICEAIRCRAFT, IF SO EQUIPPED.

NOTENOTENOTENOTE:::: COLOR IS GRAPHITE. RECOMMENDED FOR METRO GRAY OR BLACK WEBBING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-5068-5CABIN SEAT SHOULDERHARNES STOP/BLUE ATA : 25200/B200 BB-75 & AFTER200C/B200C BL-1 & AFTER200CT/B200CT BN-1 & AFTER200T/B200T BT-1 & AFTER300 FA-1 THRU FA-230A100 B-229 THRU B-247B100 BE-13 THRU BE-137B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1C90/C90A LJ-693 & AFTERE90 LW-193 THRU LW-347F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO INSTALL A STOP AND INSTRUCTIONPLACARD RETAINER ON THE CABIN CHAIR RETRACTABLE SHOULDER HARNESS ON IN-SERVICEAIRCRAFT, IF SO EQUIPPED.

NOTENOTENOTENOTE:::: OLOR IS BLUE. RECOMMENDED FOR MEDIUM BLUE OR NAVY WEBBING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-5068-7CABN SEAT SHLDER HARNES STOP/NEUTRAL ATA : 25200/B200 BB-75 & AFTER200C/B200C BL-1 & AFTER200CT/B200CT BN-1 & AFTER200T/B200T BT-1 & AFTER300 FA-1 THRU FA-230A100 B-229 THRU B-247B100 BE-13 THRU BE-137B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1C90/C90A LJ-693 & AFTERE90 LW-193 THRU LW-347F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO INSTALL A STOP AND INSTRUCTIONPLACARD RETAINER ON THE CABIN CHAIR RETRACTABLE SHOULDER HARNESS ON IN-SERVICEAIRCRAFT, IF SO EQUIPPED.

NOTENOTENOTENOTE:::: COLOR IS NEUTRAL. RECOMMENDED FOR UMBER WEBBING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-5068-9CABIN SEAT SHOULDERHARNESS STOP/RED ATA : 25200/B200 BB-75 & AFTER200C/B200C BL-1 & AFTER200CT/B200CT BN-1 & AFTER200T/B200T BT-1 & AFTER300 FA-1 THRU FA-230A100 B-229 THRU B-247B100 BE-13 THRU BE-137B300 FL-1 & AFTERB300C FM-1 & AFTERB300C(CS) FN-1C90/C90A LJ-693 & AFTERE90 LW-193 THRU LW-347F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO INSTALL A STOP AND INSTRUCTIONPLACARD RETAINER ON THE CABIN CHAIR RETRACTABLE SHOULDER HARNESS ON IN-SERVICEAIRCRAFT, IF SO EQUIPPED.

NOTENOTENOTENOTE:::: COLOR IS RED. RECOMMENDED FOR BURGUNDY OR DRAGON RED WEBBING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-5108-0001SWIVELING CHAIR PEDESTAL REPLACEMENT ATA : 25B300 FL-1 THRU FL-289, FL-292, FL-295 & FL-297"M"SB #25-3640THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE LEFT HAND FORWARD FACING/RIGHTHAND AFT FACING TOSINGTON/DERLAN/ERDA SWIVELING CABIN CHAIR PEDESTAL AND INSTALL AN ASCCHAIR PEDESTAL FOR IN-SERVICE AIRCRAFT.

WT. CHANGE : +2.4 LBS. MOMENT: LBS-INEST. MAN/HRS: : 2.5 HRSMEN : 1 (MAN)

130-5108-0002SWIVELING CHAIR PEDESTAL REPLACEMENT ATA : 25B300 FL-1 THRU FL-289, FL-292, FL-295 & FL-297"M"SB #25-3640THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE RIGHT HAND FORWARD FACING/LEFTHAND AFT FACING TOSINGTON/DERLAN/ERDA SWIVELING CABIN CHAIR PEDESTAL AND INSTALL AN ASCCHAIR PEDESTAL FOR IN-SERVICE AIRCRAFT.WT. CHANGE : 2.4 LBS MOMENT: LBS-INEST. MAN/HRS: : 2.5 HRS.MEN : 1 (MAN)

130-5300-1B300 CRASH AXE KIT ATA : 25200GT BY-1 AND AFTERB200 BB-1 AND AFTERB200C BL-1 AND AFTERB200CGT BZ-1 AND AFTERB300 FL-1 AND AFTERB300C FM-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR ADDING A CRASH AXE WITH COVER TO THE B300COCKPIT ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA9394NA" ADHESIVE & "242" LOCTITE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED PILOT'S OERATING HANDBOOK(OR SUPPLEMENT) HAS BEEN INCORPORATED. PROCURE SEPERATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

WT. CHANGE : 2.86 LB MOMENT: 426.14 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-5507-0001KIT - DUCTING, OVERHEAD ATA :B300C FM-14 THRU FM-17, FM-19, AND FM-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DUCTING DETAILS INSIDE OVERHEAD DUCTSTO BALANCE AIR FLOW OUT OF DUCT OUTLETS FOR IN SERVICE.

NOTENOTENOTENOTE:::: 5776-A/B URALANE ADHESIVE (A/R)RTV732 SEALER (A/R) BUT NOT FURNISHED IN KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 40MEN : 2 (MEN)


KIT CATALOG

130-5701-0001FIRE EXTINGUISHER INSTALLATION KIT ATA : 26B300 (350) FL-1 AND AFTERTHIS KIT CONTAINS PARTS AND INFORMATION REQUIRED TO INSTALL A352TS FIRE EXTINGUISHERMOUNTED ON THE LEFT HAND SEAT TRACKS IMMEDIATELY FWD OF THE AFT LH CABIN PARTITIONASSEMBLY ON IN-SERVICE AIRCRAFT.WT. CHANGE : +5.5 LBS. MOMENT: +1680 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-8001-0001PISTON, MAIN LANDING GEAR ATA : 32B200 BB-1764, BB-1787, BB-1789 & BB-1790 WITH

HIGH FLOTATION GEARSB200C BL-143, BL-144 & BL-145 WITH HIGH

FLOTATION GEARSB300 FL-307 THRU FL-328, FL-330 & FL-332 THRU

FL-342 WITH HIGH FLOTATION GEARS"RECOMMENDED" SB NO. 32-3662THIS KIT PROVIDES PARTS TO REPLACE A PISTON FOR THE MLG, IN ACCORDANCE WITH THE 6YEAR/8000 CYCLE LANDING GEAR INSPECTION FOR ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE -0001 PISTON MUST BE SHRINK FIT INTO AN EXISTING AXLE SOCKET. THIS MUST BEACCOMPLISHED BY A CERTIFIED LANDING GEAR OVERHAUL FACILITY. NO INSTALLATIONINSTRUCTION ARE PROVIDED ON THIS KIT.

NOTENOTENOTENOTE:::: B300/B300C WT: +1.2 LBS. MOMENT: +272 IN-LBS.300/B200/B200T/B200C/B200CT WT: +1.2 LBS. MOMENT: +253 IN-LBS.

WT. CHANGE : B300/B300C WT: +1.2 LBS. MOMENT: +272 IN-LBS.EST MAN/HEST. MAN/HRS: : 1MEN : 1 (MAN)

130-8001-0003PISTON, MAIN LANDING GEAR ATA : 32B200 BB-1764, BB-1787, BB-1789 & BB-1790 WITH

HIGH FLOTATION GEARSB200C BL-143, BL-144 & BL-145 WITH HIGH

FLOTATION GEARSB300 FL-307 THRU FL-328, FL-330 & FL-332 THRU

FL-342 WITH HIGH FLOTATION GEARS"RECOMMENDED" SB NO. 32-3662, 1/29/04

THIS KIT PROVIDES PARTS & INFORMATION TO REPLACE AN AXLE & PISTON ASSY FOR THE MLG, INACCORDANCE WITH THE 6 YEAR/8000 CYCLE LANDING GEAR INSPECTION FOR ALL IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: B300/B300C WT: +1.2 LBS. MOMENT: +272 IN-LBS.

300/B200/B200T/B200C/B200CT WT: +1.2 LBS. MOMENT: +253 IN-LBS.

NOTENOTENOTENOTE:::: 2 KITS PER A/CWT. CHANGE : B300/B300C WT: +1.2 LBS. MOMENT: +272 IN-LBS.300/B200/B200T/B200C/B200CT WT: +1.2 LBS. MOMENT:

+253 IN-LBS.EST. MAN/HRS: : 0.5 HR.MEN : 1 (MAN)


KIT CATALOG

130-8002-0001HIGH FLOTATION LANDING GEAR ATA :B300 (WITH BRAKE DE-ICE) FL-1 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HIGH FLOTATION LANDING GEAR SYSTEMFOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT MUST BE USED IN CONJUNCTION WITH STC SA4175NM.NOTENOTENOTENOTE:::: "MIL-G-81322" GREASE,AIRCRAFT GENERAL PURPOSE, "EC-3911" DEGREASE

COMPOUND, & "EC-2216-B/A" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +90.0 LBS. MOMENT: +20,196 LB-IN.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-8002-0003HIGH FLOTATION LANDING GEAR ATA :B300 (WITHOUT BRAKE DE-ICE) FL-1 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HIGH FLOTATION LANDING GEAR SYSTEMFOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT MUST BE USED IN CONJUNCTION WITH STC SA4175NM.NOTENOTENOTENOTE:::: "MIL-G-81322" GREASE,AIRCRAFT GENERAL PURPOSE, "EC-3911" DEGREASE

COMPOUND, & "EC-2216-B/A" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +90.0 LBS. MOMENT: +20,196 LB-IN.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-9001-1EXHAUST STACK FAIRING ATA : 78300 FA-225 THRU FA-230B300(350) FL-89 THRU FL-126B300C FM-8 & AFTERB300C(CS) FN-1 & AFTERWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-9003-1WASH RING INSTL ENGINE KIT ATA : 71B300 FL-1 THROUGH FL-492 AND FL-494

THROUGH FL-499THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO ADD AN ENGINE WASH RING FOR IN-SERVICE AIRCRAFT WITHOUT STC SA10470SC INSTALLED. (KEITH AIR CONDITION)WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

130-9003-5WASH RING INSTAL ENGINE - KIT ATA :B300 FL-493 AND FL-500 AND AFTER. FM-14 AND

AFTER.THIS KIT PROVIDES INFORMATION AND PARTS REQUIRED TO ADD AN ENGINE WASH RING FOR MODELB300 AIRCRAFT IN SERVICE WITH STC SA10470SC INSTALLED. (KEITH AIR CONDITION).

NOTENOTENOTENOTE:::: THIS IS A FULL KIT WITH THE WASH RING INCLUDED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

130-9005-1FUEL CELL COVER &GASKET INSTL ATA : 28C90A LJ-1 THRU LJ-1598E90 LW-1 THRU LW-347F90 LA-2 THRU LA-236H90(T-44A) LL-1 THRU LL-61"RECOMMENDED" SB NO. 28-3401THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL COVER AND GASKETINSTALLATIONS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309NA" SEALANT REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

130-9005-3FUEL CELL COVER &GASKET INSTL ATA : 28200C/B200C BL-1 THRU BL-140200CT/B200CT BN-1 THRU BN-4200T/B200T BT-1 THRU BT-39A200C(C-12C) BC-1 THRU BC-75, BD-1 THRU BD-30A200C(UC-12B) BJ-1 THRU BJ-66A200CT(C-12D) BP-1, BP-22, BP-24 THRU BP-51A200CT(C-12F) BP-52 THRU BP-63A200CT(RC-12D) GR-1 THRU GR-13A200CT(RC-12G) FC-1 THRU FC-3A200CT(RC-12H) GR-14 THRU GR-19A200CT(RC-12K) FE-1 THRU FE-9A200CT(RC-12N) FE-10 THRU FE-24A200CT(RC-12P) FE-25 THRU FE-31, FE-33, FE-35A200CT(RC-12Q) FE-32, FE-34, FE-36B200 BB-1 THRU BB-1718B200C(C-12F) BL-73 THRU BL-112, BL-118 THRU BL-123,

BP-64 THRU BP-71B200C(C-12R) BW-1 THRU BW-29B200C(RC-12F) BU-11, BU-12B200C(RC-12M) BV-11, BV-12B200C(UC-12F) BU-1 THRU BU-10B200C(UC-12M) BV-1 THRU BV-10B200CT(FWC-II) FG-1, FG-2"RECOMMENDED" SB NO. 28-3401THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL COVER AND GASKETINSTALLATIONS FOR IN-SERVICE AIRCRAFT.


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 HRS. PER COVERMEN : 1 (MAN)

130-9005-5FUEL CELL COVER &GASKET INSTL ATA : 28300 FA-1 THRU FA-230, FF-1 THRU FF-19B300 FL-1 THRU FL-265, FL-267 THRU FL-283B300C FM-1 THRU FM-10B300C(CS) FN-1"RECOMMENDED" SB NO. 28-3401 TO BE RELEASED WHEN PARTS ARE AVAILABLETHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE FUEL COVER AND GASKETINSTALLATIONS FOR IN-SERVICE AIRCRAFT.


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 HRS. PER COVERMEN : 1 (MAN)


KIT CATALOG

130-9600-1GROUND IDLE SOLENOID SYSTEM ATA : 61 300 FA-2 THRU FA-230"OPTIONAL" SB NO. 61-3125WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

130-9700-1FILTER,PNEUMATIC AIR,WIDOW DEFROST ATA : 30300 FA-1 THRU FA-230B300 FL-1 THRU FL-318B300C FM-1 THRU FM-10 & FN-1"OPTIONAL" SB NO. 30-3471THE PURPOSE OF THIS KIT IS TO INSTALL AIR FILTRATION IN THE PNEUMATIC SIDE WINDOW DEFOGSYSTEM ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5MEN : 5 (MEN)

130-9701-0001KIT TUBING, DEICE ATA :B300 SERIALS FL-427, FL-493, FL-500 THROUGH

FL-573B300C SERIALS FM-14 THROUGH FM-18THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE SECTION OF THE TAIL DEICE CONTROLTUBING THAT PASSES THROUGH THE AFT EVAPORATOR SECTION ON IN SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLE - MOMENT NEG - IN ADDITION, COMPLIANCE WITH 14 CFR 23.25 AND PART 3.74 MUST BE

MAINTAINED (WEIGHT LIMIT VS AIRCRAFT LOADING)EST. MAN/HRS: : 5MEN : 1 (MAN)

130-9701-0003KIT TUBING, DEICE ATA :B200 SERIALS BB-1926, BB-1978, BB-1988

THROUGH BB-2000B200GT SERIALS BY-1 THROUGH BY-26THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE SECTION OF THE TAIL DEICE CONTROLTUBING THAT PASSES THROUGH THE AFT EVAPORATOR SECTION ON IN SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLE - MOMENT NEG - IN ADDITION, COMPLIANCE WITH 14 CFR 23.25 AND PART 3.74 MUST BE

MAINTAINED (WEIGHT LIMIT VS AIRCRAFT LOADING)EST. MAN/HRS: : 5MEN : 1 (MAN)


KIT CATALOG

130-9702-0001AIR CONDITIONER COMPRESSOR KIT ATA :KING AIRTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED COMPRESSOR MOUNT ASSEMBLYAND ATTACHING HARDWARE ON THE RIGHT ENGINE.

NOTENOTENOTENOTE:::: IN-SERVICE AIRCRAFT KING AIRMODEL B200 SUPER KING AIR, SERIALS BB-1978, BB-1988 THROUGH BB-2007MODEL B200C, SUPER KING AIR, SERIAL BL-153MODEL B200GT, SUPER KING AIR SERIALS BY-1 THROUGH BY-80MODEL B300, SUPER KING AIR, SERIALS FL-493, FL-500 THROUGH FL-627MODEL B300C, SUPER KING AIR 350C, SERIALS FM-14 THROUGH FM-27


35-8010-5 SMAIN LANDING GEAR WHEEL BEARING REPLACEMENT ATA :A100, 200, 200C, A200, A200CT, A200C(UC-12B), B200, B200C, B200T, B200CT,C200C (C-12F), B200C (RC-12F), B200C(RC-12M)THIS KIT IS A SPARES REPLACEMENT FOR 13685XL CONE AND 13621XL CUP, P/N OF TYSON BEARING CO.ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REPLACES BEARINGS IN 101-8002-5 WHEEL.NOTENOTENOTENOTE:::: THIS KIT IS NOT FOR USAGE ON MODEL 100, A100, OR B100 AIRCRAFT. THE MODEL 100

SERIES AIRCRAFT WITH HIGH FLOTATION WHEELS USE 13889 AND 13830; STANDARDGEAR AIRCRAFT WITH GOODRICH COMPONENTS SHOWN IN COMPONENT MAINTENANCEMANUAL USE 13600/4/13685L OR 13600LA13685 CONE AND SEAL ASSEMBLY AND13621CUP.

NOTENOTENOTENOTE:::: SEE "ABS" WHEEL BULLETIN NO. BEECH 200 32-1 BEFORE ORDERING THIS KIT AIRCRAFTMFG AF 1988.

NOTENOTENOTENOTE:::: THIS KIT IS ONLY FOR AIRCRAFT WITH HIGH FLOTATION MAIN LANDING GEARASSEMBLIES. THIS KIT PROVIDES 2 BEARINGS AND SEALS AND 2 CUPS FORREPLACEMENT ON ONE MAIN WHEEL ASSEMBLY ONLY.


36-5017-1 SFIRE EXTINGUISHER REPLACEMENT ATA :1900C UC-1 THRU UC-75 SEE KIT 114-5310-1, AND

ORDER ACCORDINGLY.65-90, 65-A90, B90, C90, C90A, E90, F90,100, A100, B100, 200, 200C, 200CT, B200,B200C, B200T, B200CT, 300REPLACEMENT KITS LISTED ONLY FOR REFERENCE MODELS.THIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL A FIRE EXTINGUISHER REPLACEMENT FORAIRCRAFT EQUIPPED WITH 890017 OR 890275 FIRE EXTINGUISHER, P/N OF WALTER KIDDE OR FR-2 1/2FIRE EXTINGUISHER P/N OF GENERAL FIRE EXT. CORP. OR MODEL 2-10 FIRE EXT. PWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 3 (MEN)


KIT CATALOG

36-5017-3 SFIRE EXTINGUISHER REPLACEMENT SPARES FOR FR-2 3/4 FIREEXTINGUISHER

ATA :

A200C (H90) (T44A) LL-1 THRU LL-61THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A 352TS FIRE EXTINGUISHERTHAT WAS PREVIOUSLY EQUIPPED WITH FR-2 3/4 FIRE EXTINGUISHER ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : N/A

50-9005-0001FUEL VENT DEFLECTOR INSTL ATA : 28"OPTIONAL" SB 28-3611 - MODEL C90B PRIOR TO ECR 13926; MODEL H90 S/N: LL-17 THRU LL-61THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW FUEL VENT DEFLECTOR TO THE LHAND RH FUEL FILLER ADAPTER ON IN-SERVICE AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

55-3028-3 PCLOCK INSTALLATION, CONTROL WHEEL, (28 -VOLT) ATA :65A-90, B90, C90, 90 100, A100, B100THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-3, 50-534622-13, 50-534622-17,50-534622-21, 50-384209-1, 50-384210-1 OR 50-384211-1, 8-DAY CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-2003-1 SEXTERIOR PLACARD ATA :KING AIRTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS ON ALL INSERVICE AIRCRAFT (INCLUDING E AND F90 SERIES)AIRCRAFT.

NOTENOTENOTENOTE:::: RESTRICTED ARTICLE (SPRAY CAN) OF PROTECTIVE PAINT WAS REMOVED FROM KIT TOREDUCE COST OF KIT AND UNNECESSARY EXPENSE IN SPECIAL SHIPMENT OF SPRAYCAN OF PAINT WHICH IS READILY AVAILABLE LOCALLY.


90-2004-1 SINTERIOR PLACARD ATA :90 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

90-3085-1 SBRUSH BLOCK ASSEMBLY, MODULAR ATA :B100 BE-1 THRU BE-62SI NO. 1075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR 4E1387-3, -5AND -6 BRUSH BLOCK ASSEMBLIES WHERE APPLICABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : N/A

90-3085-3 SBRUSH BLOCK ASSEMBLY, MODULAR ATA :100, A100 B-1 THRU B-247200 BB-2 THRU BB-424200T BT-1 THRU BT-390, A90, B90, C90 LJ-1 THRU LJ-807E90 LW-1 THRU LW-305SI NO. 1075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR 4E1311-1 OR -2BRUSH BLOCK ASSEMBLIES WHERE APPLICABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5MEN : N/A

90-3089-1 SFLAP TRAVEL SWITCH COVER ATA :A100 B-233 THRU B-247B100 BE-20 THRU BE-81C90 LJ-707 THRU LJ-878E90 LW-207 THRU LW-328F90 LA-2 THRU LA-37SI NO. 1121 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEALED SWITCHES, FLAP SWITCHCOVER AND ELECTRICAL CONNECTORS FOR THE FLAP TRAVEL SWITCHES.


90-3089-3 SFLAP TRAVEL SWITCH COVER ATA :H90 LL-1 THRU LL-61THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW SEALED SWITCHES, FLAP SWITCHCOVER AND ELECTRICAL CONNECTORS FOR THE FLAP TRAVEL SWITCHES ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

90-3096-1 SAIR CONDITIONER RELAY CONTROL - SPARES ATA :100, A100 B-1 THRU B-24790, A90, B90, C90, C90A LJ-1 THRU LJ-1125B100 BE-1 THRU BE-137E90 LW-1 THRU LW-347E90 LW-1 THRU LW-347F90 LA-2 THRU LA-236SB NO. 2085 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 100-364378-5 RELAY CONTROL BOXASSEMBLY AS A SPARES REPLACEMENT FOR THE 100-364179-1 PC BOARD AND THE 100-364178-1 RELAYCONTROL BOX.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

90-3097-1 SBATTERY AMP INDICATOR, DC VOLT ATA :F90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DC VOLT BATTERY AMP INDICATOR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

90-3100-1 PWINDSHIELD, LH HEATED ATA :100 B-2 THRU B-89 AND B-93 (WITH KIT

90-3100-3 P INSTALLED)90, A90, B90, C90 LJ-1 THRU LJ-639 (WITH KIT 90-3100-3 P

INSTALLED)A100 B-1, B-90 THRU B-92, B-94 THRU B-247B100 BE-1 THRU BE-137C90 LJ-640 THRU LJ-1062E90 LW-1 THRU LW-347SB NO. 2108, REV. 1 OR SUBSEQUENT101-5041-3 S KIT IS REQUIRED FOR INSTALLATION.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH HEATED WINDSHIELD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A


KIT CATALOG

90-3100-2 PWINDSHIELD, RH HEATED ATA :100 B-2 THRU B-89, B-93 (WITH KIT 90-3100-3 P

INSTALLED)90, A90, B90, C90 LJ-1 THRU LJ-639 (WITH KIT 90-3100-3 P

INSTALLED)A100 B-1, B-90 THRU B-92, B-94 THRU B-247B100 BE-1 THRU BE-137C90 LJ-640 THRU LJ-1062E90 LW-1 THRU LW-347SB NO. 2108, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RH HEATED WINDSHIELD.

NOTENOTENOTENOTE:::: 101-5041-3 S KIT IS REQUIRED FOR INSTALLATION OF ONE KIT, BUT IF INSTALLING BOTH-1 P AND -2 P KIT AT SAME TIME, YOU ONLY WILL REQUIRE 1 EACH 101-5041-1 S TOINSTALL BOTH WINDSHIELDS.


90-3100-3 PWINDSHIELD DEICE ELECTRONICS INSTALLATION ATA :100 B-2 THRU B-89, B-9390, A90, B90, C90 LJ-1 THRU LJ-639"OPTIONAL" SB NO. 2207, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION FOR A SPARE REPLACEMENT OF (1 EACH) 50-389055-2PRESSURE SWITCH LOCATED IN MAIN GEAR WHEELS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4 HRS.MEN : N/A

90-3101-1 SBEACON, VERTICAL STABILIZER, FLASHING ATA :90, A90, B90, C90, C90A LJ-1 THRU LJ-1137E90 LW-1 THRU LW-347"OPTIONAL" SB NO. 2149THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AND THEGLARESHIELDS AS A REPLACEMENT FOR THE GRIMES ROTATING BEACON.

NOTENOTENOTENOTE:::: THIS KIT CONTAINS TIP ASSEMBLY, SOCKET HOUSING, SOCKET CONTACTS AND OTHERHARDWARE REQUIRED FOR INSTALLATION AS WELL AS KIT DRAWING. OVERALL HEIGHTOF TIP ASSEMBLY IS 7 1/2 INCHES, HEIGHT OF DOME ABOUT 5 1/4 INCHES AND 9 INCHESIN WIDTH.



KIT CATALOG

90-3102-1 SBEACON, LOWER FLASHING ATA :90, A90, B90, C90 LJ-1 THRU LJ-1062E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AND THEGLARESHIELDS AS A REPLACEMENT FOR THE GRIMES ROTATING BEACON.

NOTENOTENOTENOTE:::: NO GLARESHIELDS WERE INSTALLED OR ARE REQUIRED ON MODEL 100 AIRPLANES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3102-3 SBEACON, LOWER FLASHING ATA :100 AND A100 B-1 THRU B-247100 AND A100 B-1 THRU B-24790, A90, B90, C90 LJ-1 THRU LJ-1062B100 BE-1 THRU BE-137E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AS AREPLACEMENT FOR THE GRIMES ROTATING BEACON ON AIRPLANES PREVIOUSLY EQUIPPED WITHGLARESHIELDS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3103-1 SBEACON, LOWER FLASHING ATA :C90A LJ-1063 THRU LJ-1137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AND THEGLARESHIELDS AS A REPLACEMENT FOR THE GRIMES ROTATING BEACON.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : N/A

90-3103-3 SBEACON, LOWER FLASHING ATA :C90A LJ-1063 THRU LJ-1137THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AS AREPLACEMENT FOR THE GRIMES ROTATING BEACON ON AIRPLANES PREVIOUSLY EQUIPPED WITHGLARESHIELDS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

90-3104-1 SBEACON, LOWER FLASHING ATA :F90 LA-2 THRU LA-236THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AS AREPLACEMENT FOR THE GRIMES ROTATING BEACON.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : N/A

90-3105-1 SBEACON, UPPER FLASHING ATA :F90 LA-2 THRU LA-236THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WHELEN FLASHING BEACON AS AREPLACEMENT FOR THE GRIMES ROTATING BEACON.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

90-3106-1 SOIL PRESSURE TRANSDUCER INSTALLATION ATA :C90, C90A, E90, F90, A100, B100, 200, B200,200C, B200C, 200CT, B200CT, 200T, B200T,A200, A200C, A200CT, 300"OPTIONAL" SB NO. 2159, REV. 2 FOR AIRCRAFT SERIAL NUMBERS: EFFECTED. ALSO C, SB NO. 1072THIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACEMENT OF ENGINE OIL PRESSURETRANSDUCERS WITH REPLACEMENT TRANSDUCERS WITH GOLD PINS WHICH ALLEVIATE THEPOSSIBILITY OF ANY CORROSION AND ACCOMPANYING FLUCTUATIONS DUE TO ELECTRICAL SIGNALINTERRUPTION ON

NOTENOTENOTENOTE:::: SERVICE BULLETIN NO. 1072 NEEDS TO BE COMPLIED WITH BEFORE 90-3106-1 S KITINSTALLED AS THIS KIT DOES NOT CONTAIN INDICATOR, CLIP OR ETC. 90-3106-1 SFURNISHES IMPROVED TRANSDUCERS AND NECESSARY HARDWARE FOR INSTALLATIONOF SAME. CHECK SERVICE BULLETIN NO. 1072 TO SEE IF IT EFFECTS YOUR AIRCRAFTSERIAL NUMBER AND ORDER ACCORDINGLY.

WT. CHANGE : NEGLIGIBLE (1 KIT PER AIRCRAFT)EST. MAN/HRS: : 1MEN : N/A

90-3107-1 PICE VANE ACTUATOR ATA :C90, F90THIS KIT IS THE SPARES REPLACEMENT FOR 114-389039-5 ACTUATOR ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

90-3108-1 SHYDRAULIC LANDING GEAR MOTOR RELAY ATA :C90A LJ-1063 THRU LJ-1204F90 LA-226 THRU LA-236SB NO. 2226, REV. 2 OR SUBSEQUENTTHIS KIT CONTAINS PARTS AND INFORMATION TO REPLACE THE HYDRAULIC LANDING GEAR POWERRELAY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

90-3109-1 STIME DELAY RELAY INSTALL ATA : 21WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-3110-1 SLIMITER ATA :C90A LJ-1063 THRU LJ-1265THIS KIT PROVIDES PARTS AND INFORMATION REGARDING THE INSTALLATION OF A FUSE HOLDER ANDLIMITER ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A

90-3111-1 SINDICATOR LANDING GEAR POSITION LIGHT ATA :C90A LJ-1063 THRU LJ-1305, LJ-1309 THRU

LJ-1313, LJ-1317, LJ-1319THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE LANDING GEAR POSITIONINDICATOR LIGHT ASSEMBLY P/N 308-607-0843-004 (P/N OR KORRY) WITH A (EATON) INDICATOR LIGHTASSEMBLY P/N 351-33790-007.

NOTENOTENOTENOTE:::: FOR MODELS 300, B300 (350) AND B300C (FA, FF, FL AND FM SERIES) SEE KIT 101-3176-1S.

NOTENOTENOTENOTE:::: FOR MODELS B200, B200T, B200C AND B200CT SEE KIT 101-3175-1 S.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : N/A


KIT CATALOG

90-3112-1 SRADIO ALTIMETER ANTENNA RELOCATION ATA :C90A LJ1-147, LJ-1161, LJ-1162, LJ-1163, LJ-1177,

LJ-1178, LJ-1179, LJ-1183, LJ-1184, LJ-1196,LJ-1197, LJ-1198, LJ-1199, LJ-1305, LJ-1311,LJ-1312, LJ-1349, LJ-1350, LJ-1351, LJ-1352

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE FORWARD RADIO ALTIMETERANTENNA ON INSERVICE AIRCRAFT WITH THE DUAL RADIO ALTIMETER SYSTEMS INSTALLED.

NOTENOTENOTENOTE:::: ALODINE 1200 CLEANER AND 890B1/2 QT OR 890B1/2 6 OZ TU OR THE EQUIVALENT OFTHE CLEANER AND SEALER ARE REQUIRED FOR INSTALLATION OF THIS KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


90-3118-1PITOT HEAT INDICATOR ATA : 30WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-3119-0001REMOTE MOUNTED OIL PRESSURE TRANSDUCER ATA :A100 B-151 THRU B-247 (DIRECT MOUNT, S/N:

B-151 THRU B-240)E90 LW-39 THRU LW-347 (DIRECT MOUNT, S/N:

LW-39 THRU LW-263 AND LW-325 THRULW-332)

THIS KIT PROVIDES INFORMATION AND PARTS TO INSTALL AN IMPROVED OIL PRESSURE TRANSDUCERAND ELECTRICAL CONNECTOR ON THE RIGHT AND LEFT ENGINE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EXISTING OFF-MOUNTED TRANSDUCERS WILL BE PROVIDED A NEW HOSE ASSY ANDMOUNTING HARDWARE WHEN INSTALLING THE NEW TRANSDUCER.

NOTENOTENOTENOTE:::: 101-389023-7 REPLACES 101-389003-1 OR 101-389023-3 OR 101-389023-5 OIL PRESSURETRANSDUCER.

NOTENOTENOTENOTE:::: DIRECT MOUNTED TRANSDUCERS (TRANSDUCERS INSTALLED ON THE ENGINE) WILLNOW BE OFF-MOUNTED AS SHOWN IN THIS KIT.


90-3402-1ELT INSTL, DUAL MODE INFO ONLY ATA : 25C90A LJ-1404 AND AFTER, LJ-1305 THRU LJ-1403

PROVIDED KIT 101-3210-1, ELT REMOTESWITCH, IS INSTALLED.

THIS KIT PROVIDES INFORMATION ONLY FOR INSTALLATION OF THE ARTEX ELT C406-2 AND DUAL MODEROD ANTENNA (110-320) FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-3402-3ELT INSTL, DUAL MODE INFO ONLY ATA : 25C90A LJ-1305 THRU LJ-1403THIS KIT PROVIDES INFORMATION FOR INSTALLATION OF THE ARTEX ELT C406-2 AND DUAL MODE RODANTENNA (110-320) FOR IN-SERVICE AIRCRAFT. PROVIDED KIT 101-3210-1, ELT REMOTE SWITCH ISINSTALLED, USE 90-3402-1.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-3600-1KIT EMERGENCY LIGHTING INSTALLATION - JAR-OPS ATA : 33C90A LJ-1063 AND AFTERTHIS KIT CONTAINS PARTS AND INFORMATION NECESSARY TO INSTALL EMERGENCY LIGHTING PER JAR-OPS REQUIREMENTS.

NOTENOTENOTENOTE:::: "NASM20426AD3" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUALREVISION (OR SUPPLEMENT) HAS BEEN INCORPORATED.MAY BE OBTAINED FROM ANY COMPANY AUTHORIZED OUTLET.


90-4023- MDAMPENER AIR STADOOR (KIT) ATA : 52WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-4061- SELEVATOR, ALUMINUM ATA : 2790, A90 LJ-1 THRU LJ-317SI NO. 0333-131, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH AND RH ELEVATORS WITHALUMINUM ELEVATORS AND REWORK THE HORIZONTAL STABILIZER FOR IMPROVED PERFORMANCEAND SERVICE LIFE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : N/A

90-4062- SLH ALUMINUM ELEVATKIT ATA : 27SI NO. 0333-131, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LH ELEVATOR WITH AND ALUMINUMELEVATOR AND REWORK THE HORIZONTAL STABILIZER FOR IMPROVED PERFORMANCE AND SERVICELIFE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

90-4062-1 SELEVATOR, ALUMINUM ATA : 27B90 LJ-318 THRU LJ-501SI NO. 0333-131, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RH ELEVATOR WITH AN ALUMINUMELEVATOR AND REWORK THE HORIZONTAL STABILIZER FOR IMPROVED PERFORMANCE AND SERVICELIFE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

90-4063- SCENTER SECTION SPAPROVISION (COMM ATA : 27SI NO. 0394-018 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO PROVIDE VARIOUS ACCESS DOORS FORINSPECTING THE MAIN SPAR ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 36MEN : N/A

90-4063-1 SMAIN SPAR INSPECTION PROVISIONS, CENTER SECTION ATA :100, A100 B-1 THRU B-110SI NO. 0388-018, REV. 6 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE VARIOUS ACCESS DOORS FOR THEINSPECTION OF THE MAIN SPAR AND TO REPLACE VARIOUS HUCK BOLTS AND JO BOLTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 36MEN : N/A

90-4065- PWINDOW, POLARIZED, 6 WINDOWS ATA :90, A90, B90, C90 LJ-1 THRU LJ-568THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ADJUSTABLE POLARIZED WINDOWS FORPASSENGER COMFORT AND CONVENIENCE. DEGREE OF SHADE IS INDIVIDUALLY CONTROLLED.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 1 FOR ADDITIONAL INFORMATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 60MEN : 1 (MAN)

90-4065-1 PWINDOW, POLARIZED, 7 WINDOWS ATA :90, A90, B90, C90 LJ-1 THRU LJ-568THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ADJUSTABLE POLARIZED WINDOWS FORPASSENGER COMFORT AND CONVENIENCE. DEGREE OF SHADE IS INDIVIDUALLY CONTROLLED.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 1 FOR ADDITIONAL INFORMATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

90-4069-1DOOR SEAL PRESSURIZATION SOURCE ATA :100, A100 B-1 THRU B-168C90 LJ-502 THRU LJ-586E90 LW-1 THRU LW-54SI NO. 0580-452, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO MAKE PROVISIONS FOR PRESSURIZING THE CABINDOOR SEAL FROM EITHER ENGINE BLEED AIR SOURCE, TO REDUCE THE POSSIBILITY OF DEFLATION OFTHE DOOR SEAL WHEN ONE ENGINE IS SHUT DOWN, AND INCREASE THE CABIN DOOR SEAL PREWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : N/A

90-4069-1 SDOOR SEAL PRESS SO(COMM KIT) ATA : 52WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-4069-3 SDOOR SEAL PRESSURIZATION SOURCE ATA :A100 B-169 THRU B-240A100 B-169 THRU B-240B100 BE-1 THRU BE-38C90 LJ-587 THRU LJ-764E90 LW-55 THRU LW-271SI NO. 0580-452, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE INCREASED PRESSURE FOR THE CABINDOOR SEAL TO PROVIDE A BETTER SEAL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

90-4076-1 SBAGGAGE DOOR SECONDARY LATCH, NOSE ATA :C90 LJ-569 THRU LJ-832, LJ-834 THRU LJ-975,

LJ-977 THRU LJ-979, LJ-981 THRU LJ-985E90 LW-49, LW-51, LW-64, LW-98, LW-104,

LW-122, LW-140, LW-313THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SECONDARY LATCH ON HINGED NOSEBAGGAGE DOORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-4077-1 SWING TSPAR, CENTER SECTION AND OUTBOARD WING ATA :90, A90, B90, C90, C90A LJ-1 THRU LJ-1084, LJ-1086 AND LJ-1087E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INTEGRAL FITTING, LOWER MAIN CENTERSECTION SPAR CAP AND OUTBOARD WING MAIN SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1600MEN : N/A

90-4080-1 SPRESSURIZATION VALVE - SPARES ATA :90 LJ-1 THRU LJ-75, LJ-77 THRU LJ-113 THAT

HAVE BEEN MODIFIED TO 3.8PRESSURIZATION BY KIT 90-4005 S

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SPARES REPLACEMENT PRESSURIZATIONOUTFLOW AND SAFETY VALVES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4080-3PRESSURIZATION VALVE - SPARES ATA :90 LJ-1 THRU LJ-75, LJ-77 THRU LJ-113

EQUIPPED WITH 3.1 PRESSURIZATIONTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SPARES REPLACEMENT PRESSURIZATIONOUTFLOW AND SAFETY VALVES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4081-1 SS SCD NS DR LB ATA : 54WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-4082-1 SELEVATOR - SPARES ATA : 2790, A90, B90, C90 LJ-1 THRU LJ-827E90 LW-1 THRU LW-322SI NO. 0333-131, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 50-610000-349 OR -487 LH ELEVATOR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A


KIT CATALOG

90-4082-2 SELEVATOR - SPARES ATA : 2790, A90, B90, C90 LJ-1 THRU LJ-827E90 LW-1 THRU LW-322SI NO. 0333-131, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 50-610000-350 OR -488 RH ELEVATOR.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : N/A

90-4083-1 SELEVATOR HINGE ATA : 2790, A90, B90, C90 LJ-1 THRU LJ-827E90 LW-1 THRU LW-322SI NO. 0333-131, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED ELEVATOR HINGES ON AIRPLANESWHICH HAVE 50-610000-349, -350, OR 50-610000-487, -488 ELEVATORS INSTALLED. THIS KIT PROVIDESPARTS FOR BOTH LEFT AND RIGHT ELEVATORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

90-4084-1 SELEVATOR, MAGNESIUM ATA : 2790 LJ-1 THRU LJ-6, LJ-302 THRU LJ-317SI NO. 0333-131 REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL MAGNESIUM ELEVATORS WITH IMPROVEDHINGES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : N/A

90-4085-1 SRUDDER PEDAL ARM ASSEMBLY - SPARES ATA :100, A100 B-1 THRU B-225200 BB-2 THRU BB-11390, A90, B90, C90 LJ-1 THRU LJ-676B100 BE-1, BE-2E90 LW-1 THRU LW-164THIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 50-524326-1 OR -11 LH RUDDER PEDAL ARMASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-4085-2 SRUDDER PEDAL ARM ASSEMBLY - SPARES ATA :100 BE-1, BE-2100, A100 B-1 THRU B-225200 BB-2 THRU BB-11390, A90, B90, C90 LJ-1 THRU LJ-676E90 LW-1 THRU LW-164THIS KIT PROVIDES A SPARES REPLACEMENT FOR P/N 50-524326-2 OR -12 RH RUDDER PEDAL ARMASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4088-1 SEMERGENCY EXIT DOOR, PRESSURIZED SEAL ATA :C90 LJ-502 THRU LJ-980F90 LA-2 THRU LA-156THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PRESSURIZED SEAL ON THE EMERGENCYEXIT DOOR.

NOTENOTENOTENOTE:::: LJ-502 THRU LJ-764 AND LW-1 THRU LW-271 MUST HAVE COMPLIED WITH SERVICEINSTRUCTION NO. 0580-452 REV. 1 OR SUBSEQUENT, PRIOR TO INSTALLING THIS KIT.


90-4095-1 MWINDOW, AFT CLEAR TEARDROP ATA :100, A100 B-1 THRU B-247100, A100 B-1 THRU B-24790, A90, B90, C90, C90A LJ-1 AND AFTERB100 BE-1 THRU BE-137E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LH AND RH AFT CLEAR TEARDROP WINDOWS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4096-1 SKEEL REINFORCEMENT ATA :100, A100 B-1 THRU B-247100, A100 B-1 THRU B-24790, A90, B90, C90, C90A LJ-1 THRU LJ-1084, LJ-1086 AND LJ-1087B100 BE-1 THRU BE-137E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE AND REPLACE A PORTION OF THE LH MAINLANDING GEAR WHEEL WELL OUTBOARD KEEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-4096-2 SKEEL REINFORCEMENT ATA :100 AND 100A B-1 THRU B-247100 AND 100A B-1 THRU B-24790, A90, B90, C90, C90A LJ-1 THRU LJ-1084, LJ-1086 AND LJ-1087B100 BE-1 THRU BE-137E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE AND REPLACE A PORTION OF THE RH MAINLANDING GEAR WHEEL WELL OUTBOARD KEEL.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4098-1 SELEVATOR PULLEY BRACKET SUPPORT ATA :100, A100 B-1 THRU B-247200 BB-2 THRU BB-624200C BL-1 THRU BL-10200T BT-1 THRU BT-1390, A90, B90, C90 LJ-1 THRU LJ-889B100 BE-1 THRU BE-85E90 LW-1 THRU LW-330F90 LA-2 THRU LA-29SB NO. 2150 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REINFORCE THE ELEVATOR PULLEY BRACKETS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

90-4101-1 1SWING SPAR REINFORCEMENT ATA :C90A LJ-1085, LJ-1088 THRU LJ-1193SB NO. 2267 OR SUBSEQUENT,THIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THELEFT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-11 SWING SPAR REINFORCEMENT ATA :F90 LA-226 THRU LA-236SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THELEFT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)


KIT CATALOG

90-4101-12 SWING SPAR REINFORCEMENT ATA :F90 LA-226 THRU LA-236SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THERIGHT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-2 SWING SPAR REINFORCEMENT ATA :C90A LJ-1085, LJ-1088 THRU LJ-1193SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THERIGHT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-3 SWING SPAR REINFORCEMENT ATA :B90 LJ-327, LJ-375 THRU LJ-377, LJ-380 THRU

LJ-382, LJ-389 THRU LJ-501C90 LJ-502 THRU LJ-1062C90A LJ-1063 THRU LJ-1084, LJ-1086, LJ-1087C90A LJ-1063 THRU LJ-1084, LJ-1086, LJ-1087E90 LW-1 THRU LW-347SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THELEFT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-4 SWING SPAR REINFORCEMENT ATA :B90 LJ-327, LJ-375 THRU LJ-377, LJ-380 THRU

LJ-382, LJ-389 THRU LJ-501C90 LJ-502 THRU LJ-1062C90A LJ-1063 THRU LJ-1084, LJ-1086, LJ-1087C90A LJ-1063 THRU LJ-1084, LJ-1086, LJ-1087E90 LW-1 THRU LW-347SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THERIGHT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : N/A


KIT CATALOG

90-4101-7 SWING SPAR REINFORCEMENT ATA :100, A100, B100SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THELEFT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-8 SWING SPAR REINFORCEMENT ATA :100, A100, B100SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THERIGHT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-9 SWING SPAR REINFORCEMENT ATA :F90 LA-1 THRU LA-225SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR REINFORCEMENT OF LOWER MAIN SPAR CAP OF THELEFT AFT NACELLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4102-1 SSTABILIZER AND FIN SEALING ATA :200, B200 BB-2, BB-6 THRU BB-1302300 FA-1 THRU FA-164300 FA-1 THRU FA-164300 (FAA) FF-1 THRU FF-19F90 LA-2 THRU LA-236SB NO. 2254 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR MOISTURE PROTECTION AND INSTALLATION OFBONDING JUMPER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

90-4108-1 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 99, 99A,A99A, B99, 100, A100, B100, 200, 200C, 200T,200CT, A200CT, B200, B200C, B200T,B200CT, 300, 300C, 300T, B300, B300C, &B300C(CS)THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT UPPER WING 35-115059-4 ATTACHFITTING LH OUTBOARD FORWARD WING SPAR.

NOTENOTENOTENOTE:::: THE USE OF KIT 99-4021-1 S IS REQUIRED WHEN INSTALLING KIT -1 OR -2 AND MAY BEPURCHASED FROM ANY COMPANY AUTHORIZED OUTLET.


90-4108-2 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 99, 99A,A99A, B99, 100, A100, B100, 200, 200C, 200T,200CT, A200CT, B200, B200C, B200T,B200CT, 300, 300C, 300T, B300, B300C, &B300C(CS)THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT UPPER WING 35-115059-5 ATTACHFITTING RH OUTBOARD FORWARD WING SPAR.

NOTENOTENOTENOTE:::: THE USE OF KIT 99-4021-1 S IS REQUIRED WHEN INSTALLING KIT -1 OR -2 AND MAY BEPURCHASED FROM ANY COMPANY AUTHORIZED OUTLET.


90-4109-1 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 100, A100,B100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT WING 35-115058-2 ATTACH FITTINGLH OUTBOARD AFT WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4109-2 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 100, A100,B100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT LOWER WING 35-115058-1 ATTACHFITTING RH OUTBOARD AFT WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

90-4110-1 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, 100, A100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD WING 50-120074-2ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4110-2 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, 100, A100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD WING 50-120074-3ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4110-3 SWING ATTACH FITTING ATA :C90, E90, A100 AND B100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD LH WING 50-120074-4ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4110-4 SWING ATTACH FITTING ATA :C90, E90, A100, B100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD RH WING 50-120074-5ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4111-1 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, 100, A100,B100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER FORWARD LH WING 50-120073-7ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

90-4111-2 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, 100, A100,B100THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER FORWARD RH WING 50-120073-8ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4112-1 SWING ATTACH FITTING ATA :F90 LA-2 THRU LA-225THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD LH WING 50-120074-4ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4112-2 SWING ATTACH FITTING ATA :F90 LA-2 THRU LA-225THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD RH WING 50-120074-5ATTACH FITTING CENTER SECTION FORWARD WING SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4113-1 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 100, A100AND B100THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE UPPER AFT LH WING 50-120014 ATTACHFITTING CENTER SECTION REAR SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4113-2 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 100, A100,B100THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE UPPER AFT RH WING 50-120014-1 ATTACHFITTING CENTER SECTION REAR SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)


KIT CATALOG

90-4114-1 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 100, A100,B100THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE LOWER AFT LH WING 50-120015 ATTACHFITTING CENTER SECTION REAR SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : N/A

90-4114-2 SWING ATTACH FITTING ATA :65-90, 65-A90, B90, C90, E90, F90, 100, A100,B100THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE LOWER AFT RH WING 50-120015-1 ATTACHFITTING CENTER SECTION REAR SPAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

90-4115-1WING SPAR BRIDGE FASTENER REPLACEMENT ATA :65-90, 65-A90, B90, C90, C90A, E90, 100,A100, B100THIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO REPAIR/AND OR IMPROVE WING SPAR BRIDGESPLICE JOINT INSTALLED BY KIT DRAWINGS 90-4089 OR 100-4011. ONLY AIRCRAFT MODIFIED BY THESEKIT DRAWINGS ARE APPLICABLE TO THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4116-1 SWING TIP PODS REMOVAL AND REPLACEMENT WITH STANDARD C90AWING TIPS

ATA :

A90-1 (RU- 21H, GR V) LM-101, LM-107, LM-115, LM-125, LM-127,LM-128, LM-129, LM-132, LM-133, LM-136,LM-137, LM-138

A90-4 (RU-12H, GR V) LU-002, LU-005, LU-006, LU-009,LU-010,LU-011, LU-012, LU-013, LU-015

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR REPLACEMENT OF WING TIP PODS WITHSTANDARD C90A WING TIPS ON THE INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOLLOWING REQUIRED FOR INSTALLATION, BUT NOT FURNISHED WITH KIT: "PR1440"SEALANT, "DEVCON F" FILLER, AND "EA9309NA QT" ADHESIVE. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 11.3 LBS; MOMENT: 1474 IN.-LBSEST. MAN/HRS: : 24 TO 32MEN : 2 (MEN)


KIT CATALOG

90-4118-1BATTERY ACCESS DOOR AIR SCOOP ATA :C90A LJ-1085, LJ-1088 THRU LJ-1533THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW AIR SCOOP ASSEMBLY FOR INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: EC1300L ADHESIVE AND MS20426AD4 RIVETS REQUIRED BUT NOT FURNISHED WITH KIT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


90-4119-1PLACARD, NOSE BAGGAGE/AVIONICS DOOR ATA :65-A90-1 LM-1 THRU LM-14165-A90-2 LS-1 THRU LS-365-A90-3 LT-1, LT-265-A90-3 LT-1, LT-265-A90-4 LU-1 THRU LU-16THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO THE EXTERIOR MARKINGS REGARDINGNOSE LANDING AVIONICS DOOR ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EC3960 EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


90-4121-1AILERON AERODYNAMIC BALANCE WEDGE INSTALLATION ATA : 22THIS KIT PROVIDES PARTS AND INSTRUCTIONS FOR THE INSTALLATION OF AILERON AERODYNAMICBALANCE WEDGES FOR IN-SERVICE AIRCRAFT WHEN EQUIPPED WITH COLLINS AUTOPILOT MODELSAP-106, APC-65, OR APC-65H.

NOTENOTENOTENOTE:::: "MIL-C-38736" SOLVENT AND "EA9394" ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


90-5015- SIMPROVED HEATERINSTALLATION KIT ATA : 21SI NO. 0230-104 ON 90-5015 STHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK THE EXISTING HEATER INSTALLATION INTOAN IMPROVED INSTALLATION ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 90MEN : N/A


KIT CATALOG

90-5027-1 SAIR CONDITIONER START CONTROL ATA :A90, B90 LJ-76, LJ-114 THRU LJ-501SI NO. 0503-351, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED START CONTROL FOR THE AIRCONDITIONER.WT. CHANGE : WT: 8 LBS @ 61 ARMEST. MAN/HRS: : 16MEN : N/A

90-5027-3 SAIR CONDITIONER START CONTROL ATA :90, C90 LJ-1 THRU LJ-75, LJ-77 THRU LJ-113, LJ-502

THRU LJ-565E90 LW-1 THRU LW-5SI NO. 0503-351, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED START CONTROL FOR THE AIRCONDITIONER.WT. CHANGE : WT: 8 LBS @ 61 ARMEST. MAN/HRS: : 16MEN : N/A

90-5027-5 SAIR CONDITIONER START CONTROL ATA :100, A100 B-1 THRU B-123SI NO. 0503-351, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED START CONTROL FOR THE AIRCONDITIONERWT. CHANGE : WT: 8 LBS @ 61 ARMEST. MAN/HRS: : 16MEN : N/A

90-5031-1 SOXYGEN REGULATOR VALVE - SPARES ATA :90, A90, B90 LJ-5, LJ-11 THRU LJ-489THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CONSTANT FLOW SCOTT REGULATOR INLIEU OF A ZEP ZR-665-3 REGULATOR WHICH IS NO LONGER AVAILABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A


KIT CATALOG

90-5034-1 PSHOULDER HARNESS, PILOT AND COPILOT ATA : 25100, A100 B-1 THRU B-223100, A100 B-1 THRU B-22390, A90, B90, C90 LJ-1 THRU LJ-673B100 BE-1E90 LW-1 THRU LW-156SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW SEAT BELT AND SHOULDERHARNESSES FOR EITHER THE PILOT OR COPILOT SEAT. (ORIGINAL EQUIPMENT CHAIRS ONLY, ONE KITPER SEAT)WT. CHANGE : WT: 3 LBS @ 137 ARMEST. MAN/HRS: : 30MEN : N/A

90-5041-1 SVENTILATION BLOWER - SPARES ATA :100 AND A100 B-1 THRU B-24790, A90, B90, C90 LJ-1 THRU LJ-924B100 BE-1 THRU BE-102E90 LW-1 THRU LW-341F90 LA-2 THRU LA-81SI NO. 0762-427 AND "OPTIONAL" SB NO. 2606, APRIL, 1995THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 90-384031-1 BLOWER ASSEMBLY IN LIEU OF50-380116 AND 60-384002-9 ASSEMBLIES ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A

90-5044-1 SS PLRZD WD PNE ATA : 25WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-5046-1 PCONTROL WHEEL, HEAVY TWINS - SPARES ATA :A90 LJ-214, LJ-216 THRU LJ-317THIS KIT PROVIDES PARTS AND INFORMATION TO MODERNIZE THE PILOT AND COPILOT CONTROLWHEELS WITH RAM HORN WHEELS. THE NEW CONTROL WHEEL MAY BE ADAPTED FOR OPTIONALAVIONICS OR SPECIAL EQUIPMENT (ONE KIT REQUIRED FOR EACH WHEEL).WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-5048-1 SWINDSHIELD ANTI-STATIC TAB BONDING ATA :200 BB-77 THRU BB-189A100 B-223 THRU B-230B100 BE-1 THRU BE-18C90 LJ-673 THRU LJ-703E90 LW-152 THRU LW-203CLASS I SI NO. 885, APRIL, 1977THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL WINDSHIELD ANTI-STATIC TABS ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: A GENEROUS AMOUNT OF CONDUCTIVE SILICONE P/N: "72-00002" WILL BE REQUIREDFOR THIS KIT INSTALLATION. IT CAN BE OBTAINED LOCALLY AS INDICATED ON SERVICEINSTRUCTION IF NOT AVAILABLE IN YOUR SHOP STOCK.


90-5051-1 SAIR CONDITIONER MOTOR, IMPROVED ATA :100, A100 B-1 THRU B-225100, A100 B-1 THRU B-22590, A90, B90, C90 LJ-1 THRU LJ-981B100 BE-2 THRU BE-101E90 LW-1 THRU LW-347SI NO. 0718-429, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HIGHER HORSEPOWER COMPRESSORMOTOR, IMPROVED FRAME ASSEMBLY FOR MOUNTING THE MOTOR AND MAKES PROVISIONS FORBETTER ACCESS TO THE COMPRESSOR COMPARTMENT (MOTOR IS INCLUDED)

NOTENOTENOTENOTE:::: THIS KIT ALLOWS USAGE OF CURRENT MOTOR ON AIRCRAFT (NEW OR EXCHANGEMOTOR) REF KIT DRAWING, SHEET 1, SECTION 9A STATEMENT BELOW 8TH LINE BELOW(G) "USE EXISTING MOTOR FOR -5 OR -7 S ONLY" KITS.

WT. CHANGE : WT: 12.53 LBS @ 53 ARMEST. MAN/HRS: : 16MEN : N/A

90-5051-7 SAIR CONDITIONER MOTOR, IMPROVED ATA :100, A100 B-1 THRU B-225100, A100 B-1 THRU B-22590, A90, B90, C90 LJ-1 THRU LJ-678B100 BE-1, BE-2E90 LW-1 THRU LW-165SI NO. 0718-429 ON KIT 90-5051-1 S AND -5 S FOR ADDITIONAL INFORMATION, AS 90-5051-7 S KIT IS SAMEAS -1 S KIT, BUT LESS THE MOTOR, DECALS, WIRE SET, LIMITERS, MOUNTING BASES AND OTHERELECTRICAL HARDWARETHIS PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL AN IMPROVED FRAMEASSEMBLY TO MOUNT THE MOTOR AND COMPRESSOR (WITHOUT FURNISHING THE MOTOR) THATWOULD BE PART OF THE 90-5051-1 S KIT, AND ALSO MAKES PROVISIONS FOR BETTER ACCESS TO THECOMPRESSWT. CHANGE : WT: 12.53 LBS @ 53 ARMEST. MAN/HRS: : 16MEN : N/A


KIT CATALOG

90-5052-1 PFIRE EXTINGUISHER, ENGINE ATA :C90 LJ-502 THRU LJ-1062THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE FIRE EXTINGUISHER SYSTEM FORADDED SAFETY AND PROTECTION. WHEN COMBINED WITH KIT 90-5053-1 P OR 90-5053-3 P, THEYPROVIDE A MEANS TO QUICKLY DETECT AND CONTROL AN ENGINE FIRE.WT. CHANGE : WT: 23.8 LBS @ 137 ARMEST. MAN/HRS: : 80MEN : N/A

90-5053-1 PFIRE DETECTOR, ENGINE ATA :C90 LJ-502 THRU LJ-1062E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE FIRE DETECTION SYSTEMINCORPORATING 3 DETECTORS.WT. CHANGE : WT: 6.12 LBS @ 105.19 ARMEST. MAN/HRS: : 40MEN : N/A

90-5053-3 PFIRE DETECTOR, ENGINE ATA :C90 LJ-502 THRU LJ-1062E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE FIRE DETECTION SYSTEMINCORPORATING 4 DETECTORS.WT. CHANGE : WT: 7.94 LBS @ 102.96 ARMEST. MAN/HRS: : 40MEN : N/A

90-5058-1 SOUTFLOW AND SAFETY VALVE GASKET - SPARES ATA :100, A100 B-1 THRU B-247200 BB-2 THRU BB-568200C BL-1 THRU BL-4200T BT-1 THRU BT-1990, A90, B90, C90 LJ-1 THRU LJ-867B100 BE-1 THRU BE-77E90 LW-1 THRU LW-326F90 LA-2 THRU LA-17THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED GASKET AT THE OUTFLOW ANDSAFETY VALVES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-5059-1 SCONDENSATION DRAIN SEAL - SPARES ATA :100, A100 B-1 THRU B-24790, A90, B90, C90 LJ-1 THRU LJ-1002B100 BE-1 THRU BE-125E90 LW-1 THRU LW-347F90 LA-21 THRU LA-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FORCONDENSATION DRAIN SEALS 50-554267-9 AND 50-554267-29.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5060-1 SPOWER TEST JACK ATA :F90 LA-1 THRU LA-30THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL POWER TEST JACKS TO FACILITATEELECTRICAL SYSTEM MAINTENANCE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5MEN : N/A

90-5061-1 STEMPERATURE SENSOR - SPARES ATA :90, A90, B90 LJ-1 THRU LJ-351THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE SPARES REPLACEMENT FOR THE50-554246-15 TEMPERATURE SENSOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5062-1 SANTI-SIPHON, FUEL ATA :F90 LA-2 THRU LA-62SI NO. 1201, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 101-920061-37 ANTI-SIPHON ASSEMBLIES ATTHE FUEL FILLER PORTS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-5063-1 STURN AND BANK INDICATOR - SPARES ATA :100, A100 B-1 THRU B-247200, B200 BB-2 THRU BB-1025, BB-1027 THRU

BB-1038, BB-1040 THRU BB-1061, BB-1063THRU BB-1076

200C, B200C BL-1 THRU BL-56200CT BN-1200T BT-1 THRU BT-2290, A90, B90, C90 LJ-1 THRU LJ-1040B100 BE-1 THRU BE-134E90 LW-1 THRU LW-347F90 LA-2 THRU LA-195THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT TURN AND BANKINDICATOR (P/N 101-380030-5 OR -9).WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5064-1 SAIR CONTROL VALVE, CABIN ATA :A100 B-157 THRU B-247B100 BE-1 THRU BE-137C90 LJ-576 THRU LJ-1062E90 LW-45 THRU LW-347F90 LA-2 THRU LA-225THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CABIN/COCKPIT HEAT CONTROL VALVE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5065-1 SELEVATOR TRIM TAB CABLE GUARD ATA :200, B200 BB-2 THRU BB-1217200C, B200C BL-1 THRU BL-112, BL-124200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30300 FA-1 THRU FA-38, FA-40 THRU FA-5090, A90, B90, C90, C90A LJ-114 THRU LJ-1110E90 LW-1 THRU LW-347F90 LA-2 THRU LA-235"MANDATORY" SB NO. 2028, REV. 4 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CABLE GUARD AND TORQUELIMITER ON THE ELECTRIC TRIM ACTUATOR.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CABLE GUARDON THE ELEVATOR TRIM CABLE DRUM IN THE PEDESTAL.



KIT CATALOG

90-5065-3 SELEVATOR TRIM TAB CABLE GUARD ATA :A90, B90, C90, C90A LJ-114 THRU LJ-1110E90 LW-1 THRU LW-347"MANDATORY" SB NO. 2028, REV. 4 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CABLE GUARD AND TORQUELIMITER ON THE ELECTRIC TRIM ACTUATOR.

NOTENOTENOTENOTE:::: THIS KIT IS NEEDED ONLY IF TRIM ACTUATOR 33-524023 OR 50-524495 IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4.5MEN : N/A

90-5065-5 SELEVATOR TRIM TAB CABLE GUARD ATA :200, B200 BB-2 THRU BB-1217200C, B200C BL-1 THRU BL-112, BL-124200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30F90 LA-2 THRU LA-235"MANDATORY" SB NO. 2028, REV. 4 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CABLE GUARD AND TORQUELIMITER ON THE ELECTRIC TRIM ACTUATOR.

NOTENOTENOTENOTE:::: THIS KIT IS NEEDED ONLY IF TRIM ACTUATOR 33-524023 OR 50-524495 IS INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4.5MEN : N/A

90-5066-1 PFIRE EXTINGUISHER, ENGINE ATA :A90, B90, C90 LJ-1 THRU LJ-1062THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FIRE EXTINGUISHER SYSTEM ON INSERVICEMODEL C90A AIRCRAFT, PREVIOUSLY EQUIPPED WITH THE FIRE DETECTOR SYSTEM.

NOTENOTENOTENOTE:::: FOR E90 AIRCRAFT SEE 90-5052-3 P KIT AND FOR OTHER 90 MODELS SEE KIT 90-5052-1 PAS C90A SERIAL NUMBERS START AT LJ-1063 THRU LJ-1299, EXCEPT FOR C90B SERIALNUMBERS: LJ-1288, LJ-1295 AND LJ-1300 AND AFTER.

NOTENOTENOTENOTE:::: THIS KIT CONTAINS A RESTRICTED ARTICLE WHICH WILL HAVE TO SHIP SEPARATELYFROM WICHITA, SO YOU NEED TO ORDER EARLY IN THE MORNING TO GET BOTHSHIPPED THE SAME DAY.

NOTENOTENOTENOTE:::: KIT 90-5067 INSTALLS FIRE DETECTOR SYSTEM ON AIRCRAFT NOT PREVIOUSLYEQUIPPED WITH FIRE DETECTOR.

WT. CHANGE : WT: 26.6 LBS; ARM: 135 IN., MOMENT 3591 IN.-LBSEST. MAN/HRS: : 60MEN : N/A


KIT CATALOG

90-5066-3 PFIRE EXTINGUISHER, ENGINE ATA :90 LJ-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WARNING HORN IN CONJUNCTION WITH90-5066-1 P, -5 P OR -7 P KITS FOR FAA CERTIFIED AIRCRAFT.WT. CHANGE : WT: 0.1 LB.; ARM: 90 IN.; MOMENT: 9 IN.-LBSEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

90-5066-5 PFIRE EXTINGUISHER, ENGINE ATA :C90A LJ-1063 THRU LJ-1084, LJ-1086 THRU

LJ-1087THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FIRE EXTINGUISHER SYSTEM ON INSERVICEAIRCRAFT PREVIOUSLY EQUIPPED WITH FIRE DETECTOR SYSTEMS.

NOTENOTENOTENOTE:::: KIT 90-5067 INSTALLS FIRE DETECTOR ON AIRCRAFT NOT PREVIOUSLY EQUIPPED.WT. CHANGE : WT: 26.6 LBS; ARM: 135 IN.; MOMENT: 3591 IN.-LBSEST. MAN/HRS: : 40 TO 60MEN : N/A

90-5066-7 PFIRE EXTINGUISHER, ENGINE ATA :C90A LJ-1085, LJ-1088 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FIRE EXTINGUISHER SYSTEM ON INSERVICEAIRCRAFT PREVIOUSLY EQUIPPED WITH FIRE DETECTOR SYSTEMS.

NOTENOTENOTENOTE:::: KIT 90-5067 INSTALLS FIRE DETECTOR ON AIRCRAFT NOT PREVIOUSLY EQUIPPED.WT. CHANGE : WT: 26.6 LBS; ARM: 135 IN.; MOMENT: 3591 IN.-LBSEST. MAN/HRS: : 40 TO 60MEN : N/A

90-5066-9FIRE EXTINGUISHER INSTALL ENGINE ATA :KING AIR C90GTI LJ-1847, LJ-1853 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FIRE EXTINGUISHER SYSTEM ON INSERVICE MODEL C90GTI AIRCRAFT. PREVIOUSLY EQUIPPED WITH THE FIRE DETECTOR SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT TECH SUPPORTMEN : N/A

90-5067-1 PFIRE DETECTOR, ENGINE (3 DETECTOR SYSTEM) ATA :90 LJ-1063 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ENGINE FIRE DETECTIONSYSTEM, INCORPORATING 3 DETECTORS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT.WT. CHANGE : WT: 3.9 LBS @ 64.5EST. MAN/HRS: : 40 TO 60MEN : N/A


KIT CATALOG

90-5067-3 PFIRE DETECTOR, ENGINE (4 DETECTOR SYSTEM) ATA :90 LJ-1063 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ENGINE FIRE DETECTIONSYSTEM, INCORPORATING 4 DETECTORS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT.WT. CHANGE : WT: 3.9 LBS @ 64.5EST. MAN/HRS: : 60 TO 80MEN : N/A

90-5067-5FIRE DETECTOR INSTL ENGINE ATA :KING AIR C90GTI LJ-1847, LJ-1853 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE FIRE DETECTION SYSTEMINCORPORATING 3 DETECTORS ON IN-SERVICE MODEL C90GTI AIRCRAFT, SERIALS LJ-1847, LJ-1853 ANDAFTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT TECH SUPPORTMEN : N/A

90-5068-1 SSEALANT - BATTERY BOX - ELECTRICAL SHELF ATA :F90 LA-1 THRU LA-133THIS KIT PROVIDES "INFORMATION ONLY" NECESSARY TO SEAL THE BATTERY BOX AND ELECTRICALSHELF INSTALLATION.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5068-3 SSEALANT - BATTERY BOX - ELECTRICAL SHELF ATA :F90 LA-1 THRU LA-201THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE BUS TIE RELAY WITH MOISTUREPROOF RELAY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5069-1 SHEAT DEFLECTOR SHIELD ATA :B90, C90, C90A, E90, F90, 100, A100, B100"MANDATORY" SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES "INFORMATION ONLY" NECESSARY TO INSTALL HEAT DEFLECTOR SHIELDS ONBLEED AIR PLUMBING IN RH AND LH AFT NACELLES FOR HEAT PROTECTION OF FUEL CELLS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : N/A


KIT CATALOG

90-5070-1 SFUEL TOTALIZER GROUND STRAP ATA :C90A LJ-1147 AND AFTER (EQUIPPED WITH

SHADIN DIGITAL FUEL TOTALIZERSYSTEM).

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELECTRICAL BONDING JUMPER TOGROUND THE ENGINE IGNITOR BOX TO THE AIRFRAME ON INSERVICE AIRCRAFT WHEN EQUIPPED WITHTHE SHADIN COMPANY DIGITAL FUEL FLOW INDICATING SYSTEM:WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.3 TO 2MEN : N/A

90-5072-1 SMIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE ATA :65-A90, B90, C90, C90A, E90, F90, 100, A100,B100, 200, A200, B200, B200CT, 300, B300,B300C.THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE PILOT AND COPILOT MICSELECT SWITCH ASSEMBLY P/N: PA-037-246IDI WITH RV6NAYSL103A POT WITH 54D0-03-2-AJN, ADDRV6NAYSL103A POT TO SWITCH (10K POT) SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: -1 S KIT FOR AIRCRAFT WITH MASTER VOL POT (10K POT). NEED TO CHECK RAYTHEONAVIONICS CUSTOMER SUPPORT FOR CONFIRMATION OF SYSTEM ON YOUR AIRCRAFT.



90-5072-3 SMIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE ATA :65-A90, B90, C90, C90A, E90, F90, 100, A100,B100, 200, A200, B200, B200C, B200CT, 300,B300, B300CTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE PILOT AND COPILOT MICSELECT SWITCH ASSEMBLY P/N: PA037-258 (1K POT) WITH RV6NAYSL102A POT WITH P/N: 54D30-03-AJN,ADD RV6NAYSL102A POT TO SWITCH (1K POT) SYSTEM ON INSERVICE AIRCRAFT.


NOTENOTENOTENOTE:::: -3 S KIT FOR AIRCRAFT WITH MASTER VOL POT (1K POT). NEED TO CHECK RAYTHEONAVIONICS CUSTOMER SUPPORT FOR CONFIRMATION OF SYSTEM ON YOUR AIRCRAFT.



KIT CATALOG

90-5072-5MIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE ATA :65-A90, B90, C90, C90A, E90, 100, A100,B100, 200, A200, B200, B200C, B200CT, 300,B300, B300C.THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE PILOT AND COPILOT MICSELECT SWITCH ASSEMBLY P/N: PA037-179IDI WITH RV6NAY5L103C POT WITH P/N: 54D30-03-2-AJN, ADDRV6NAY5L103C POT TO SWITCH (10K POT) SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: -5 KIT FOR AIRCRAFT WITH MASTER VOL POT (10K POT). NEED TO CHECK RAYTHEONAVIONICS CUSTOMER SUPPORT FOR CONFIRMATION OF SYSTEM ON YOUR AIRCRAFT.



90-5072-7MIC SELECT SWITCH, (PILOT AND COPILOT) - SPARE ATA :65-A90, B90, C90, C90A, E90, F90, 100, A100,B100, 200, A200, B200, B200C, B200CT, 300,B300, B300C.THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE PILOT AND COPILOT MICSELECT SWITCH ASSEMBLY P/N: PA037-101IDI WITH RV6NAY5L104C POT WITH P/N: 54D30-03-2-AJN, ADDRV6NAY5L104C POT TO SWITCH (1K POT) SYSTEM AIRCRAFT.


NOTENOTENOTENOTE:::: -7 KIT FOR AIRCRAFT WITH MASTER VOL POT (1K POT). NEED TO CHECK RAYTHEONAVIONICS CUSTOMER SUPPORT FOR CONFIRMATION OF SYSTEM ON YOUR AIRCRAFT.



KIT CATALOG

90-5077-1REFRIGERANT CHANGE AIR CONDITIONER TO R134A ATA :C90A, C90A (SE) LJ-982 THRU LJ-1408THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT TO R134A REFRIGERANT INTHE AIR CONDITIONING SYSTEM ON AIRCRAFT WITH SHANKYO AIR CONDITIONER.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED ITEMS WILL NOT BE FURNISHED WITH THIS KIT: "R134A"REFRIGERANT, "PRIMER N" LOCTITE, "LOCTITE 271" BOTTLE 10CC, AND "FLUSH OIL 1GAL" OR "FLUSH OIL 5 GL" AC FLUSH FLUID. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: IF OLD COMPRESSOR BAD, ORDER KIT 100-5018-1 TO INSTALL R134A COMPRESSOR INCONJUNCTION WITH THIS KIT. BOTH KITS WOULD BE REQUIRED.

NOTENOTENOTENOTE:::: EQUIPMENT AND SUPPLIES REQUIRED: FLUSH CART - A SUITABLE FLUSH CART ISCLASSIC TOOL FLUSH R CART, MANUFACTURED BY CLASSIC TOOL DESIGN, INC. NEWWINDSOR, NY. ANY SUITABLE DEVICE CONSISTING OF A PUMP, RESERVOIR, FILTER, ANDCONTROL VALVE TO CONTROL AND CONTAIN THE SHOP AIR FLOW COULD BESATISFACTORY. FILTERED SHOP AIR: SUPPLYING A MINIMUM OF 90 PSI, FILTERED TOREDUCE MOISTURE, MUST BE SUPPLIED TO THE FLUSH CART. RECOMMENDED FLUSHFLUID IS AC FLUSH SUPPLIED BY CASTROL NORTH AMERICA, SPECIALTY PRODUCTSDIVISION, 16715 VONRMAN AVE., IRVINE, CA. 92714-4918. APPROXIMATELY 5.0 GALLONSWILL BE REQUIRED. RECOMMENDED REFRIGERANT OIL IS RL 100S SUPPLIED BYVIRGINIA KMP 400 PLATINUM WAY, DALLAS, TX 75237. OTHER ESTER REFRIGERANTLUBRICANTS OF ISO 100 VISCOSITY MAY BE USED, APPROXIMATELY 1 QUARTREQUIRED. REFRIGERANT - APPROXIMATELY 5.0 LBS OF R134A REFRIGERANT ISREQUIRED TO CHARGE SYSTEM. LEAK DETECTOR- A LEAK DETECTION DEVICE CAPABLEOF SENSING R134A LEAKS AS SMALL AS 0.5 OZ. PER YEAR IS REQUIRED.



KIT CATALOG

90-5077-3REFRIGERANT CHANGE AIR CONDITIONER TO R134A ATA :90 LJ-78 THRU LJ-113A90 LJ-114 THRU LJ-317B90 LJ-318 THRU LJ-501B90 LJ-318 THRU LJ-501C90 LJ-502 THRU LJ-981THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT TO R134A REFRIGERANT INTHE AIR CONDITIONING SYSTEM WITH YORK AIR CONDITIONER.

NOTENOTENOTENOTE:::: IF OLD COMPRESSOR BAD, ORDER KIT 100-5018-1 TO INSTALL R134A COMPRESSOR INCONJUNCTION WITH THIS KIT. BOTH KITS WOULD BE REQUIRED.

NOTENOTENOTENOTE:::: EQUIPMENT AND SUPPLIES REQUIRED: FLUSH CART - A SUITABLE FLUSH CART ISCLASSIC TOOL FLUSH-R-CART, MANUFACTURED BY CLASSIC TOOL DESIGN, INC. NEWWINDSOR, NY. ANY SUITABLE DEVICE CONSISTING OF A PUMP, RESERVOIR, FILTER, ANDCONTROL VALVE TO CONTROL AND CONTAIN THE SHOP AIR FLOW COULD BESATISFACTORY. FILTERED SHOP AIR: SUPPLYING A MINIMUM OF 90 PSI, FILTERED TOREDUCE MOISTURE, MUST BE SUPPLIED TO THE FLUSH CART. RECOMMENDED FLUSHFLUID IS AC FLUSH SUPPLIED BY CASTROL NORTH AMERICA, SPECIALTY PRODUCTSDIVISION, 16715 VONRMAN AVE., IRVINE, CA. 92714-4918. APPROXIMATELY 5.0 GALLONSWILL BE REQUIRED. RECOMMENDED REFRIGERANT OIL IS RL 100S SUPPLIED BYVIRGINIA KMP 400 PLATINUM WAY, DALLAS, TX 75237. OTHER ESTER REFRIGERANTLUBRICANTS OF ISO 100 VISCOSITY MAY BE USED, APPROXIMATELY 1 QUARTREQUIRED. REFRIGERANT - APPROXIMATELY 5.0 LBS OF R134A REFRIGERANT ISREQUIRED TO CHARGE SYSTEM. LEAK DETECTOR- A LEAK DETECTION DEVICE CAPABLEOF SENSING R134A LEAKS AS SMALL AS 0.5 OZ. PER YEAR IS REQUIRED.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED ITEMS WILL NOT BE FURNISHED WITH THIS KIT: "R134A"REFRIGERANT, "PRIMER N" LOCTITE, "LOCTITE 271" BOTTLE 10CC, AND "FLUSH OIL 1GAL" OR "FLUSH OIL 5 GL" AC FLUSH FLUID. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


90-5078-1FIRE EXTINGUISHERINSTL ATA : 26WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-5078-1 SFIRE EXTINGUISHER (352TS) RELOCATION AFT CABIN FLOOR MOD ATA :C90B LJ-1288, LJ-1295, LJ-1300 THRU LJ-1376"OPTIONAL" SB NO. 2612, APRIL, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE 352TS FIREEXTINGUISHER ON THE AFT CABIN FLOOR TO ELIMINATE THE EXISTING INTERFERENCE WITH THEUNDERSEAT STORAGE COMPARTMENT ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: POTTING COMPOUND FOR INSTALLATION OF INSERTS "METALSET A4 60 OZ" OR"METALSET A4 11 OZ" IS NOT FURNISHED WITH THIS KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY. INSTALL THE INSERTS PER APPROVEDCOMMERCIAL PRACTICE.



KIT CATALOG

90-5079-1PRESSURIZATION CONTROL TUBES ATA :200/B200 BB-114 THRU BB-1553200C, B200C BL-73200C/B200C BL-1 THRU BL-72, BL-124 THRU BL-140200CT/B200CT BN-1 THRU BN-4200T/B200T BT-1 THROUGYH BT-38A100 B-228 THRU B-247A200C (C-12C) BC-19 THRU BC-75, BD-15 THRU BD-30A200C (UC-12B) BJ-1 THRU BJ-66A200CT (C-12D/F) BP-1 AND BP-23, BP-24 THRU BP-63A200CT (FWC-12D) BP-7 THRU BP-11A200CT (RC-12D) GR-1 THRU GR-13A200CT (RC-12G) FC-1 THRU FC-3A200CT (RC-12H) GR-14 THRU GR-19A200CT (RC-12K) FE-1 THRU FE-91A200CT (RC-12N) FE-10 THRU FE-31A200CT (RC-12P) FE-33, FE-35A200CT (RC-12Q) FE-32, FE-34, FE-36B100 BE-6 THRU BE-137B200C (C-12F) BW-1 THRU BW-29B200C (C-12F) BP-64 THRU BP-71B200C (UC-12F/RC-12F) BU-1 THRU BU-12B200C (UC-12M/RC-12M) BV-1 THRU BV-12C90 LJ-683 THRU LJ-1062C90A LJ-1063 THRU LJ-1463E90 LW-177 THRU LW-347F90 LA-1 THRU LA-236H90 LL-1 THRU LL-61PENDING "RECOMMENDED" SB NO. 2676THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NYLON TUBING IN PLACE OF CLEAR POLY-FLOW OR GREY ETHYLENE VINYL ACETATE (EVA) PLASTIC TUBES FOR PRESSURIZATION VACUUMCONTROLS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-5079-3PRESSURIZATION CONTROL TUBES ATA :300 FA-1 THRU FA-230300 (FAA) FF-1 THRU FF-19B300 FL-1 THRU FL-154B300C FN-1B300C FM-1 THRU FM-9PENDING "RECOMMENDED" SB NO. 2676 SEE 90-5079-1 KIT FOR 200 SERIES.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL RUBBER HOSES REINFORCED WITH FABRIC INPLACE OF PLASTIC TUBES FOR PRESSURIZATION VACUUM CONTROLS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5080-1CREW MASK REPL(-5-7-9-11 FOR MASK) ATA :200 BB-55 THRU BB-733, BB-735 THRU BB-792,

BB-794 THRU BB-828, BB-830 THRU BB-853,BB-871 THRU BB-873, BB-892, BB-912

200C BL-1 THRU BL-36300 FA-1 THRU FA-230A100 B-240A200C (C-12A)(C-12C) BC-1 THRU BC-75, BD-1 THRU BD-30A200C (UC-12B) BJ-1 THRU BJ-66A200CT (C-12D) BP-1 THRU BP-6, BP-12 THRU BP-51A200CT (FWC-12D) BP-7 THRU BP-11B100 BE-36 THRU BE-123B200 BB-734, BB-793, BB-829, BB-854 THRU

BB-870, BB-874 THRU BB-891, BB-894 THRUBB-911, BB-913 THRU BB-1443

B200C BL-37 THRU BL-138B200C (C-12F) BP-52 THRU BP-71B200C (RC-12F) BU-11, BU-12B200C (RC-12M) BV11, BV-12B200C (UC-12F) BU-1 THRU BU-10B200C (UC-12M) BV-1 THRU BV-10B200CT (FWC-12D) FG-1, FG-2C90A LJ-755 THRU LJ-1492, LJ-1063 THRU LJ-1353E90 LW-265 THRU LW-347F90 LA-1 THRU LA-236H90 LL-1 THRU LL-61THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OXYGEN MASK STORAGE CUP ASSEMBLIES,WALL OUTLETS, PLUMBING, AND CREW OXYGEN MASKS AS SPARE REPLACEMENTS FOR EXISTINGDILUTER DEMAND OXYGEN MASKS WITH MICROPHONES FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT REQUIRES EITHER -5, -7, -9, OR -11 TO COMPLETE THE INSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-5080-11CREW MASK REPLACEMENT, OXYGEN ATA :C90ATHIS KIT PROVIDES SCOTT/EROS BRAND CREW MASKS (WITHOUT COMFORT CONTROL) AND HOLDINGCUPS TO COMPLETE 90-5080-1 OR -3 KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5080-3CREW MASK REPL(-5-7-9-11 FOR MASK) ATA :C90A LJ-1353 THRU LJ-1427THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OXYGEN MASK STORAGE CUP ASSEMBLIES,AND CREW OXYGEN MASKS AS SPARE REPLACEMENTS FOR EXISTING DILUTER DEMAND OXYGENMASKS WITH MICROPHONES FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT REQUIRES EITHER -5, -7, -9, OR -11 TO COMPLETE THE INSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5080-5CREW MASK REPLACEMENT, OXYGEN ATA :C90ATHIS KIT PROVIDES PURITAN/BENNETT BRAND CREW MASKS (WITH COMFORT CONTROL) AND HOLDINGCUPS TO COMPLETE 90-5080-1 OR -3 KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5080-7CREW MASK REPLACEMENT, OXYGEN ATA :C90ATHIS KIT PROVIDES SCOTT/EROS BRAND CREW MASKS (WITH COMFORT CONTROL) AND HOLDING CUPSTO COMPLETE 90-5080-1 OR -3 KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5080-9CREW MASK REPLACEMENT, OXYGEN ATA :C90ATHIS KIT PROVIDES PURITAN/BENNETT BRAND CREW MASKS (WITHOUT COMFORT CONTROL) ANDHOLDING CUPS TO COMPLETE 90-5080-1 OR -3 KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-5081-1FR12 REFRIGERANT CHANGE FOR R12 FREON SYSTEM ATA :C90, C90ATHIS KIT PROVIDES PARTS AND INSTRUCTIONS REQUIRED TO CONVERT R12 FREON REFRIGERANT INTHE AIR CONDITIONING SYSTEM TO A "FR12" REFRIGERANT SYSTEM.

NOTENOTENOTENOTE:::: FOR 1ST KIT INSTALLATION ESPECIALLY, WICHITA PENNZOIL DISTRIBUTOR HASAVAILABLE IN 12EA-8OZ CASE LOT OF POE ESTER OIL AND 1 CYLINDER 30LBS OF FR12REFRIGERANT, AND A LINE OF FR12 TYPE SERVICE EQUIPMENT. CHECK YOUR LOCALPENNZOIL DISTRIBUTOR OR UNIVERSAL LUBRICANTS, 2821 N. OHIO, WICHITA, KS.

NOTENOTENOTENOTE:::: MODEL C90* PRODUCTION INSTALLATION OF R134A SYSTEM STARTED AT LJ-1417, ALLPRIOR SERIALS HAVE R12 REFRIGERANT. CURRENT EXPANSION VALVE IN AIRCRAFTACCEPTABLE, BUT IF REPLACEMENT REQUIRED USE EXPANSION VALVE P/N: 031134-310.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, POE 8OZ OIL-POLYESTER AND FR12REFRIGERANT.


90-5081-3FR12 REFRIGERANT CHANGE, AIR CONDITIONER ATA :90, A90, B90, E90, F90, H90, 100, A100,B100THIS KIT PROVIDES PARTS AND INSTRUCTIONS REQUIRED TO CONVERT R12 FREON REFRIGERANT INTHE AIR CONDITIONING SYSTEM TO A "FR12" REFRIGERANT SYSTEM.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, POE 8OZ OIL-POLYESTER AND FR12REFRIGERANT.

NOTENOTENOTENOTE:::: FOR 1ST KIT INSTALLATION ESPECIALLY, WICHITA PENNZOIL DISTRIBUTOR HASAVAILABLE IN 12EA-8OZ CASE LOT OF POE ESTER OIL AND 1 CYLINDER 30LBS OF FR12REFRIGERANT, AND A LINE OF FR12 TYPE SERVICE EQUIPMENT. CHECK YOUR LOCALPENNZOIL DISTRIBUTOR OR UNIVERSAL LUBRICANTS, 2821 N. OHIO, WICHITA, KS.


90-5082-1SPARE COMPRESSOR, AIR CONDITIONER ATA :ALL 100’SC90, C90A LJ-982 THRU LJ-1408THIS KIT PROVIDES COMPONENTS AND INFORMATION TO REPLACE THE COMPRESSOR IN THE AIRCONDITIONING SYSTEM ON INSERVICE AIRCRAFT WHICH HAVE BEEN RETROFITTED TO R134A OR FR12REFRIGERENT (WITH SANDEN COMP.) (REFERENCE RAYTHEON KITS 90-5077 AND 90-5081)WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5082-3SPARE COMPRESSOR, AIR CONDITIONER ATA :C90, C90A LJ-1409 AND AFTERTHIS KIT PROVIDES COMPONENTS AND INFORMATION TO REPLACE THE COMPRESSOR IN THE AIRCONDITIONING SYSTEM ON INSERVICE AIRCRAFT USING R134A OR FR12 REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-5085-1FURNISHINGS - INFORMATION ONLY ATA :C90A LJ-1504 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY NECESSARY TO INSTALL THE FURNISHINGS COMPONENTSOMITTED ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5085-3FURNISHINGS - INFORMATION ONLY ATA :C90A LJ-1508 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY NECESSARY TO INSTALL THE FURNISHINGS COMPONENTSOMITTED ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5087-1INDICATOR REPL TURN AND SLIP, AIR ATA : 3120095-B55F-90THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE A UNLIGHTED 101-380030-5 OR -9TURN AND SLIP INDICATOR WITH A LIGHTED 101-380030-7 TURN AND SLIP INDICATOR ON IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5088-1FURNISHINGS - INFORMATION ONLY ATA :C90A LJ-1549 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY NECESSARY TO INSTALL THE FURNISHINGS COMPONENTSOMITTED ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS FOR USE AT RAYTHEON AIRCRAFT OR RAYTHEON AIRCRAFT CENTERS ONLY.WT. CHANGE : WT: MOMENT: AIRCRAFT MUST BE WEIGHED AFTER KIT INSTALLATIONS COMPLETE.

COMPLIANCE WITH FAR 23.25/CAR 3.74 MUST BE MAINTAINED.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5089-1AIRCRAFT OWNERSHIP PLATES INFO ONLY ATA : 31C90A TO BE DETERMINED BY RACCTHIS KIT PROVIDES INFORMATION ONLY REQUIRED TO INSTALL, REPLACE AND/OR REMOVE OWNERSHIPPLACARDS ON LEASED OR FINANCED AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-5093-1PLACARD, SPANISH TRANSLATION ATA : 11C90A WITH STANDARD INTERIORSTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PLACARDS AND DECALS WITH SPANISHTRANSLATIONS.

NOTENOTENOTENOTE:::: "608" ADHESIVE IS REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM RAPID OR YOUR LOCAL SUPPLIER.


90-5095-1ALTIMETER INSTL INFO ONLY ATA : 31C90A LJ-1548 AND AFTER AS APPROPRIATE

WITH A MEGGITT ENCODING ALTIMETERAND ALT ALERTER/PRESELECTOR.

THIS KIT PROVIDES INFORMATION ONLY TO REPLACE THE AIRCRAFT MEGGITT ALTIMETER (28007-01-01)AND PRESELECTOR (10379-11-01) WITH A KOLLSMAN ALTIMETER (28704-D4001) AND PRESELECTOR(45100-D4010).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5095-3ALTIMETER INSTL INFO ONLY ATA : 31C90A LJ-1548 AND AFTER AS APPROPRIATETHIS KIT PROVIDES INFORMATION ONLY TO REMOVE THE -1 KIT AND RETURN THE AIRCRAFT TO THEORIGINAL CONFIGURATION WITH THE MEGGITT ALTIMETER (28007-01-01) AND PRESELECTOR(10379-11-01) REPLACING THE KOLLSMAN ALTIMETER (28704-D4001) AND PRESELECTOR (45100-D401WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-5328-0 1MAGAZINE RACK REPLACEMENT ATA :C90A LJ-1727 & LJ-1738 & AFTER.THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE AND INSTALL MAGAZINE RACKON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NEED S/N AND/OR COLOR OR WOOD TYPE OF FURNITURE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-8002-1 SLANDING GEAR GREASE PROVISIONS, NOSE ATA :100 AND A100 B-1 THRU B-16190, A90, B90, C90 LJ-1 THRU LJ-576E90 LW-1 THRU LW-50SI NO. 0516-200, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL CURRENT PRODUCTION GREASE BUSHINGSAND FITTINGS. (ON MODELS 100 AND A100, USE KIT 99-8003-3 P IN CONJUNCTION WITH THIS KIT TOPROVIDE MAIN LANDING GEAR GREASE PROVISIONS).

NOTENOTENOTENOTE:::: THIS KIT CANNOT BE INSTALLED IF KIT 101-8017-1 HAS BEEN PREVIOUSLY INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 15MEN : N/A

90-8003-1 PBRAKE DEICE, STANDARD LANDING GEAR ATA :F90 LA-6, LA-13, LA-18 THRU LA-185, LA-187

THRU LA-199, LA-201, LA-203, LA-204THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BRAKE DEICE SYSTEM ON AIRPLANESEQUIPPED WITH STANDARD LANDING GEAR.WT. CHANGE : WT: 26 LBS @ 173 ARMEST. MAN/HRS: : 48MEN : N/A

90-8003-3 PBRAKE DEICE, HIGH FLOTATION LANDING GEAR ATA :F90 LA-6, LA-13, LA-18 THRU LA-185, LA-187

THRU LA-199, LA-201, LA-203, LA-204THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BRAKE DEICE SYSTEM ON AIRPLANESEQUIPPED WITH STANDARD LANDING GEAR.WT. CHANGE : WT: 26 LBS @ 173 ARMEST. MAN/HRS: : 48MEN : N/A

90-8011-1 PLANDING GEAR, HYDRAULIC ATA :F90 LA-1 THRU LA-225THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HYDRAULIC LANDING GEAR SYSTEM ONAIRPLANES WITH STANDARD LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-8011-3 PLANDING GEAR INSTALLATION, HYDRAULIC ATA :F90 LA-1 THRU LA-225THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HYDRAULIC LANDING GEAR SYSTEM ONAIRPLANES WITH STANDARD LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-8012-1 SLANDING GEAR EMERGENCY EXTEND PLUMBING ATA :C90A LJ-1063 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TUBES AND FITTINGS TO REPLACEPERMASWAGE TUBES AND FITTINGS ON THE HYDRAULIC LANDING GEAR EMERGENCY EXTENDPLUMBING.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-8013-1 SPLACARD INSTL,HYDRAULIC LANDING ATA : 11WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-8015-0001SUPPORT ASSY ACTUATOR BEARING, MLG ATA : 32C90A LJ-1085, LJ-1088 THRU LJ-1442"MANDATORY" SB NO. 32-3345THIS KIT PROVIDES PARTS AND INSTRUCTIONS FOR THE INSTALLATION OF NEW ACTUATOR SUPPORTBRACKETS, THE NEW BRACKETS (MADE OF STEEL) REPLACE THE OLD BRACKETS (MADE OF ALUMINUM)TO PROVIDE FOR IMPROVING THE SERVICE LIFE ON THE MAIN LANDING GEAR ON IN-SERVICE AWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-9001- SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA : 7190, A90, B90, C90 LJ-1 THRU LJ-667, LJ-670THIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PRATT AND WHITNEY PT6A-6, -20, AND -20A ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-9001-1 SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA :100 AND A100 B-1 THRU B-247C90, C90A LJ-668, LJ-669, LJ-671 AND AFTERE90 LW-1 THRU LW-347THIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PRATT AND WHITNEY PT6A-21, -25, -27 AND -28 ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9001-3 SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA :200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-11 AND AFTERTHIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PRATT AND WHITNEY PT6A-38, -41, AND -42 ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9001-5 SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA :F90 LA-2 AND AFTERTHIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PRATT AND WHITNEY PT6A-34B AND -135 ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9060-1 SPOWER CONTROL CABLE BOOT ATA :100, A100 B-1 THRU B-223100, A100 B-1 THRU B-223200 BB-2 THRU BB-83A90, B90, C90 LJ-76, LJ-114 THRU LJ-673E90 LW-1 THRU LW-156SI NO. 0734-159, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RUBBER BOOT ON THE POWER CONTROLCABLE TO PREVENT MOISTURE FROM ENTERING THE HOUSING AND FREEZING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

90-9061-1 SBLEED AIR WARNING PRESSURE SWITCH REPLACEMENT ATA :200 BB-2 THRU BB-77A100 B-90 THRU B-92, B-94 THRU B-207A100 B-90 THRU B-92, B-94 THRU B-207C90 LJ-502 THRU LJ-639E90 LW-1 THRU LW-119SI NO. 0738-456 AND "OPTIONAL" SB NO. 2207THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EXISTING PRESSURE SWITCHES WHENREQUIRED (EXISTING SWITCHES ARE NO LONGER AVAILABLE).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : N/A

90-9062-3 SFUEL PRESSURE SWITCH, IMPROVED ATA :100, A100 B-1 THRU B-226100, A100 B-1 THRU B-226200 BB-2 THRU BB-11090, A90,. B90, C90 LJ-1 THRU LJ-677E90 LW-1 THRU LW-164SI NO. 0739-282 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE FUEL PRESSURE SWITCHES WITHIMPROVED SWITCHES HAVING FIRE RESISTANT CAPABILITY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

90-9062-5 SFUEL PRESSURESWITCH KIT ATA : 28WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-9064-1 SPROPELLER SEAL DRAIN LINE ATA :90, A90, B90, C90 LJ-1 THRU LJ-670, LJ-672, LJ-674, LJ-676E90 LW-1 THRU LW-161, LW-165SI NO. 0769-241, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DRAIN LINE FOR THE PROPELLER SHAFTSEAL DRAIN.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A


KIT CATALOG

90-9064-5 SPROPELLER SEAL DRAIN LINE ATA :200 BB-2 THRU BB-82SI NO. 0769-241, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DRAIN LINE FOR THE PROPELLER SHAFTSEAL DRAIN.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

90-9067-1 SAUTOPILOT ELEVATORSERVO ATA : 22WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-9068-3 SWASH RING, ENGINE ATA :100, A100 B-1 THRU B-204, B-206 THRU B-247C90, C90A LJ-502 AND AFTERE90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PERMANENTLY MOUNTED ENGINE WASHRINGS FOR CLEANING THE COMPRESSOR SECTION OF THE ENGINES.

NOTENOTENOTENOTE:::: THIS KIT IS NOT APPLICABLE TO AIRPLANES EQUIPPED WITH A BLEED AIR BRAKEDEICER SYSTEM.

WT. CHANGE : C90 AND E90: WT: 12 LBS @ 98 ARM100 AND A100: WT: 12 LBS @ 128 ARM

EST. MAN/HRS: : 12MEN : N/A

90-9070-1 SPROPELLER GROUND IDLE STOP ATA :F90 LA-2 THRU LA-19, LA-21 THRU LA-79, LA-82

THRU LA-99, LA-101 THRU LA-110, LA-112THRU LA-120

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A GROUND IDLE STOP SYSTEM FOR THEPROPELLER. (1 KIT PER AIRCRAFT).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 48MEN : N/A


KIT CATALOG

90-9072-1 SFIREWALL SHUTOFF VALVE - SPARES ATA :100 B-1 THRU B-1890, A90, B90 LJ-1 THRU LJ-478SI NO. 2108, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL WINDSHIELD DEICE ELECTRONICS FORWINDSHIELDS INSTALLED BY KITS 90-3100-1 P OR 90-3100-2 P.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24MEN : 1 (MAN)

90-9072-3 SFIREWALL SHUTOFF VALVE - SPARES ATA :99 U-1 THRU U-49, U-51 THRU U-79C99 U-50 ONLYTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A FUEL FIREWALL SHUTOFFVALVE AS A SPARE REPLACEMENT FOR THE AV-16B-1700B OR 101-389025-1 VALVE ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: FOR MODEL 99’S U-80 AND AFTER FOR A SPARES REPLACEMENT FOR AV-16B-1799B OR101-389025-1 VALVE ONLY PART NUMBER 101-389025-5 IS REQUIRED, NO KIT PURCHASEIS NECESSARY.


90-9072-5CROSSFEED VALVE - SPARES ATA :90, A90 LJ-1 THRU LJ-113THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A SPARE REPLACEMENT FORTHE AV-16B-1795B CROSSFEED VALVE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR FIREWALL SHUTOFF VALVES AV-16B-1700B OR 101-389025-1 NEED TO SEEINFORMATION ON 90-9072-1 S KIT IN YOUR KIT CATALOG OR ON "SSTX" SCREEN.


90-9073-1 PFIRE EXTINGUISHER, ENGINE ATA :F90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LH AND RH ENGINE FIRE EXTINGUISHERSYSTEMS.WT. CHANGE : WT: 24.3 LBS @ 136.2 ARMEST. MAN/HRS: : 80MEN : 1 (MAN)


KIT CATALOG

90-9074-1 PDEICE, 3 BLADE HARTZELL PROPELLER ATA :A90, B90, C90 LJ-76, LJ-114 THRU LJ-954E90 LW-1 THRU LW-347THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A THERMALLY EFFICIENT 28 VOLT 3 BLADEPROPELLER DEICER.WT. CHANGE : N/AEST. MAN/HRS: : 60 TO 80MEN : N/A

90-9075-1 SPARALLELING RELAY DC GENERATOR ATA :100 & A100 B1 THRU B207A90, B90 & C90 LJ114 THRU LJ639E90 LW1 THRU LW119WITH THIS INSTALLATION ABLE TO GO TO SOLID STATE VOLTAGE REGULATOR IF SO DESIRE. SEE SI#:0766-354 REV:II FOR INFORMATION ON PARTS REQUIRED TO MAKE CHANGE OVER TO SOLID STATEVOLTAGE REQULATOR IN CONJUNCTION WITH THIS KIT INSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

90-9077-1 SENGINE MOUNT VIBRATION ISOLATOR CORE - SPARES ATA :100, A100 B-1 THRU B-247200, B200 BB-2 THRU BB-904200C, B200C BL-1 THRU BL-39200CT, B200CT BN-1200T, B200T BT-1 THRU BT-2190, A90, B90, C90 LJ-1 THRU LJ-979E90 LW-1 THRU LW-347F90 LA-2 THRU LA-143THIS KIT PROVIDES PARTS AND INFORMATION FOR THE REPLACEMENT OF AN ENGINE MOUNT ISOLATORCORE R20700-1. 1 KIT PER ENGINE MOUNTING POINT. 4 MOUNTING POINTS PER AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9078-1 SOIL VENT EXHAUST, PT6A ENGINE ATA :F90 LA-226 THRU LA-236SB NO. 2072 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RELOCATED OIL VENT EXHAUST ON BOTHENGINES.WT. CHANGE : WT: 7.2 LBS @ 154.3 ARMEST. MAN/HRS: : 40MEN : 1 (MAN)


KIT CATALOG

90-9078-3 SOIL VENT EXHAUST, PT6A ENGINE ATA :C90A LJ-1085, LJ-1088 THRU LJ-1120SB NO. 2072 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RELOCATED OIL VENT EXHAUST ON BOTHENGINES.WT. CHANGE : WT: 7.2 LBS @ 154.3 ARMEST. MAN/HRS: : 40MEN : N/A

90-9079-1 SOIL VENT EXHAUST, PT6A ENGINE ATA :F90 LA-202, LA-205 THRU LA-225SB NO. 2072 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RELOCATED OIL VENT EXHAUST ON BOTHENGINES.WT. CHANGE : WT: 7.1 LBS @ 154.2 ARMEST. MAN/HRS: : 40MEN : N/A

90-9079-3 SOIL VENT EXHAUST, PT6A ENGINE ATA :C90A LJ-1063 THRU LJ-1084, LJ-1086, LJ-1087SB NO. 2072 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RELOCATED OIL VENT EXHAUST ON BOTHENGINES.WT. CHANGE : WT: 7.2 LBS @ 154.3 ARMEST. MAN/HRS: : 40MEN : N/A

90-9080-1 SPLACARD, CAUTION ATA :C90A LJ-1063 THRU LJ-1116F90 LA-202, LA-205 THRU LA-236SB NO. 2134 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CAUTION PLACARD ON THE UPPERFORWARD ENGINE COWLING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

90-9081-1 SENGINE QUICK CHANGE, PT6A-21 ATA :C90A LJ-1139 THRU LJ-1150THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PT6A-21 ENGINE (EITHER LH OR RH).ENGINE IS INCLUDED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-9083-1 SCOWLING REINFORCEMENT - LOWER FORWARD ATA :C90A LJ-1063 THRU LJ-1161F90-1 LA-202, LA-205 THRU LA-237"OPTIONAL" SB 2218 - 1 KIT PER AIRCRAFTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REINFORCE THE LOWER FORWARDCOWL ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 20 PER COWLMEN : 2 (MEN)

90-9084-1 SINVERTER, LH INSTALLATION - SPARES ATA :65-90, B90, C90THIS KIT IS THE SPARES REPLACEMENT FOR SE-16-3, SE-16-35, SE-16-350, MGH229-100 AND MGH159-200.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9084-2 SINVERTER, RH INSTALLATION - SPARES ATA :65-90, B90, C90THIS KIT IS THE SPARES REPLACEMENT FOR SE-16-3, SE-16-35, SE-16-350, MGH229-100 AND MGH159-200INVERTER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9085-1 SINVERTER ATA :65-90, 65-A90, B90, C90THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 20063, 20121, 20139, 20153 AND F-20-9INVERTERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9085-3 SINVERTER ATA :65090, 65-90A, B90, C90THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR MGH-182-100 AND MG-22-1 INVERTERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-9086-1 SINVERTER - SPARES ATA :65-90, 65-A90, 100THIS KIT IS THE SPARES REPLACEMENT FOR MGE123-400 INVERTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

90-9087-1 SINVERTER - SPARES ATA :B90THIS KIT IS THE SPARES REPLACEMENT FOR THE 20051 INVERTER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9088-1 PFIRE RESISTANT HOSE ATA : 71WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

90-9088-5 PFIRE RESISTANT HOSE ATA :C90, E90, F90, A100, 200, 200CTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE 106200FR-6-46 HOSE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : N/A

90-9088-7 PFIRE RESISTANT HOSE ATA :C90, E90, F90, A100, 200, 200CTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE 106200FR-6-51 HOSE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : N/A

90-9093-0001REMOTE MOUNTED OIL PRESSURE TRANSDUCER ATA :C90A LJ-1139 THRU LJ-1735THIS KIT PROVIDES INFORMATION AND PARTS TO REMOTE MOUNT THE OIL PRESSURE TRANSDUCER ONTHE RIGHT AND LEFT ENGINE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 101-389023-7 REPLACES 101-389023-3 OR 101-389023-5 OIL PRESSURE TRANSDUCER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-9093-0003REMOTE MOUNTED OIL PRESSURE TRANSDUCER ATA :C90 AND C90A LJ-572 THRU LJ-1138F90 LA-2 THRU LA-236THIS KIT PROVIDES INFORMATION AND PARTS TO REMOTE MOUNT THE OIL PRESSURE TRANSDUCER ONTHE RIGHT AND LEFT ENGINE FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

90-94-0001PLACARD INSTL,INTERIOR & EXTERIOR, SPANISH(CHILI) ATA :

C90GT LJ-1835 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PLACARDS AND DECALS WITH SPANISH(CHILI) TRANSLATIONS ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 608" CLEAR ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


91-3001-49VHF ANTENNA ASSEMBLY ATA : 34A200CT (FWC-12D),(RC-12D),(RC-12H),(RC-12K),(RC-12N) & (RC-12P)A90-4 & A90-1 (RU-21H) & (GR V)THIS KIT PROVIDES PARTS & INFORMATION NECESSARY TO INSTALL ANTENNA BASE PLATES AFTERINSTALLATION OF ANTENNA ELEMENT AND/OR NETWORK IN ANTENNA MAST ASSEMBLY ON IN-SERVICEMODELS

NOTENOTENOTENOTE:::: ONLY ORDERS FROM "BASI" ACCEPTABLE FOR THIS MILITARY ONLY KITWT. CHANGE : 5.4 LBS; MOMENT TO BE CALCULATED BY ESL AT TIME OF INSTLNEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

99-3027-1 SLIFT TRANSDUCER HEAT CONTROL ATA :100 B-1 THRU B-155, EXCEPT B-152THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW LIFT TRANSDUCER AND HEATCONTROL PANEL. THIS INSTALLATION REDUCES THE HEAT WHILE THE AIRCRAFT IS ON THE GROUNDFOR INSERVICE AIRCRAFT.WT. CHANGE : WT: ARM: 214”, MOMENT: 428”EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-3027-3 SLIFT TRANSDUCER HEAT CONTROL FOR AIRCRAFT WITH 795-6 OR 795-9TRANSDUCER

ATA :

A100 B-152, B156 THRU B239 EXCEPT B-205795-6 OR 795-9 TRANSDUCER IS NOT IN THIS KIT.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEAT CONTROL PANEL ON AIRPLANES WITHA 795-6 OR 795-9 TRANSDUCER. THIS INSTALLATION REDUCES THE HEAT WHILE THE AIRPLANE IS ONTHE GROUND. TRANSDUCERS NOT INCLUDED WITH KIT INDICATED.WT. CHANGE : WT: 2 LBS, @ 214 ARMEST. MAN/HRS: : 2 TO 4MEN : N/A

99-3028-1 SDIRECTIONAL GYRO - SPARES ATA :C90 LJ-502 THRU LJ-568THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR GYRO P/NAIM200E.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-3038-1 PSERVO AMPLIFIER - SPARES ATA :C90, E90, F90, C99, A100, B100, 200THIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT FOR THE 513-1 SERVO.WT. CHANGE : N/AEST. MAN/HRS: : 180MEN : 1 (MAN)

99-4017- SFLAP EXTENSION MECHANISM ATA :100 AND A100 B-1 THRU B-89, B-9390, A90, B90, C90 LJ-1 THRU LJ-526SI NO. 0673-282, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FUEL DRAIN COLLECTOR SYSTEM TOCATCH FUEL DUMPED DURING ENGINE SHUTDOWN AND RETURN IT TO THE FUEL SYSTEM. THISMODIFICATION IS MANDATORY IN COMPLIANCE WITH ENVIRONMENTAL PROTECTION AGENCYREQUIREMENTS SWT. CHANGE : E90: WT: 10.3 LBS @ 98.6 ARM

100 AND A100: WT: 10.3 LBS @ 128.6 ARMEST. MAN/HRS: : 8MEN : N/A


KIT CATALOG

99-4026-1 SHORIZONTAL STABILIZER HINGE ATA :100, A100, B100SB NO. 2137 OR SUBSEQUENTTHIS KIT CONSIST OF PARTS AND INFORMATION TO REPLACE HINGES ON HORIZONTAL STABILIZER ANDCHANNEL ASSEMBLY ON ELEVATORS. INSTALLATION REQUIRES 99-5020-1 S ALIGNMENT FIXTURE KIT.WT. CHANGE : N/AEST. MAN/HRS: : 26MEN : N/A

99-5012-1 SHORIZONTAL STABILIZER CHECK FIXTURE ATA :100, A100 B-1 THRU B-247B100 BE-1 THRU BE-137THIS KIT PROVIDES INFORMATION TO BUILD A HORIZONTAL STABILIZER ACTUATOR CHECK FIXTURE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-5017-1 PSEAT BELT EXTENDER (BLACK) AIRCRAFT PASSENGER SEATSWITHOUT SHOULDER HARNESS

ATA :

B200HDC (MODEL 1300) BB-1296, BB-1302, BB-1305, BB-1309,BB-1314, BB-1338 THRU BB-1342

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A BLACK SEAT BELT EXTENDERON AIRCRAFT WITH HIGH DENSITY PASSENGER CHAIRS WITHOUT SHOULDER HARNESS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.5MEN : N/A

99-5017-3 PSEAT BELT EXTENDER (BEIGE) AIRCRAFT PASSENGER SEAT WITHSHOULDER HARNESS

ATA :

B200 BB-734, BB-793, BB-829,BB-854 THRU BB-870, BB-874 THRU BB-891,BB-894, BB-896 THRU BB-911, BB-913 THRUBB-923, BB-925 AND AFTER.

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BEIGE SEAT BELT EXTENDER ON AIRCRAFTEXISTING PASSENGER SEATS WITH A SHOULDER HARNESS SYSTEM INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.5MEN : N/A


KIT CATALOG

99-5020-1 SHINGE ALIGNMENT FIXTURE HORIZONTAL STABILIZER ATA :100, A100, B100SB NO. 2137 OR SUBSEQUENTTHIS KIT CONSIST OF ALIGNMENT TOOL AND INFO FOR ALIGNMENT IMPROVED HORIZONTAL STABILIZERHINGES AND BEARING. USED WITH 99-4026-1 S HORIZONTAL STABILIZER HINGE KIT.WT. CHANGE : N/AEST. MAN/HRS: : 26MEN : 1 (MAN)

99-8009-3 SLANDING GEAR GREASE PROVISIONS, MAIN ATA :A100 B-121 THRU B-161SI NO. 0516-200, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL GREASE PROVISIONS ON STANDARD MAINLANDING GEAR.

NOTENOTENOTENOTE:::: USE KIT 90-8002-1 S IN CONJUNCTION WITH THIS KIT TO PROVIDE NOSE GEAR GREASEPROVISIONS.


99-8009-5 SLANDING GEAR GREASE PROVISIONS, MAIN ATA :100, A100 B-1 THRU B-120SI NO. 0516-200, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL GREASE PROVISIONS ON STANDARD MAINLANDING GEAR.

NOTENOTENOTENOTE:::: USE KIT 90-8002-1 S IN CONJUNCTION WITH THIS KIT TO PROVIDE NOSE GEAR GREASEPROVISIONS.


99-9017-1 SIMPROVED PROPELLER SEAL DRAIN ATA :65-90, 65A90, B90, C90SB NO. 2048 OR SUBSEQUENTTHIS KIT CONSIST OF PARTS AND INFORMATION TO INSTALL LARGER DRAIN LINE FOR FLOW DISCHARGETO OVERBOARD BREATHER MANIFOLD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A


KIT CATALOG

99-9017-3 SIMPROVED PROPELLER SEAL DRAIN ATA :F90 LA-1 THRU LA-201,

LA-203 AND LA-204SB NO. 2087, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LARGER DRAIN LINE FOR FLOW DISCHARGETO OVERBOARD BREATHER MANIFOLD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

99-9017-7 SPROPELLER SEAL DRAIN ATA :200 BB-2 THRU BB-202, BB-204 THRU BB-271"OPTIONAL" SB NO. 2087, REV. 1 OR SUBSEQUENTTHIS KIT INSTALLATION FEATURES A LARGER DRAIN LINE TO ALLOW FREE FLOW OF SEAL DISCHARGETO THE COMMON OVERBOARD BREATHER MANIFOLDWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 2 (MEN)

99-9017-9 SPROPELLER SEAL DRAIN ATA :200, B200 BB-203, BB-272 THRU BB-1157, BB-1159

THRU BB-1234200C, B200C BL-1 THRU BL-112, BL-118 THRU BL-126200CT, B200CT BN-1 THRU BN-4200CT, B200CT BN-1 THRU BN-4200T, B200T BT-1 THRU BT-30SB NO. 2087, REV. 1 OR SUBSEQUENTTHIS KIT INSTALLATION FEATURES A LARGER DRAIN LINE TO ALLOW FREE FLOW OF SEAL DISCHARGETO THE COMMON OVERBOARD BREATHER MANIFOLD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : N/A



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberBATTERY CHARGE CURRENT SENSOR - (100-3009-1 S) 1

ANTENNA, MARKER BEACON - SPARES - (100-3016-9 S) 1

SPAR INSTALLATION, OUTBOARD WING, FORWARD - (100-4002-3 S) 1

SPAR INSTALLATION, OUTBOARD WING, FORWARD - (100-4002-4 S) 1

ELEVATOR ASSEMBLY, UPDATE - (100-4005-1 S) 1

SPAR BRIDGE INSTALLATION, WING (STANDARD LANDING GEAR) - (100-4011-1 S) 2

SPAR BRIDGE INSTALLATION, WING (HIGH FLOTATION LANDING GEAR) - (100-4011-3 S) 2

ATTITUDE GYRO - SPARES - (100-5012-1 S) 2

FIRE DETECTOR, ENGINE- SPARES - (100-5017-1 S) 2

MAIN LANDING GEAR INSTALLATION (HIGH FLOTATION GEAR) - (100-8001-3 P) 2




CHIP DETECTOR WARNING, IMPROVED - (100-9013-1 S) 3

IGNITION SPARK - (100-9014-1 S) 4


EXTERNAL POWER OVERVOLTAGE SENSOR - (101-3042-1 S) 4

EMERGENCY LOCATOR TRANSMITTER, NARCO - (101-3046-1 S) 4



TIME INDICATOR - (101-3066-5 P) 5

LANDING GEAR MOTOR, CIRCUIT BREAKER - (101-3069-5 S) 5

FUEL QUANTITY INDICATOR INSTALLATION - (101-3111-1 S) 5

EMERGENCY LOCATOR TRANSMITTER REPLACEMENT - (101-3127-1 S) 6

EXTERNAL POWER SWITCH MODULE INSTALLATION- SPARES - (101-3168-1 S) 6

ANTENNA, MARKER BEACON INSTALLATION - (101-3170-1 S) 6





WING BOLT INSTALLATION, LOWER FORWARD - (101-4024-3 S) 7

WING BOLT INSTALLATION, LOWER FORWARD - (101-4024-5 S) 7

WING BOLT INSTALLATION, UPPER FORWARD - (101-4025-1 S) 7



CHARTHOLDER, BEECHCRAFT CONTROL WHEEL, 720 SERIES - (101-5039-1 P) 8

CARPET FASTENERS - SPARES - (101-5081-1 S) 8



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCONTROL WHEEL REPLACEMENT AND BUILT-UP INFORMATION ON - SPARES - (101-5156-1 S) 9

COMPRESSOR INSTL, AIR CONDITIONING - (101-5170-1) 9









BRAKE SHUTTLE VALVE, DUAL BRAKES - SPARES - (101-8008-1) 11

LANDING GEAR DOOR RETRACT MECHANISM IMPROVEMENT, MAIN - (101-8013-1 S) 11

LANDING GEAR BUSHING, NOSE - (101-8017-1 S) 11

NOSE LANDING GEAR INSTALLATION - (101-8021-3 P) 11

NOSE LANDING GEAR INSTALLATION - (101-8021-7 P) 11

ALUMINUM NOSE WHEEL INSTALLATION - (101-8027-3 P) 12

ALUMINUM NOSE WHEEL INSTALLATION - (101-8027-5 P) 12

NEW NOSE LANDING GEAR PISTON ASSEMBLY WITHY WEIGHT AND BALANCE. - (101-8030-1 S) 12

AIR CONDITIONER COMPRESSOR - SPARES - (101-9021-1 S) 12

AIR CONDITIONER COMPRESSOR - SPARES - (101-9021-5) 13

OIL VAPOR BARRIER - SPARES - (101-9024-1 S) 13

OIL VAPOR BARRIER - SPARES - (101-9024-3 S) 13

SYNCHROPHASER - (101-9029-1 S) 14

PROPELLER DYNAMIC BALANCING - (114-9035-3 S) 14

PROPELLER DYNAMIC BALANCE PROVISIONS INSTALLATION - (90-3084-7 S) 14

PROPELLER DYNAMIC BALANCE PROVISIONS INSTALLATION - (90-3084-9 S) 14


SPEED CONTROL INDICATOR INSTALLATION - (90-3092-5 S) 15

HEATER IGNITION VIBRATOR - SPARES - (90-3093-1 S) 15

HEATER IGNITION UNIT- SPARES - (90-3093-3 S) 15



CENTER SECTION MAIN SPAR INSPECTION PROVISIONS INSTALLATION - (90-4063-1 S) 16

RUDDER PEDAL ARM ASSEMBLY- SPARES - (90-4085-1 S) 16


SPAR BRIDGE INSTALLATION, WING (STANDARD LANDING GEAR) - (90-4090-1 S) 17

SPAR BRIDGE INSTALLATION, WING (HIGH FLOTATION LANDING GEAR) - (90-4090-3 S) 17



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSPAR REINFORCEMENT, LOWER MAIN, LEFT AFT - (90-4101-7 S) 17

SPAR REINFORCEMENT, LOWER MAIN, RIGHT AFT - (90-4101-8 S) 17

WING ATTACH FITTING, AFT UPPER (LH) - (90-4108-1 S) 18

WING FITTING, AFT UPPER (RH) - (90-4108-2 S) 18

WING ATTACH FITTING, AFT LOWER (LH) - (90-4109-1 S) 18

WING ATTACH FITTING, AFT LOWER (RH) - (90-4109-2 S) 18

WING ATTACH FITTING, UPPER FORWARD (LH) - (90-4110-1 S) 18

WING ATTACH FITTING, UPPER FORWARD (RH) - (90-4110-2 S) 19

WING ATTACH FITTING, UPPER FORWARD (LH) - (90-4110-3 S) 19

WING ATTACH FITTING, UPPER FORWARD (RH) - (90-4110-4 S) 19

WING ATTACH FITTING, LOWER FORWARD (LH) - (90-4111-1 S) 19

WING ATTACH FITTING, LOWER FORWARD (RH) - (90-4111-2 S) 19

WING ATTACH FITTING, UPPER AFT (LH) - (90-4113-1 S) 20

WING ATTACH FITTING, UPPER AFT (RH) - (90-4113-2 S) 20

WING ATTACH FITTING, LOWER AFT (LH) - (90-4114-1 S) 20

WING ATTACH FITTING, LOWER AFT (RH) - (90-4114-2 S) 20

WING SPAR BRIDGE FASTENER REPLACEMENT - (90-4115-1) 20

SHOULDER HARNESS INSTALLATION, PILOT AND COPILOT - (90-5034-1 P) 21

TURN AND BANK INDICATOR - SPARES - (90-5063-1 S) 21

HEAT DEFLECTOR SHIELD - (90-5069-1 S) 21

ENGINE HOT SECTION INSPECTION REPLACEMENT PARTS - (90-9001- S) 21


POWER CONTROL CABLE BOOT - (90-9060-1 S) 22

FUEL PRESSURE SWITCH, IMPROVED - (90-9062-3 S) 22

PROPELLER SEAL DRAIN LINE INSTALLATION - (90-9064-1 S) 22

FIREWALL SHUTOFF VALVE INSTALLATION- SPARES - (90-9072-3 S) 22



TRIM IN MOTION INDICATOR CONTROL AND AUDIO CONTROL BOX - (99-3024-1 S) 23

PROPELLER DEICE AMMETER - SPARES - (99-3025-1 S) 23

PROPELLER SECONDARY LOW PITCH STOP REMOVAL - (99-3026-1 S) 23

LIFT TRANSDUCER HEAT CONTROL INSTALLATION - (99-3027-1 S) 23

LIFT TRANSDUCER HEAT CONTROL - (99-3027-3 S) 24

DIRECTIONAL GYRO - SPARES - (99-3028-1 S) 24

WINDSHIELD WIPER MOTOR AND CONVERTER - SPARES - (99-3029-1 S) 24

VOLTAGE REGULATOR - SPARES - (99-3030-1 S) 24

ELECTRICAL LOAD REDISTRIBUTION - (99-3031-1 S) 24



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberHARNESS INSTALLATION, LANDING GEAR - (99-3033-1 S) 25

BLOWER ASSEMBLY, VENTILATION - (99-3034-1 S) 25

FLASHING BEACON, UPPER - (99-3035-0003) 25

BEACON FLASHING, UPPER, OPTIONAL INSTALLATION - (99-3035-1 S) 25

BEACON FLASHING, LOWER, OPTIONAL INSTALLATION - (99-3036-1 S) 25

BEACON FLASHING, BAGGAGE POD, OPTIONAL INSTALLATION - (99-3037-1 S) 26

SERVO AMPLIFIER INSTALLATION- SPARES - (99-3038-1 S) 26

RESISTOR INSTALLATION, OVERHEAD PANEL - (99-3039-1 S) 26

COCKPIT VOICE RECORDER - (99-3040-1 S) 26



CARGO POD INSTALLATION - (99-4002-1 P) 27

FLAP EXTENSION MECHANISM INSTALLATION - (99-4017- S) 27

HORIZONTAL STABILIZER TRAILING EDGE MODIFICATION - (99-4018- S) 27

NOSE BAGGAGE DOOR LATCH INSTALLATION - (99-4019- S) 28

WING ATTACH FITTING HOLE PATTERN TOOL - (99-4021-1 S) 28

WING ATTACH FITTINGS HOLE PATTERN TOOL - (99-4021-3 S) 28

WING MAIN SPAR, IMPROVED - (99-4023-1 S) 28

SPAR CAP, LOWER MAIN AND OUTBOARD WING SPAR ASSEMBLY - (99-4023-3 S) 29

STEP INSTALLATION, FOLDING - (99-4025-1 S) 29

HORIZONTAL STABILIZER HINGE INSTALLATION - (99-4026-1 S) 29

DOOR LOCK SWITCH MOUNT CABIN - (99-4027-1 S) 29

CENTER SECTION AND OUTBOARD WING LOWER MAIN SPAR CAP INSTALLATION - (99-4028-1 S) 29

EXTERIOR PLACARD MARKING - (99-4032-1) 30

STATIC AIR SELECTOR VALVE - (99-5005- S) 30

HORIZONTAL STABILIZER CHECK FIXTURE - (99-5012-1 S) 30

GROSS WEIGHT AND PERFORMANCE INCREASE - (99-5014-1 P) 30

GROSS WEIGHT AND PERFORMANCE INCREASE - (99-5014-3 P) 31

SEAT BELT EXTENDER - (99-5017-1 P) 31

AIR DEFLECTOR (PASSENGER DOOR ONLY REMOVED) CARGO DOOR - (99-5018-1 P) 31

AIR DEFLECTOR INSTALLATION (PASSENGER AND CARGO DOOR ONLY REMOVED) FOR CARGO DOOR -(99-5018-3 P)

31

STATIC LINE SECURING CLAMP - (99-5019-1 S) 32

HINGE ALIGNMENT FIXTURE HORIZONTAL STABILIZER - (99-5020-1 S) 32

PLACARD INSTALLATION, LANDING GEAR ACCUMULATOR - (99-5021-1 S) 32

EVAPORATOR DRAIN RELOCATION - (99-5022-1 S) 32

FIRE EXTINGUISHER *RESTRICTED ARTICLE* - SPARES - (99-5023-1) 33




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFIRE EXTINGUISHER *RESTRICTED ARTICLE* - SPARES - (99-5023-5) 33


AIR CONDITIONING RELIEF VALVE INSTALLATION - (99-5024-1) 34

AIR CONDITIONING RELIEF VALVE INSTALLATION - (99-5024-3) 34

LANDING GEAR RETRACT BRACKET INSTALLATION - (99-8008-1 S) 34

LANDING GEAR GREASE PROVISIONS, MAIN AND NOSE - (99-8009-1 S) 35

LANDING GEAR INSTALLATION, HYDRAULIC - (99-8010-1 P) 35

99-8018-3 ACTUATOR INSTALLATION,HYDRAULIC LANDING GEAR - (99-8018-3) 35

LANDING GEAR HYDRAULIC POWER PACK - SPARES - (99-8019-1 S) 35

LANDING GEAR HYDRAULIC POWER PACK - SPARES - (99-8019-3 S) 35

BRAKE DEICE INSTALLATION, STANDARD LANDING GEAR - (99-8020-1 P) 36

BRAKE DEICE INSTALLATION, HIGH FLOTATION LANDING GEAR - (99-8020-3 P) 36

LANDING GEAR INSPECTION AND COMPONENT INSTALLATION, NOSE - (99-8022-1 S) 36

LANDING GEAR INSPECTION AND COMPONENT INSTALLATION, STANDARD MAIN - (99-8023-1 S) 36

LANDING GEAR INSPECTION AND COMPONENT INSTALLATION, HIGH FLOTATION MAIN - (99-8024-1 S) 36

SERVICE VALVE RETAINER - (99-8025-3 S) 37

SERVICE VALVE RETAINER AND HAT SECTION - (99-8025-5 S) 37

LANDING GEAR ACTUATOR SEALS, HYDRAULIC MAIN - SPARES - (99-8026-1 S) 37

LANDING GEAR ACTUATOR SEALS, HYDRAULIC NOSE - SPARES - (99-8026-11 S) 37

LANDING GEAR ACCUMULATOR SEALS, HYDRAULIC - SPARES - (99-8026-3 S) 37

LANDING GEAR SERVICE VALVE SEALS, HYDRAULIC - SPARES - (99-8026-5 S) 38

LANDING GEAR POWER PACK SEALS, HYDRAULIC - SPARES - (99-8026-7 S) 38

LANDING GEAR HAND PUMP SEALS, HYDRAULIC - SPARES - (99-8026-9 S) 38

CABIN AUXILIARY HEAT - (99-9003- P) 38

CABIN AUXILIARY HEAT - (99-9003-3 P) 38

OIL LINE HOSE ASSEMBLY- SPARES - (99-9011-1 S) 39

HEATER, POWER CONTROL CABLE - (99-9012-1 S) 39

FUEL CHECK VALVE- SPARES - (99-9014-1 S) 39

WATER MENTHANOL INJECTION SYSTEM INSTALLATION - (99-9015-1 P) 39

PROPELLER, IMPROVED SEAL DRAIN - (99-9017-5 S) 39

PROPELLER, IMPROVED SEAL DRAIN - (99-9018-1) 40


KIT CATALOG

100-3009-1 SBATTERY CHARGE CURRENT SENSOR ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-151SI NO. 0587-356 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A BATTERY CHARGE CURRENT DETECTINGDEVICE TO MONITOR THE CONDITION OF THE NICKEL-CADMIUM BATTERY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

100-3016-9 SANTENNA, MARKER BEACON - SPARES ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT MARKER BEACONANTENNA.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-4002-3 SSPAR INSTALLATION, OUTBOARD WING, FORWARD ATA :99, 99A, A99A, B99 PRIOR TO U-154 EXCEPT U-50 (C99)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH OUTBOARD WING FORWARD SPAR. SPARIS INCLUDED IN THE KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-4002-4 SSPAR INSTALLATION, OUTBOARD WING, FORWARD ATA :99, 99A, A99A, B99 PRIOR TO U-154 EXCEPT U-50 (C99)THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE A RH OUTBOARD WING FORWARD SPAR.SPAR IS INCLUDED IN THE KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-4005-1 SELEVATOR ASSEMBLY, UPDATE ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164SI NO. 0799-133, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK ONE ELEVATOR ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)


KIT CATALOG

100-4011-1 SSPAR BRIDGE INSTALLATION, WING (STANDARD LANDING GEAR) ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLING A WING SPAR BRIDGE ON AIRPLANESEQUIPPED WITH STANDARD LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-4011-3 SSPAR BRIDGE INSTALLATION, WING (HIGH FLOTATION LANDING GEAR) ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLING A WING SPAR BRIDGE ON AIRPLANESEQUIPPED WITH HIGH FLOTATION LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-5012-1 SATTITUDE GYRO - SPARES ATA :B99, C99 U-50, U-152 THRU U-165THIS KIT IS THE SPARES REPLACEMENT FOR 500ECF, 100-384070-1 OR 101-384120-1 GYROS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-5017-1 SFIRE DETECTOR, ENGINE- SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES A SPARES REPLACEMENT FIRE DETECTOR FOR 30-215.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

100-8001-3 PMAIN LANDING GEAR INSTALLATION (HIGH FLOTATION GEAR) ATA :C99 U-165 AND AFTERTHIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL HIGH FLOTATION MAIN LANDING GEARSON AIRCRAFT EQUIPPED WITH HYDRAULIC GEAR AND PNEUMATIC BRAKE DEICE.WT. CHANGE : N/AEST. MAN/HRS: : 250MEN : 1 (MAN)


KIT CATALOG

100-9008-1 SENGINE FUEL DRAIN COLLECTOR ATA :99, 99A U-1 THRU U-49, U-51 THRU U-131, U-133

THRU U-145, U-147SI NO. 0673-282, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FUEL DRAIN COLLECTOR SYSTEM TOCATCH FUEL DUMPED DURING ENGINE SHUTDOWN AND RETURN IT TO THE FUEL SYSTEM. THISMODIFICATION IS MANDATORY IN COMPLIANCE WITH ENVIRONMENTAL PROTECTION AGENCYREQUIREMENTS SWT. CHANGE : WT: 10.3 LBS @ 128.6 ARMEST. MAN/HRS: : 8MEN : 1 (MAN)

100-9011-1 SENGINE CHIP DETECTOR ATA :99, 99A, A99A, 899 U-1 THRU U-49, U-51 THRU U-164SI NO. 0733-257 REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CHIP DETECTOR AND TEST POINTS TODETECT METAL PARTICLES IN THE OIL. ONE KIT IS REQUIRED FOR EACH ENGINE.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

100-9011-3 SENGINE CHIP DETECTOR ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164SI NO. 0733-257, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE PROVISIONS FOR A CHIP DETECTOR(NOT FURNISHED WITH THIS KIT) TO DETECT METAL PARTICLES IN THE OIL. ONE KIT IS REQUIRED FOREACH ENGINE.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

100-9013-1 SCHIP DETECTOR WARNING, IMPROVED ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO ADD AN ANNUNCIATOR PANEL WARNING LIGHT TO THECHIP DETECTOR INSTALLATION FOR IMPROVED OIL CONDITION MONITORING. AIRPLANES WITHOUT CHIPDETECTORS WILL REQUIRE INSTALLATION OF KIT 100-9011 -1 S OR 100-9011-3 S FORWT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

100-9014-1 SIGNITION SPARK ATA :99A, A99A, B99THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SPARK IGNITION ON AIRPLANES EQUIPPEDWITH PT6A-21, -27 OR -28 ENGINES (1 KIT PER AIRCRAFT). THIS KIT CONSISTS OF IGNITION EXCITERS,IGNITERS, CABLE ASSEMBLIES, IGNITION CONNECTOR PLUGS, BRACKET ASSEMBLIESWT. CHANGE : WT: 3 LBS, ARM: 135 IN.; MOMENT: 405 IN. LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3039-1 SEMERGENCY LOCATOR TRANSMITTER REMOTE SWITCH ATA :B99 U-149 THRU U-164SI NO. 1139, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REMOTE SWITCH FOR THE TR70-13 E.L.T.(ELT AND BATTERY PACK ARE NOT PART OF THIS KIT).WT. CHANGE : N/AEST. MAN/HRS: : 2-5MEN : 1 (MAN)

101-3042-1 SEXTERNAL POWER OVERVOLTAGE SENSOR ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO ADD AN OVERVOLTAGE SENSOR TO PROTECTONBOARD CIRCUITS AND INSTRUMENTS DURING EXTERNAL POWER OPERATIONS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3046-1 SEMERGENCY LOCATOR TRANSMITTER, NARCO ATA :B99 U-149 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NARCO ELT UNIT TO REPLACE TR70-13 ORTR70-09 TRANSMITTERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3055-3 PTIME INDICATOR INSTALLATION ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELAPSED TIME INDICATOR FOR ALL 28-VDC ELECTRICAL EQUIPMENT REQUIRING AN INSPECTION AT INTERVALS UP TO 2,000 HOURS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-3066-3 PTIME INDICATOR INSTALLATION ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELAPSED TIME INDICATOR FOR ALL 28-VDC ELECTRICAL EQUIPMENT REQUIRING AN INSPECTION AT INTERVALS UP TO 2,000 HOURS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-3066-5 PTIME INDICATOR ATA :100, A100 B-1 THRU B-247200, B200 BB-2 AND AFTER200C, B200C BL-1 AND AFTER200CT, B200CT BN-1 AND AFTER200T, B200T BT-1 AND AFTER90, A90, B90, C90, C90A LJ-1 AND AFTERB100 BE-1 THRU BE-137E90 LW-1 THRU LW-347F90 LA-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ELAPSED TIME INDICATOR FOR ALL 28-VDC ELECTRICAL EQUIPMENT REQUIRING AN INSPECTION AT INTERVALS UP TO 10,000 HOURS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3069-5 SLANDING GEAR MOTOR, CIRCUIT BREAKER ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164SB NO. 2035 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LANDING GEAR MOTOR CIRCUIT BREAKERFOR INSERVICE AIRCRAFT WITH MECHANICAL GEAR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

101-3111-1 SFUEL QUANTITY INDICATOR INSTALLATION ATA :C99THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE 100-380006-47, 101-384150-7 AND101-384151 FUEL QUANTITY INDICATOR WITH REPLACEMENT INDICATOR.WT. CHANGE : N/AEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)


KIT CATALOG

101-3127-1 SEMERGENCY LOCATOR TRANSMITTER REPLACEMENT ATA :99THIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL AN ARTEX 110-4-002 E.L.T. ONIN-SERVICE AIRCRAFT THAT WERE PREVIOUSLY EQUIPPED WITH COMMUNICATIONS COMPONENTSCORP. TR70-09, TR70-13 AND TR70-17 OR NARCO ELT 10 OR DOME MARGOLIN DMN8-1 TRANSM

NOTENOTENOTENOTE:::: THIS KIT CAN ONLY BE USED IN CONJUNCTION WITH 101-3210-1 & -3, OR 36-3020-1 KITSTO BE IN COMPLIANCE WITH LATEST FAA REGULATIONS. IF NO KIT IS AVAILABLE FORINSTRUMENT PANEL INSTALLATION FOR YOUR AIRCRAFT, CONTACT PRODUCTSUPPORT BEFORE ORDERING 101-3127-1 S.


101-3168-1 SEXTERNAL POWER SWITCH MODULE INSTALLATION- SPARES ATA :99 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT OF THE 101-361045-1 OR -5OVERVOLTAGE SWITCH MODULE ASSEMBLY ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

101-3170-1 SANTENNA, MARKER BEACON INSTALLATION ATA :99, 99A, A99A, B99, C99THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION FOR SPARES REPLACEMENT OF100-384120 MARKER BEACON ANTENNA WITH A 101-384179 MARKER BEACON ANTENNA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10 TO 12 HRSMEN : 1 (MAN)




KIT CATALOG

101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES FOR PROPER ELECTRICAL BONDING TO METALS ON ALL NON-COMPOSITERAYTHEON AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-4019-5 SVENTRAL FIN - SPARES ATA :C99 U-50, U-165 THRU U-182THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 99-440023-61 FIN ASSEMBLY AS A SPARESREPLACEMENT FOR THE 99-440023-23 ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4024-3 SWING BOLT INSTALLATION, LOWER FORWARD ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164 WITH KIT

99-4023-1 S INSTALLEDC99 U-50, U-165 THRU U-179SI NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4024-5 SWING BOLT INSTALLATION, LOWER FORWARD ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164 WITHOUT

KIT 99-4023-1 S INSTALLEDSI NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4025-1 SWING BOLT INSTALLATION, UPPER FORWARD ATA :B99 U-50, U-165 THRU U-179SI NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-4025-5 SWING BOLT INSTALLATION, UPPER FORWARD ATA :B99 U-151 THRU U-164SI NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-4025-7 SWING BOLT INSTALLATION, UPPER FORWARD ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-150SI NO. 1235 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN INCONEL WING ATTACH BOLT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5039-1 PCHARTHOLDER, BEECHCRAFT CONTROL WHEEL, 720 SERIES ATA :C99 U-50, U-165 THRU U-239THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CHART HOLDER WHICH ALLOWS ADEQUATENIGHT TIME LIGHTING OF MAPS AND CHARTS WITHOUT INTERFERING WITH THE PILOT'S NIGHT VISION.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 1, FOR ADDITIONAL INFORMATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5 TO 1.5MEN : 1 (MAN)

101-5081-1 SCARPET FASTENERS - SPARES ATA :99THIS KIT PROVIDES A SPARES REPLACEMENT FOR SJ 3283 HEDLOCK FASTENERS USED ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES 25 PAIRS OF CARPET FASTENERS (50 PARTS, 25 FOR ATTACHMENTTO CARPET BACKING AND 25 FOR ATTACHMENT TO THE FLOORPANEL.) YOU NEED TOCHANGE ALL YOUR SJ3283 FASTENERS TO THE REPLACEMENT FASTENERS AT THESAME TIME FOR OVERALL INTEGRITY OF THE SYSTEM.

NOTENOTENOTENOTE:::: ADHESIVE "EC847 QT" WILL BE REQUIRED FOR USE WITH THIS KIT. IF NOT IN YOU SHOPSTOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

101-5156-1 SCONTROL WHEEL REPLACEMENT AND BUILT-UP INFORMATION ON -SPARES

ATA :

99 SERIES ALLTHIS KIT WILL FURNISH A REPLACEMENT CONTROL WHEEL FOR THE 720-042-200, 720-042-203 OR50-524592-( ) WHEEL; 720-1001, 720-1002, 720-1401, 720-1402, 720-4401, OR 720-4402 WHEEL ASSEMBLIES.

THIS KIT CONTAINS A CONTROL WHEEL ASSEMBLY WITH FINGER GRIPS AWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

101-5170-1COMPRESSOR INSTL, AIR CONDITIONING ATA :99, A99, B99, C99 U-1 THRU U-239THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A/C COMPRESSORS FOR AIRCRAFT WITH AHEAVY DUTY COMPRESSOR AND R-12 REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5170-3COMPRESSOR INSTL, AIR CONDITIONING ATA :99, A99, B99, C99 U-1 THRU U-239THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A/C COMPRESSORS FOR AIRCRAFT WITH AHEAVY DUTY COMPRESSOR AND R-134A REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5170-5COMPRESSOR INSTL, AIR CONDITIONING ATA :99, A99, B99, C99 U-1 THRU U-239THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A/C COMPRESSORS FOR AIRCRAFT WITH AHEAVY DUTY COMPRESSOR AND FR-12 REFRIGERANT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5171-1COMPRESSOR SERVICE FITTING CHANGE ATA :99, A99, A99A, B99, C99 ALL SERIESTHE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY GM TYPECOMPRESSORS. (FOR R-12 SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-5171-17COMPRESSOR SERVICE FITTING CHANGE ATA :99, A99, A99A, B99, C99 ALL SERIALSTHE PURPOSE OF THIS KIT IS TO MODIFY EXISTING NON-STEP PORT COMPRESSOR FITTINGS TO BESTEP PORT-TYPE COMPRESSOR FITTINGS FOR USE WITH NEW LIGHT WEIGHT, GM-TYPECOMPRESSORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5171-3COMPRESSOR SERVICE FITTING CHANGE ATA :99, A99, A99A, B99, C99 ALL SERIALSTHE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY GM TYPECOMPRESSORS. (FOR FR-12 SERVICE PORTS).WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

101-5171-5COMPRESSOR SERVICE FITTING CHANGE ATA :99, A99, A99A, B99, C99 ALL SERIALSTHE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY GM TYPECOMPRESSORS. (FOR R-134A SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPRTMEN : N/A

101-5171-7COMPRESSOR SERVICE FITTING CHANGE ATA :99, A99, A99A, B99, C99 ALL SERIALSTHE PURPOSE OF THIS KIT IS TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICEPORTS MOUNTED VERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY GM TYPECOMPRESSORS. (FOR R-12 SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5171-9COMPRESSOR SERVICE FITTING CHANGE ATA :99, A99, A99A, B99, C99 ALL SERIALSTHE PURPOSE OF THIS KIT IS TO PROVIDE STEP PORT COMPRESSOR FITTINGS FOR USE WITH SPAREREPLACEMENT LIGHT WEIGHT, GM-TYPE COMPRESSORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-8008-1BRAKE SHUTTLE VALVE, DUAL BRAKES - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED BRAKE SHUTTLE VALVES AS ASPARES REPLACEMENT.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

101-8013-1 SLANDING GEAR DOOR RETRACT MECHANISM IMPROVEMENT, MAIN ATA : 3299, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164SI NO. 1114 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED SWITCH AND LINK ASSEMBLYFOR THE HIGH FLOTATION LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : 1 (MAN)

101-8017-1 SLANDING GEAR BUSHING, NOSE ATA :99, 99A, A99A, B99, C99 U-1 THRU U-170THIS KIT PROVIDES PARTS AND INFORMATION TO REWORK THE NOSE LANDING GEAR BRACE.

NOTENOTENOTENOTE:::: THIS KIT CANNOT BE INSTALLED IF KIT 90-8001-2 S HAS BEEN PREVIOUSLY INSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-8021-3 PNOSE LANDING GEAR INSTALLATION ATA :ALL MODEL 99 AIRLINERSTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 50-820204-41 BRACE ASSEMBLY ON IN-SERVICE AIRCRAFT. OIL AIR STRUT INSTRUCTION PLATE NOT FURNISHED WITH KIT. ORDER ASREQUIRED.WT. CHANGE : 8 LBS. @ 34 IN.EST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

101-8021-7 PNOSE LANDING GEAR INSTALLATION ATA :ALL MODEL 99 AIRLINERSTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 50-820196-671 NOSE GEAR ASSEMBLYON IN-SERVICE AIRCRAFT. DOES NOT INCLUDE WHEEL AND TIRE.WT. CHANGE : 16 LBS.; MOMENT: -52 IN. -LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-8027-3 PALUMINUM NOSE WHEEL INSTALLATION ATA :99, 99A, B99, C99THIS KIT IS THE SPARES REPLACEMENT FOR 101-8015-11, 50-300011-43, 50-300011-29 OR 50-300011-1 TIREAND WHEEL ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-8027-5 PALUMINUM NOSE WHEEL INSTALLATION ATA :THIS KIT IS THE SPARES REPLACEMENT FOR 101-8015-3, 50-300011-41, 50-300011-23 OR 50-300011-19WHEEL ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-8030-1 SNEW NOSE LANDING GEAR PISTON ASSEMBLY WITHY WEIGHT ANDBALANCE.

ATA :

99, 99A, A99A, B99, C99SB NO. 2103, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT FOR 101-820072-1,101-820025-5, 101-820025-3, 101-820025-1, 115-820066-3, 50-820197-11, 50-820197-9, 50-820197-7,50-820197-5, 50-820197-3 AND 50-820197-1 NOSE LANDING GEAR LOWER SHOCK ASSEMBLWT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

101-9021-1 SAIR CONDITIONER COMPRESSOR - SPARES ATA :99, 99A, A99A, B99THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 101-555214-1 COMPRESSOR WITH A 24-VOLTCLUTCH AS A SPARE FOR A 115-555040-1 COMPRESSOR ASSEMBLY WITH A 12-VOLT CLUTCH ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MS20995C32 LOCK-WIRE REQUIRED BUT IS NOT FURNISHED WITH THE KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

101-9021-5AIR CONDITIONER COMPRESSOR - SPARES ATA :99, 99A, A99A, B99KITS 101-5160, 101-5163, 101-5168, 99-5025, 99-5026 ON IN-SERVICE AIRCRAFT.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMPRESSOR WITH A 24-VOLT CLUTCH ASA SPARE FOR A 115-555040-1 COMPRESSOR ASSEMBLY WITH A 12-VOLT CLUTCH AND WITH AN AIRCONDITIONING SYSTEM THAT HAS BEEN RETROFITTED TO R134A OR FR-12 REFRIGERANTS.

NOTENOTENOTENOTE:::: MS20995C32 LOCKWIRE REQUIRED BUT IS NOT FURNISHED WITH THE KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. 555040-1COMPRESSOR ASSEMBLY WITH A 12-VOLT CLUTCH ON IN-SERCICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT CONTAIN A COMPRESSOR. THE COMPRESSOR MUST BE INSTALLEDPER KIT 101-5170 AND MUST MATCH THE TYPE OF REFRIGERANT CURRENTLY USED INTHE AIR CONDITIONING SYSTEM.


101-9024-1 SOIL VAPOR BARRIER - SPARES ATA :99A U-89, U-93, U-96, U-97, U-101, U-104, U-105,99A U-115 THRU U-118, U-123,99A U-110 THRU U-113,99A U-125 THRU U-135,99A, A99A, B99 U-36, U-80 THRU U-85,99A, B99 U-137 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 101-389026-1 OIL VAPOR BARRIERASSEMBLY IN THE TORQUE TRANSMITTER VENT SYSTEM AS A SPARES REPLACEMENT FOR THE25LHN-1-E AIR FILTER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-9024-3 SOIL VAPOR BARRIER - SPARES ATA :C99 U-50, U-165 THRU U-207THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARE REPLACEMENT TUBE AND HOSEFOR THE ORIGINAL 330997F-4-0074 HOSE USED ON THE VAPOR BARRIER INSTALLATION.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

101-9029-1 SSYNCHROPHASER ATA :C99 U-165 THRU U-225"OPTIONAL" SB NO. 2115THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED TYPE II SYNCHROPHASERCONTROL BOX ON IN-SERVICE AIRCRAFT.

THESE AIRCRAFT ALL HAVE CONTROL BOX 213762 FOR A TYPE II SYNCHROPHASER CURRENTLYINSTALLED ON THE PILOT'S SIDE OF THE PEDESTAL.WT. CHANGE : N/AEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

114-9035-3 SPROPELLER DYNAMIC BALANCING ATA :ALL MODEL 99 AIRLINERS ALL SERIALSTHIS KIT PROVIDES "INFORMATION ONLY" ON HOW TO MODIFY THE COWLING AND WHERE TO ROUTEWIRING FOR DYNAMIC PROPELLER BALANCING USING THE CHADWICK HELMUTH MODEL 8500 OR 192ASYSTEMS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

90-3084-7 SPROPELLER DYNAMIC BALANCE PROVISIONS INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DYNAMIC PROPELLER BALANCINGPROVISIONS FOR USE WITH A CHADWICK HELMUTH OR SIMILAR TYPE TEST UNIT. (TEST UNIT NOTFURNISHED WITH KIT).

NOTENOTENOTENOTE:::: SEE CLASS 2, SERVICE INSTRUCTION NO. 0928 FOR ADDITIONAL INFORMATION ONSD119B BALANCE ANALYZER (CHADWICK-HELMUTH) AND MODEL 330 VIBRATIONANALYZER AND DYNAMIC BALANCER OF INTERNATIONAL RESEARCH ANDDEVELOPMENT CORP.


90-3084-9 SPROPELLER DYNAMIC BALANCE PROVISIONS INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SEE 90-3084-7 S IF KIT FOR USE WITH CHADWICK-HELMUTH SYSTEM OR SIMILAR TYPE UNIT.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DYNAMIC PROPELLER BALANCINGPROVISIONS FOR USE WITH A SPECTRAL DYNAMICS OR SIMILAR TYPE TEST UNIT. (TEST UNIT NOTFURNISHED WITH KIT).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 2 (MEN)


KIT CATALOG

90-3085-3 SBRUSH BLOCK ASSEMBLY, MODULAR ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SI NO. 1075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR 4E1311-1 OR -2BRUSH BLOCK ASSEMBLIES WHERE APPLICABLE.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : 1 (MAN)

90-3092-5 SSPEED CONTROL INDICATOR INSTALLATION ATA :99, 99A, A99A, B99 PRIOR TO U-160THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE 571-28 SPEED CONTROL INDICATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3093-1 SHEATER IGNITION VIBRATOR - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATER IGNITION VIBRATOR AS A SPARESREPLACEMENT FOR THE 12C60 AND 12C60-1VIBRATORS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3093-3 SHEATER IGNITION UNIT- SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATER IGNITION UNIT AS A SPARESREPLACEMENT FOR THE 11-C30 IGNITION UNIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-3106-1 SOIL PRESSURE TRANSDUCER INSTALLATION ATA :C99"OPTIONAL" SB NO. 2159, REV. 2 FOR AIRCRAFT SERIAL NUMBER EFFECTED. ALSO REFERENCE SI NO.1072THIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACEMENT OF ENGINE OIL PRESSURETRANSDUCERS WITH REPLACEMENT TRANSDUCERS WITH GOLD PINS WHICH ALLEVIATE THEPOSSIBILITY OF ANY CORROSION AND ACCOMPANYING FLUCTUATIONS DUE TO ELECTRICAL SIGNALINTERRUPTION ON

NOTENOTENOTENOTE:::: SERVICE BULLETIN NO. 1072 NEEDS TO BE COMPLIED WITH BEFORE 90-3106-1 S KIT ISINSTALLED AS THIS KIT DOES NOT CONTAIN INDICATOR, CLIP OR ETC. 90-3106-1 SFURNISHES IMPROVED TRANSDUCERS AND NECESSARY HARDWARE FOR INSTALLATIONOF SAME. CHECK SERVICE BULLETIN NO. 1072 TO SEE IF IT EFFECTS YOUR AIRCRAFTSERIAL NUMBER AND ORDER ACCORDINGLY.

WT. CHANGE : NEGLIGIBLE (1 KIT PER AIRCRAFT)EST. MAN/HRS: : 1MEN : 1 (MAN)

90-3119-0001REMOTE MOUNTED OIL PRESSURE TRANSDUCER ATA :C99 U-50, U-165 THRU U-239;A100THIS KIT PROVIDES INFORMATION AND PARTS TO INSTALL AN IMPROVED OIL PRESSURE TRANSDUCERAND ELECTRICAL CONNECTOR ON THE RIGHT AND LEFT ENGINE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 101-389023-7 REPLACES 101-389003-1 OR 101-389023-3 OR 101-389023-5 OIL PRESSURETRANSDUCER.

NOTENOTENOTENOTE:::: DIRECT MOUNTED TRANSDUCERS (TRANSDUCERS INSTALLED ON THE ENGINE) WILLNOW BE OFF-MOUNTED AS SHOWN IN THIS KIT.

NOTENOTENOTENOTE:::: EXISTING OFF-MOUNTED TRANSDUCERS WILL BE PROVIDED A NEW HOSE ASSY ANDMOUNTING HARDWARE WHEN INSTALLING THE NEW TRANSDUCER.


90-4063-1 SCENTER SECTION MAIN SPAR INSPECTION PROVISIONS INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SI NO. 0388-018, REV 6 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE VARIOUS ACCESS DOORS FOR THEINSPECTION OF THE MAIN SPAR AND TO REPLACE VARIOUS HUCK BOLTS AND JO-BOLTS.WT. CHANGE : N/AEST. MAN/HRS: : 36MEN : 1 (MAN)

90-4085-1 SRUDDER PEDAL ARM ASSEMBLY- SPARES ATA :99, 99A, A99A, B99, C99 U-1 THRU U-173THIS KIT PROVIDES A SPARES REPLACEMENT FOR 50-524326-1 OR -11 LH RUDDER PEDAL ARMASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-4085-2 SRUDDER PEDAL ARM ASSEMBLY - SPARES ATA :99, 99A, A99A, B99, C99 U-1 THRU U-173THIS KIT PROVIDES A SPARES REPLACEMENT FOR 50-524326-2 OR -12 RH RUDDER PEDAL ARMASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-4090-1 SSPAR BRIDGE INSTALLATION, WING (STANDARD LANDING GEAR) ATA :C99 U-50, U-165 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WING SPAR BRIDGE ON AIRPLANESEQUIPPED WITH STANDARD LANDING GEAR CONTACT PRODUCT SUPPORT FOR ADDITIONALINFORMATION.WT. CHANGE : WT: 100.3 LBS @ 190 ARMEST. MAN/HRS: : 400 TO 500MEN : 1 (MAN)

90-4090-3 SSPAR BRIDGE INSTALLATION, WING (HIGH FLOTATION LANDING GEAR) ATA :C99 U-50, U-165 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WING SPAR BRIDGE ON AIRPLANESEQUIPPED WITH HIGH FLOTATION LANDING GEAR. CONTACT PRODUCT SUPPORT FOR ADDITIONALINFORMATION.WT. CHANGE : WT: 99.3 LBS @ 190 ARMEST. MAN/HRS: : 400 TO 500MEN : 1 (MAN)

90-4101-7 SSPAR REINFORCEMENT, LOWER MAIN, LEFT AFT ATA :99, A99, 99A, A99A, B99SB NO. 2267 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REINFORCE SPAR OF LOWER MAIN SPAR CAP, LEFTAFT NACELLE.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : 1 (MAN)

90-4101-8 SSPAR REINFORCEMENT, LOWER MAIN, RIGHT AFT ATA :99, A99, 99A, A99A, B99SB NO. 2267 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REINFORCE SPAR OF LOWER MAIN SPAR CAP,RIGHT AFT NACELLE.WT. CHANGE : N/AEST. MAN/HRS: : 80MEN : 1 (MAN)


KIT CATALOG

90-4108-1 SWING ATTACH FITTING, AFT UPPER (LH) ATA :99, 99A, A99A, B99THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT UPPER WING 35-115059-4 ATTACHFITTING, LH OUTBOARD AFT WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4108-2 SWING FITTING, AFT UPPER (RH) ATA :99, 99A, A99A, B99THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT UPPER WING 35-115059-5 ATTACHFITTING, RH OUTBOARD AFT WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4109-1 SWING ATTACH FITTING, AFT LOWER (LH) ATA :99, 99A, A99A, B99 U-1 THRU U-164THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT LOWER WING 35-115058-2 ATTACHFITTING, LH OUTBOARD AFT WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4109-2 SWING ATTACH FITTING, AFT LOWER (RH) ATA :99 THRU B99 (AS -1 S KIT)THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE AFT LOWER WING 35-115058-1 ATTACHFITTING, RH OUTBOARD AFT WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4110-1 SWING ATTACH FITTING, UPPER FORWARD (LH) ATA :99, 99A, A99A, 699 U-1 THRU U-150THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD LH WING 50-120074-2ATTACH FITTING, CENTER SECTION FORWARD WING SPARWT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)


KIT CATALOG

90-4110-2 SWING ATTACH FITTING, UPPER FORWARD (RH) ATA :99 THRU B99 (AS -1 S KIT) U-1 THRU U-150THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD RH WING 50-120074-3ATTACH FITTING, CENTER SECTION FORWARD WING SPARWT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4110-3 SWING ATTACH FITTING, UPPER FORWARD (LH) ATA :B99 U-151 THRU U-164THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD LH WING 50-120074-4ATTACH FITTING, CENTER SECTION WING SPARWT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4110-4 SWING ATTACH FITTING, UPPER FORWARD (RH) ATA :B99 U-151 THRU U-164THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER FORWARD RH WING 50-120074-5ATTACH FITTING, CENTER SECTION FORWARD WING SPARWT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4111-1 SWING ATTACH FITTING, LOWER FORWARD (LH) ATA :99, 99A, A99A, B99THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER FORWARD WING 50-120073-7ATTACH FITTING, CENTER SECTION FORWARD WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4111-2 SWING ATTACH FITTING, LOWER FORWARD (RH) ATA :99 THRU B99 (AS -1 S KIT)THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER FORWARD WING 50-120073-8ATTACH FITTING, CENTER SECTION FORWARD WING SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)


KIT CATALOG

90-4113-1 SWING ATTACH FITTING, UPPER AFT (LH) ATA :99, 99A, A99A, B99THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER AFT LH WING 50-120014 ATTACHFITTING, CENTER SECTION REAR SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4113-2 SWING ATTACH FITTING, UPPER AFT (RH) ATA :B99 (AS -1 S KIT)THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE UPPER AFT RH WING 50-120014-1 ATTACHFITTING, CENTER SECTION REAR SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4114-1 SWING ATTACH FITTING, LOWER AFT (LH) ATA :99, 99A, A99A, B99 U-1 THRU U-164THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER AFT LH WING 50-120015 ATTACHFITTING, CENTER SECTION REAR SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4114-2 SWING ATTACH FITTING, LOWER AFT (RH) ATA :99 THRU B99 (AS -1 S KIT) U-1 THRU U-164THIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE LOWER AFT RH WING 50-120015-1ATTACH FITTING, CENTER SECTION REAR SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 50MEN : 2 (MEN)

90-4115-1WING SPAR BRIDGE FASTENER REPLACEMENT ATA :99, 99A, A99A, B99THIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO REPAIR/AND OR IMPROVE WING SPAR BRIDGESPLICE JOINT INSTALLED BY RAYTHEON KIT DRAWINGS 90-4089 OR 100-4011. ONLY AIRCRAFT MODIFIEDBY THESE KIT DRAWINGS ARE APPLICABLE TO THIS KIT. MODELS THAT WERE APPROVEDWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

90-5034-1 PSHOULDER HARNESS INSTALLATION, PILOT AND COPILOT ATA : 2599, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SB NO. 2031, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW SEAT BELT AND SHOULDERHARNESSES FOR EITHER THE PILOT OR COPILOT SEAT (RAYTHEON ORIGINAL EQUIPMENT CHAIRSONLY, ONE KIT PER SEAT).WT. CHANGE : WT: 3 LBS @ 137 ARMEST. MAN/HRS: : 30MEN : 1 (MAN)

90-5063-1 STURN AND BANK INDICATOR - SPARES ATA :99, 99A, A99A, B99, C99 U-1 THRU U-195, U-197 THRU U-200THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT TURN AND BANKINDICATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-5069-1 SHEAT DEFLECTOR SHIELD ATA :ALSO MODELS 99, A99, A99A, B99PER CO G05993,SB NO. 2267 OR SUBSEQUENTTHIS KIT PROVIDES INFORMATION ONLY NECESSARY TO INSTALL HEAT DEFLECTOR SHIELDS ON BLEEDAIR PLUMBING IN RH AND LH AFT NACELLES FOR HEAT PROTECTION OF FUEL CELLS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

90-9001- SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA :99, 99A, A99A U-1 THRU U-145, EXCEPT U-50 AND U-146THIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PRATT AND WHITNEY PT6A-20.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-9001-1 SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA :99, 99A, A99A, B99 U-36, U-80 THRU U-164THIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PRATT AND WHITNEY PT6A-27 OR -28 ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

90-9060-1 SPOWER CONTROL CABLE BOOT ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SI NO. 0734-159, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RUBBER BOOT ON THE POWER CONTROLCABLE TO PREVENT MOISTURE FROM ENTERING THE HOUSING AND FREEZING.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

90-9062-3 SFUEL PRESSURE SWITCH, IMPROVED ATA :99,99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SI NO. 0739-282 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE FUEL PRESSURE SWITCHES WITHIMPROVED SWITCHES HAVING FIRE RESISTANT CAPABILITY.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

90-9064-1 SPROPELLER SEAL DRAIN LINE INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-164, EXCEPT U-50SI NO. 0769-241, REV. 1 OR SUBSEQUENTWT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

90-9072-3 SFIREWALL SHUTOFF VALVE INSTALLATION- SPARES ATA :99, 99A U-1 THRU U-49, U-51 THRU U-79C99 U-50THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A FUEL FIREWALL SHUTOFFVALVE AS A SPARE REPLACEMENT FOR THE AV-16B-1700B VALVE.

NOTENOTENOTENOTE:::: FOR MODEL 99'S U-80 AND AFTER FOR A SPARES REPLACEMENT FOR AV-16B-1700B OR101-389025-1 VALVE ONLY PART NUMBER: 101-389025-5 IS REQUIRED, NO KIT PURCHASEIS NECESSARY.


99-2002-1 SEXTERIOR PLACARD ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-2003-1 SINTERIOR PLACARD ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-3024-1 STRIM IN MOTION INDICATOR CONTROL AND AUDIO CONTROL BOX ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164SI NO. 0656-350, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SINGLE COMPONENT TRIM IN MOTIONINDICATOR CONTROL AND AUDIO NOISE CONTROL BOX ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

99-3025-1 SPROPELLER DEICE AMMETER - SPARES ATA :99, 99A, A99A, 699 U-1 THRU U-49, U-51 THRU U-163THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT PROPELLER DEICEAMMETER.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

99-3026-1 SPROPELLER SECONDARY LOW PITCH STOP REMOVAL ATA :99, 99A, A99A, B99 U-36, U-80 THRU U-164SI NO. 0844-247, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE PROPELLER SECONDARY LOW PITCHSTOP SYSTEM ON AIRPLANES EQUIPPED WITH PT6A-27 OR -28 ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : 10MEN : 1 (MAN)

99-3027-1 SLIFT TRANSDUCER HEAT CONTROL INSTALLATION ATA :99 SERIES U-1 THRU U-151THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW LIFT TRANSDUCER WHICH PROVIDESFOR REDUCED HEAT ON THE GROUND FOR EXTENDED SERVICE LIFE.WT. CHANGE : WT: + 2.0 LBS @ 214.00 ARMEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)


KIT CATALOG

99-3027-3 SLIFT TRANSDUCER HEAT CONTROL ATA :B99 U-152 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEAT CONTROL PANEL ON AIRPLANESEQUIPPED WITH A 795-6 OR -9 TRANSDUCER. THIS INSTALLATION REDUCES THE HEAT WHILE THEAIRPLANE IS ON THE GROUND. TRANSDUCER NOT INCLUDED WITH KIT.WT. CHANGE : WT: 2 LBS @ 214 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-3028-1 SDIRECTIONAL GYRO - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-155THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR GYROAIM200E.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-3029-1 SWINDSHIELD WIPER MOTOR AND CONVERTER - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THEWINDSHIELD WIPER MOTOR AND CONVERTER 50-380051-3.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-3030-1 SVOLTAGE REGULATOR - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SPARES REPLACEMENTS FOR THECSV1152-10 VOLTAGE REGULATORS.

NOTENOTENOTENOTE:::: SERIALS U-3, U-5 THRU U-10 AND U-13 THRU U-25 MUST HAVE COMPLIED WITHRAYTHEON SERVICE INSTRUCTION NO. 0162-355 OR SUBSEQUENT.


99-3031-1 SELECTRICAL LOAD REDISTRIBUTION ATA :C99 U-50, U-165 THRU U-192, U-194 THRU U-198SB NO. 2008 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED BUS FEEDER DISTRIBUTION.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

99-3033-1 SHARNESS INSTALLATION, LANDING GEAR ATA :C99 U-50, U-165 THRU U-179, U-181 THRU U-184,

U-186 THRU U-192, U-194 THRU U-196SB NO. 2012 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REDUCE THE POSSIBILITY OF ERRATIC COMPASSREADINGS WHILE THE LANDING LIGHTS ARE IN USE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-3034-1 SBLOWER ASSEMBLY, VENTILATION ATA :99, 99A, A99A, B99, C99 U-1 THRU U-49, U-51 THRU U-231THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE115-384007 BLOWER ASSEMBLY.WT. CHANGE : WT: 7 2 LBS @ 74.5 ARMEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

99-3035-0003FLASHING BEACON, UPPER ATA :99 99A, A99A, B99 AND C99 ALLTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WHELEN FLASHING BEACONAS REPLACEMENT FOR GRIMES ROTATING BEACON ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "890" PROSEAL & "ALODINE 1200" CORROSION PREVENTATIVE REQUIRED, BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


99-3035-1 SBEACON FLASHING, UPPER, OPTIONAL INSTALLATION ATA :99, 99A, A99A, B99, C99THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WHELEN FLASHING BEACON(BEACON, ATTACHING HARDWARE AND INSTALLATION DRAWING) AS A REPLACEMENT FOR GRIMESROTATING BEACON.

WHELEN FLASHING BEACON USES A HALOGEN FLASH TUBE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

99-3036-1 SBEACON FLASHING, LOWER, OPTIONAL INSTALLATION ATA :99, 99A, A99A, B99, C99THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WHELEN FLASHING BEACON.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)


KIT CATALOG

99-3037-1 SBEACON FLASHING, BAGGAGE POD, OPTIONAL INSTALLATION ATA :99, 99A, A99A, B99, C99 AIRCRAFT WITH BAGGAGE POD

INSTALLATIONTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A WHELEN FLASHING BEACONAS A REPLACEMENT FOR THE GRIMES ROTATING BEACON.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

99-3038-1 SSERVO AMPLIFIER INSTALLATION- SPARES ATA :C99THIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT FOR THE 513-1 SERVO.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

99-3039-1 SRESISTOR INSTALLATION, OVERHEAD PANEL ATA :C99 U-50, U-165 THRU U-239SB NO. 2222 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE RESISTORS FROM THE OVERHEAD CONTROLPANEL ASSEMBLY TO PREVENT RESISTOR OVERHEATING.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

99-3040-1 SCOCKPIT VOICE RECORDER ATA :99, A99, B99, C99 U-1 THRU U-239THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COCKPIT VOICE RECORDER ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT INSTALLS CONTROL IN BRACKET AT AFT END OF STANDARD PEDESTAL.WT. CHANGE : N/AEST. MAN/HRS: : 48 TO 90MEN : 1 (MAN)


NOTENOTENOTENOTE:::: THIS KIT INSTALLS CONTROL IN CUTOUT ON TOP OF EXTENDED PEDESTAL.WT. CHANGE : N/AEST. MAN/HRS: : 48 TO 90MEN : 1 (MAN)


KIT CATALOG


NOTENOTENOTENOTE:::: THIS KIT INSTALLS CONTROL IN BRACKET ON AFT END OF EXTENDED PEDESTAL.WT. CHANGE : N/AEST. MAN/HRS: : 48 TO 90MEN : 1 (MAN)

99-4002-1 PCARGO POD INSTALLATION ATA :99, A99, 99A, A99AINCREASE PAYLOAD CAPABILITIES OF YOUR AIRCRAFT WITH THE CARGO AND BAGGAGE POD KIT.GREAT FOR FREIGHT. PROVIDES AN UNOBSTRUCTED CARGO AREA APPROXIMATELY 11 FEET 3 INCHESLONG, 3 FEET 5 INCHES WIDE, 14 INCHES DEEP WITH A CAPACITY OF 88.5 CUBIC FEET. VERSATI

NOTENOTENOTENOTE:::: THE BASIC ANTENNA RELOCATION KIT IS INCLUDED IN THE CARGO AND BAGGAGE PODKIT.

NOTENOTENOTENOTE:::: THIS KIT WAS DESIGNED FOR IN PLANT INSTALLATION.WT. CHANGE : WT: 148 LBS @ 204 ARMEST. MAN/HRS: : 200MEN : 1 (MAN)

99-4017- SFLAP EXTENSION MECHANISM INSTALLATION ATA :99, 99A, A99A U-1 THRU U-49, U-51 THRU U-145, U-147SI NO. 0604-160 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED FLAP DRIVE SYSTEM,COMPLETE WITH FLEX DRIVE SHAFTS, ACTUATORS, DRIVE MOTOR AND GEARBOX.WT. CHANGE : WT: -7.2 LBS @ 74.5 ARMEST. MAN/HRS: : 40MEN : 1 (MAN)

99-4018- SHORIZONTAL STABILIZER TRAILING EDGE MODIFICATION ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-146SI NO. 0467-131 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE HORIZONTAL STABILIZER TRAILING EDGETO ACCOMMODATE IMPROVED ALUMINUM ELEVATORS. ELEVATORS NOT INCLUDED WITH KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-4019- SNOSE BAGGAGE DOOR LATCH INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-148SI NO. 0501-113 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CERAMIC DOOR LATCHING ASSEMBLY ONTHE NOSE BAGGAGE DOOR. ONE KIT PER DOOR.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

99-4021-1 SWING ATTACH FITTING HOLE PATTERN TOOL ATA :99, 99A, A99A, B99 U-1 THRU U-49, U- 51 THRU U-150SI NO. 0986 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO FABRICATE A LH AND RH WING ATTACH FITTINGSHOLE PATTERN TO BE USED WITH KIT 99-4023-1 S.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-4021-3 SWING ATTACH FITTINGS HOLE PATTERN TOOL ATA :B99 U-151 THRU U-164SI NO. 0986 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO FABRICATE A LH AND RH WING ATTACH FITTINGSHOLE PATTERN TO BE USED WITH KIT 99-4023-1S.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-4023-1 SWING MAIN SPAR, IMPROVED ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164 WITH

10,000 AIRFRAME HOURS OR MORESI NO. 0986 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LOWER CENTER SECTION MAIN SPARCAP AND THE OUTBOARD WING MAIN SPARS. THIS PROVIDES A SERVICE LIFE OF 20,000 HOURS WITHFEWER REQUIRED INSPECTIONS SPAR AND SPAR CAP INCLUDED WITH KIT.

NOTENOTENOTENOTE:::: KITS, 99 4021 1 S (SERIALS U-1 THRU U-49 AND U-51 THRU U-150), 99-4021-3 S AND 101-4025-5 S (SERIALS U-151 THRU U-164), ARE REQUIRED FOR THE INSTALLATION OF THISKIT.



KIT CATALOG

99-4023-3 SSPAR CAP, LOWER MAIN AND OUTBOARD WING SPAR ASSEMBLY ATA :99, 99A, A99, A99A, B99 U-1 THRU U-164 EXCEPT U-50THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A REPLACEMENT TO THE LOWERMAIN SPAR CAP AND OUTBOARD WING MAIN SPAR ASSEMBLIES ON AIRCRAFT WHICH HAVE THE99-4023-1 S KIT INSTALLED.

NOTENOTENOTENOTE:::: THIS KIT IS FOR 99'S THAT HAD 99-4023-1 KIT INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1600MEN : 1 (MAN)

99-4025-1 SSTEP INSTALLATION, FOLDING ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FOLDING STEP ON AIRPLANES EQUIPPEDWITH A FIXED STEP MAIN ACCESS AIRSTAIR DOOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-4026-1 SHORIZONTAL STABILIZER HINGE INSTALLATION ATA :99, 99A, A99A, B99, C99SB NO. 2137 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REPLACE HINGES ON HORIZONTAL STABILIZER ANDCHANNEL ASSEMBLY ON ELEVATORS. INSTALLATION REQUIRES 99-5020-1 S ALIGNMENT FIXTURE KIT.WT. CHANGE : N/AEST. MAN/HRS: : 26MEN : 2 (MEN)

99-4027-1 SDOOR LOCK SWITCH MOUNT CABIN ATA :99, 99A, A99A, B99, C99SB NO. 2088 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION FOR MODIFICATION OF CABIN DOOR LOCK SWITCHHARDWARE.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

99-4028-1 SCENTER SECTION AND OUTBOARD WING LOWER MAIN SPAR CAPINSTALLATION

ATA :

C99 U-50, U-165 THRU U-239THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE CENTER SECTION LOWERMAIN SPAR CAP AND OUTBOARD WING MAIN SPAR ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1600MEN : 1 (MAN)


KIT CATALOG

99-4032-1EXTERIOR PLACARD MARKING ATA :ALLTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE EXTERIOR MARKINGSREGARDING DOOR OPENING PROCEDURES FOR IN SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EC3960" EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTRACT PRODUCT SUPPORTMEN : N/A

99-5005- SSTATIC AIR SELECTOR VALVE ATA :99 U-1 THRU U-103, U-106 THRU U-135SI NO. 0291-394THIS KIT CONSISTS OF PARTS AND INFORMATION FOR MODIFICATION OF PRIMARY AND ALTERNATESTATIC AIR SYSTEMS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

99-5012-1 SHORIZONTAL STABILIZER CHECK FIXTURE ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES INFORMATION TO BUILD A HORIZONTAL STABILIZER ACTUATOR CHECK FIXTURE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-5014-1 PGROSS WEIGHT AND PERFORMANCE INCREASE ATA :99, 99A U-1 THRU U-49, U-51 THRU U-55THIS KIT PROVIDES PARTS AND INFORMATION TO INCREASE THE GROSS WEIGHT TO 10,900 LBS ANDALLOW A PERFORMANCE INCREASE EQUAL TO THAT OF THE MODEL B99, 680 SHP, 1628 FT/LB TORQUEAT 2,200 PROPELLER RPM, MAXIMUM 725°C ITT.

NOTENOTENOTENOTE:::: KITS 99-4023-1 S, 99-5005 S AND 99-4017 S MUST BE INSTALLED PRIOR TO OR INCONJUNCTION WITH THE INSTALLATION OF THIS KIT.



KIT CATALOG

99-5014-3 PGROSS WEIGHT AND PERFORMANCE INCREASE ATA :99, 99A, A99A U-1 THRU U-49, U-51 THRU U-55 WITH

115-620010-305 OR -459 HORIZONTALSTABILIZER INSTALLEDU-56 THRU U-145, U-147

THIS KIT PROVIDES PARTS AND INFORMATION TO INCREASE THE GROSS WEIGHT TO 10,900 LBS ANDALLOW A PERFORMANCE INCREASE EQUAL TO THAT OF THE MODEL B99, 680 SHP, 1628 FT/LB TORQUEAT 2,200 PROPELLER RPM, MAXIMUM 725°C ITT.

NOTENOTENOTENOTE:::: KITS 99-4023-1 S AND 99-4017 S MUST BE INSTALLED PRIOR TO OR IN CONJUNCTIONWITH THE INSTALLATION OF THIS KIT. KIT 99-5005 S MUST ALSO BE INSTALLED FOR U-1THRU U-49, U-51 THRU U-103 AND U-106 THRU U-135.


99-5017-1 PSEAT BELT EXTENDER ATA :C99 U-50, U-165 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SEAT BELT EXTENDER ON EXISTINGPASSENGER SEATS. BLACK (ONE KIT PER SEAT).WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-5018-1 PAIR DEFLECTOR (PASSENGER DOOR ONLY REMOVED) CARGO DOOR ATA :99, 99A, A99A, B99, C99 AIRCRAFT WITH ACARGO

U-1 AND AFTER

NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT PART NUMBER 130944 WILL BE REQUIRED FOR USAGEWITH THIS KIT BUT IS NOT PART OF KIT. YOU WILL NEED TO ORDER IT SEPARATELY.

WT. CHANGE : WT: -34 LBS @ 312 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-5018-3 PAIR DEFLECTOR INSTALLATION (PASSENGER AND CARGO DOOR ONLYREMOVED) FOR CARGO DOOR

ATA :

99, 99A, A99A, B99, C99 U-1 AND AFTERNOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT PART NUMBER: 130944 REQUIRED BUT NOT FURNISHED

AS PART OF THIS KIT. YOU WILL NEED TO ORDER IT SEPARATELY.WT. CHANGE : WT: -62 LBS @ 311 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-5019-1 SSTATIC LINE SECURING CLAMP ATA :C99SB NO. 2097 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO REDUCE POSSIBILITY OF MOISTURE BEINGTRAPPED IN NAV/PITOT STATIC LINES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 5MEN : 1 (MAN)

99-5020-1 SHINGE ALIGNMENT FIXTURE HORIZONTAL STABILIZER ATA :99, 99A, A99A, B99, C99SB NO. 2137 OR SUBSEQUENTTHIS KIT CONSISTS OF ALIGNMENT TOOL AND INFORMATION FOR ALIGNMENT IMPROVED HORIZONTALSTABILIZER HINGES AND BEARINGS. USED WITH 99-402-1 S HORIZONTAL STABILIZER HINGE KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 26MEN : 2 (MEN)

99-5021-1 SPLACARD INSTALLATION, LANDING GEAR ACCUMULATOR ATA :99, C99SB NO. 2238 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PLACARD SHOWING HOW TO SERVICE THEHYDRAULIC LANDING GEAR ACCUMULATOR. FOR AIRPLANES WITH HYDRAULIC LANDING GEARINSTALLED PER KIT 99-8010.WT. CHANGE : N/AEST. MAN/HRS: : 2.5MEN : 1 (MAN)

99-5022-1 SEVAPORATOR DRAIN RELOCATION ATA :C99 U-50, U-165 THRU U-238"OPTIONAL" SB NO. 2469THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO DIRECT WATER TO THE OUTSIDE OFTHE BAGGAGE POD AFT FAIRING.

NOTENOTENOTENOTE:::: THE FOLLOWING SEALERS AND ADHESIVES ARE NOT FURNISHED WITH KIT. IF NOTALREADY IN YOUR SHOP STOCK, MAY BE PROCURED LOCALLY.

ADHESIVE PART NUMBER "EA9309 QT"SEALER PART NUMBER "EC2216A/B 20Z"URALANE KIT PART NUMBER "5776"

THE ADHESIVE AND SEALER ARE AS REQUIRED, THE URALANE ONE PER AIRCRAFT.THESE ARE PERISHABLEITEMS WHICH SHOULD BE OBTAINED NO MORE THAN 30 DAYS PRIOR TO EXPECTED KITINSTALLATION ON AIRCRAFT.



KIT CATALOG

99-5023-1FIRE EXTINGUISHER *RESTRICTED ARTICLE* - SPARES ATA :B99 U-146 THRU U-164C99 U-50, U-165 THRU U-230THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE 344T FIREEXTINGUISHER LOCATED ON THE COPILOT'S CHAIR WITH AN AMEREX 352TS FIRE EXTINGUISHER ONTHE ABOVE IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: *RA* MEANS THIS KIT CONTAINS A RESTRICTED ARTICLE THAT SHIPS SEPARATELYFROM WICHITA. YOU WILL NEED TO ORDER EARLY IN THE MORNING TO HAVE BOTHSHIPPED THE SAME DAY.

WT. CHANGE : WT: 2 5 LBS; MOMENT 315 IN. LBS (INCREASE)EST. MAN/HRS: : 3MEN : 1 (MAN)

99-5023-3FIRE EXTINGUISHER *RESTRICTED ARTICLE* - SPARES ATA :B99 U-146 THRU U-164C99 U-50, U-165 THRU U-230THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE 344T FIREEXTINGUISHER LOCATED ON THE COPILOT'S CHAIR WITH A "GENERAL" PART NUMBER GH2-1/2J FIREEXTINGUISHER ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: *RA* MEANS THIS KIT CONTAINS A RESTRICTED ARTICLE THAT SHIPS SEPARATELYFROM REST OF THE KIT OUT OF WICHITA YOU WILL NEED TO ORDER EARLY IN THEMORNING TO HAVE THE BEST CHANCE FOR BOTH SALINA AND WICHITA TO SHIP THESAME DAY.

NOTENOTENOTENOTE:::: WILL NEED 080X2.63X5.88 PIECE OF "2024-T3AL" TO MAKE DOUBLER FOR USE WITH THISKIT IF NOT IN YOUR SHOP STOCK, NEED TO PROCURE LOCALLY.

WT. CHANGE : WT: 2.5 LBS; MOMENT: 315 IN. LBS (INCREASE)EST. MAN/HRS: : 3MEN : 1 (MAN)

99-5023-5FIRE EXTINGUISHER *RESTRICTED ARTICLE* - SPARES ATA :C99 U-50, U-165 THRU U-230THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE 344T FIREEXTINGUISHER LOCATED ON THE LH AFT CABIN CHAIR WITH AN "AMEREX" PART NUMBER 352TS FIREEXTINGUISHER ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: WILL NEED 080X2.63X5.88 PIECE OF "2024-T3AL" TO MAKE DOUBLER FOR USE WITH THISKIT IF NOT IN YOUR SHOP STOCK, NEED TO PROCURE LOCALLY.

NOTENOTENOTENOTE:::: *RA* MEANS THIS KIT CONTAINS A RESTRICTED ARTICLE THAT SHIPS SEPARATELYFROM REST OF THE KIT OUT OF WICHITA. YOU WILL NEED TO ORDER EARLY IN THEMORNING TO HAVE THE BEST CHANCE FOR BOTH SALINA AND WICHITA TO SHIP THESAME DAY.

WT. CHANGE : WT: 2.5 LBS; MOMENT: 682 IN. IBS (INCREASE)EST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)


KIT CATALOG

99-5023-7FIRE EXTINGUISHER *RESTRICTED ARTICLE* - SPARES ATA :C99 U-50, U-165 THRU U-230THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE 344T FIREEXTINGUISHER LOCATED ON THE LH AFT CABIN CHAIR WITH A "GENERAL" GH-2-1/2J FIRE EXTINGUISHERON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: *RA* MEANS THIS KIT CONTAINS A RESTRICTED ARTICLE THAT SHIPS SEPARATELYFROM THE REST OF THE KIT OUT OF WICHITA. YOU WILL NEED TO ORDER EARLY IN THEMORNING TO HAVE BEST CHANCE FOR BOTH SALINA AND WICHITA TO SHIP THE SAMEDAY.

NOTENOTENOTENOTE:::: WILL NEED O8OX2 63X5 88 PIECE OF "2024-T3-AL "TO MAKE DOUBLER FOR USE WITHTHIS KIT IF NOT IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY

WT. CHANGE : WT: 2.5 LBS; MOMENT 682 IN. LBS (INCREASE)EST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

99-5024-1AIR CONDITIONING RELIEF VALVE INSTALLATION ATA :C99 U-50, U-165 THRU U-224THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AIR CONDITIONING SYSTEM RELIEF VALVEASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

99-5024-3AIR CONDITIONING RELIEF VALVE INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AIR CONDITIONING SYSTEM RELIEF VALVEASSEMBLY FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

99-8008-1 SLANDING GEAR RETRACT BRACKET INSTALLATION ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-151SI NO. 0538-062 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED SUPPORT ASSEMBLY FOR THELANDING GEAR GEARBOX.WT. CHANGE : N/AEST. MAN/HRS: : 16MEN : 1 (MAN)


KIT CATALOG

99-8009-1 SLANDING GEAR GREASE PROVISIONS, MAIN AND NOSE ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-148, U-150

AND U-151SI NO. 0516-200, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL GREASE PROVISIONS ON THE STANDARDMAIN AND NOSE LANDING GEARS.WT. CHANGE : N/AEST. MAN/HRS: : 64MEN : 1 (MAN)

99-8010-1 PLANDING GEAR INSTALLATION, HYDRAULIC ATA :99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-153THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMPLETE HYDRAULIC LANDING GEARSYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : 250MEN : 1 (MAN)

99-8018-399-8018-3 ACTUATOR INSTALLATION,HYDRAULIC LANDING GEAR ATA :99,A99,A99A & B99: U-1 THRU U-164 EXCEPT FOR U-50 A/C,

EQUIPPED WITH HYDRAULIC LANDINGGEAR.

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR INSTALLING A 99-820123-3 HYDRAULICNOSE ACTUATOR AS SPARE REPLACEMENT FOR THE 99-388000-1 ACTUATOR ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MS20426AD3" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.


99-8019-1 SLANDING GEAR HYDRAULIC POWER PACK - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 99-388002 3 POWER PACK AS A SPARESREPLACEMENT FOR THE 99-388002 1 POWER PACK.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8019-3 SLANDING GEAR HYDRAULIC POWER PACK - SPARES ATA :C99 U-50, U-165 THRU U-253THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 99-388002-11 POWER PACK AND A99-388007-1 LIQUID LEVEL SENSOR AS SPARES REPLACEMENTS FOR THE 99-388002-5 POWER PACK AND20625-2 LIQUID LEVEL SENSOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-8020-1 PBRAKE DEICE INSTALLATION, STANDARD LANDING GEAR ATA :C99 U-50, U-165 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMPLETE BRAKE DEICE SYSTEM.WT. CHANGE : WT: 23.4 LBS @ 208.3 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8020-3 PBRAKE DEICE INSTALLATION, HIGH FLOTATION LANDING GEAR ATA :C99 U-50, U-165 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMPLETE BRAKE DEICE SYSTEM.WT. CHANGE : WT: 20.9 LBS @ 208 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8022-1 SLANDING GEAR INSPECTION AND COMPONENT INSTALLATION, NOSE ATA :99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSPECT THE NOSE LANDING GEAR ASSEMBLY ANDREPLACE VARIOUS COMPONENTS AT EACH 7500 CYCLE INTERVAL REPLACEMENT OF THE REMAININGCOMPONENTS, ON CONDITION, AT EACH 7500 CYCLE INTERVALS AND EVERY SUBSEQUENT 1500 CYCLWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8023-1 SLANDING GEAR INSPECTION AND COMPONENT INSTALLATION,STANDARD MAIN

ATA :

99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSPECT THE MAIN LANDING GEAR ASSEMBLY ANDREPLACE VARIOUS COMPONENTS AT EACH 7,500 CYCLE INTERVAL REPLACEMENT OF THE REMAININGCOMPONENTS, ON CONDITION, AT EACH 7,500 CYCLE INTERVALS AND EVERY SUBSEQUENT 1,500 CWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8024-1 SLANDING GEAR INSPECTION AND COMPONENT INSTALLATION, HIGHFLOTATION MAIN

ATA :

99, 99A, A99A, B99, C99 U-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSPECT THE MAIN LANDING GEAR ASSEMBLY ANDREPLACE VARIOUS COMPONENTS AT EACH 7,500 CYCLE INTERVAL. REPLACEMENT OF THE REMAININGCOMPONENTS, ON CONDITION, AT EACH 7,500 CYCLE INTERVALS AND EVERY SUBSEQUENT 1,500WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-8025-3 SSERVICE VALVE RETAINER ATA :99, 99A, A99A, B99SB NO. 2023 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL A SAFETY WIRE TO AIRCRAFT WITHHYDRAULIC LANDING GEAR.WT. CHANGE : N/AEST. MAN/HRS: : 2.5MEN : 1 (MAN)

99-8025-5 SSERVICE VALVE RETAINER AND HAT SECTION ATA :C99 U-50, U-165 THRU U-238SB NO. 2023 OR SUBSEQUENTTHIS KIT CONTAINS PARTS AND INFORMATION TO INSTALL SAFETY WIRE TO LANDING GEAR VALVE ANDINSTALL HAT SECTION IN CABIN FLOORBOARD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

99-8026-1 SLANDING GEAR ACTUATOR SEALS, HYDRAULIC MAIN - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES SEALS FOR THE HYDRAULIC MAIN LANDING GEAR ACTUATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8026-11 SLANDING GEAR ACTUATOR SEALS, HYDRAULIC NOSE - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES SEALS FOR THE HYDRAULIC NOSE LANDING GEAR ACTUATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8026-3 SLANDING GEAR ACCUMULATOR SEALS, HYDRAULIC - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES SEALS FOR THE HYDRAULIC LANDING GEAR ACCUMULATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

99-8026-5 SLANDING GEAR SERVICE VALVE SEALS, HYDRAULIC - SPARES ATA :99,99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES SEALS FOR THE HYDRAULIC LANDING GEAR SERVICE VALVE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8026-7 SLANDING GEAR POWER PACK SEALS, HYDRAULIC - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES SEALS FOR THE HYDRAULIC LANDING GEAR POWER PACK.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-8026-9 SLANDING GEAR HAND PUMP SEALS, HYDRAULIC - SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES SEALS FOR THE HYDRAULIC LANDING GEAR HAND PUMP.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-9003- PCABIN AUXILIARY HEAT ATA :99 U-1 THRU U-35, U-37 THRU U-49, U-51 THRU

U-79, U-86 THRU U-88, U-90 THRU U-92,U-94, U-95, U-98 THRU U-100, U-102, U-103,U-106 THRU U-109, U-114, U-119 THRUU-122, U-124, U-136

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AUXILIARY CABIN HEATING SYSTEM ONAIRPLANES WITH PT6A-20 ENGINES.WT. CHANGE : WT: 28 LBS @ 143 ARMEST. MAN/HRS: : 80MEN : 1 (MAN)

99-9003-3 PCABIN AUXILIARY HEAT ATA :99A, A99A, B99 U-36, U-80 THRU U-85, U-89, U-93, U-96,

U-97, U-101, U-104, U-105, U-110 THRUU-113, U-115 THRU U-118, U-123, U-125THRU U-135, U-137 THRU U-164

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AUXILIARY CABIN HEATING SYSTEM ONAIRPLANES WITH PT6A-27 ENGINES.WT. CHANGE : WT: 28 LBS @ 143 ARMEST. MAN/HRS: : 80MEN : 1 (MAN)


KIT CATALOG

99-9011-1 SOIL LINE HOSE ASSEMBLY- SPARES ATA :99, 99A, A99A, B99 U-80 THRU U-164THIS KIT PROVIDES A SPARES REPLACEMENT FOR THE 130F006-12D-0220-180, 156F115-180 OR 41-F11180-12D-0220 OIL-LINE HOSE ASSEMBLIES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

99-9012-1 SHEATER, POWER CONTROL CABLE ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164SI NO. 0863-159 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HEATER ON THE ENGINE POWER CONTROLCABLE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

99-9014-1 SFUEL CHECK VALVE- SPARES ATA :99, 99A, A99A, B99 U-1 THRU U-49, U-51 THRU U-164THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 101-389011-57 CHECK VALVE AS A SPARESREPLACEMENT FOR THE 99-389013 CHECK VALVE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-9015-1 PWATER MENTHANOL INJECTION SYSTEM INSTALLATION ATA :C99 U-50, U-165 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A WATER METHANOL INJECTION SYSTEM.WT. CHANGE : WT: 59 LBS @ 166.8 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

99-9017-5 SPROPELLER, IMPROVED SEAL DRAIN ATA :C99 U-50, U-165 THRU U-238"OPTIONAL" SB NO 2087, REV. 1 AND SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION TO INSTALL LARGER DRAIN LINE FOR FLOWDISCHARGE TO COM OVERBOARD BREATHER MANIFOLD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

99-9018-1PROPELLER, IMPROVED SEAL DRAIN ATA :ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE MODEL P-5 POLY-PLANAR SPEAKER WITHQUAM 4C3Z8FR SPEAKER ON ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberBULKHEAD CONNECTOR CHANGE (SPARE FOR 207201-1 AND 207200-1) - (101-3202-1) 1




CHART HOLDER, BEECHCRAFT CONTROL WHEEL, 720 SERIES - (101-5039-1 P) 1



CLOCK INSTALLATION, CONTROL WHEEL - (101-5137-1) 2

CONTROL WHEEL REPLACEMENT AND BUILD UP - SPARES - (101-5156-1 S) 2









HYDRAULIC OIL LINE REPAIR - (101-8023-1) 4

OPERATION PER FAR PART 121 - INFORMATION ONLY - (114-0001-1) 5

INCREASE GROSS WEIGHT - (114-0002-3) 5

CARGO CONFIGURATION (PERMANENT CHANGE) - (114-0100-1) 5



FUEL TOTALIZER INSTL - (114-3001-1) 6

POWER DC DISTRIBUTION PANEL, FASTENER INSTALLATION - (114-3002-1 S) 6

ANNUNCIATOR DELAY, ENVIRONMENTAL SYSTEM - (114-3003-1 S) 6

FIRE EXTINGUISHER/DETECTOR SWITCH, ENGINE - (114-3004-1 S) 6

INVERTER COOLING FAN - (114-3006-1 S) 7

INVERTER RELOCATION, PC-17 - (114-3006-3 S) 7

FLIGHT DATA RECORDER - (114-3007-1 S) 7

FLIGHT DATA RECORDER INSTALLATION - (114-3007-3 S) 8

VOICE RECORDER INSTALLATION - (114-3008-1 S) 8

HIGH SPEED WARNING INSTALLATION - (114-3009-1 S) 8

HIGH SPEED WARNING INSTALLATION - (114-3009-3 S) 8

POWER STEERING WIRING MODIFICATION - (114-3010-1 S) 9

EMERGENCY LOCATOR TRANSMITTER, IMPROVED REMOTE SWITCH - (114-3011-1 S) 9

FLAP SWITCH BY-PASS - (114-3012-1 S) 9



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberINDICATOR LIGHT INSTALLATION, LANDING GEAR POSITION - (114-3013-1 S) 9

GYRO, DC INSTALLATION - (114-3014-1 S) 10

GYRO, DC INSTALLATION - (114-3014-3 S) 10

SIGN INSTALLATION, NO SMOKE/FASTEN SEAT BELT - (114-3015-1 S) 10

POWER STEERING, DECOTO, FAILURE ANNUNCIATION ACCESS IMPROVEMENT - (114-3016-1 S) 10

ANTENNA INSTALLATION, MARKER BEACON - (114-3017-1 S) 11

POWER STEERING ACTUATOR HARNESS - (114-3018-1) 11

CONTROL SWITCH, VAPOR CYCLE AIR CONDITIONER - (114-3019-1 S) 11

COCKPIT VOICE RECORDER INSTALLATION - (114-3020-1 S) 11






WIRE HARNESS SUPPORT, UPPER AFT NACELLE - (114-3021-1 S) 13

FLIGHT DATA RECORDER INSTALLATION - (114-3022-1 S) 13

FLAP BIAS SENSING - (114-3023-1) 13

FDR ACCELEROMETER RELOCATION MODIFICATION - (114-3024-1 M) 13

TURN AND BANK INDICATOR INSTALLATION - (114-3026-1 S) 14

ENVIRONMENTAL PROTECTION IMPROVEMENT, FUEL QUANTITY SYSTEM - (114-3027-1 S) 14

CIRCUIT BREAKER PANEL ASSEMBLY ATTACHMENT - (114-3028-1 S) 14

STATIC DISCHARGER INSTL - (114-3029-1) 14

PRESSURIZATION CONTROL DIAL ILLUMINATION - (114-3030-1 S) 15

HOT MIKE CVR MODIFICATION - (114-3032-1 S) 15

HOT MIKE CVR MODIFICATION - (114-3033-1 S) 15

STATIC DISCHARGER INSTALLATION - (114-3034-1 S) 15

GPWS REWORK PROVISIONING INSTALLATION - (114-3035-1) 16

LANDING GEAR MOTOR CIRCUIT BREAKER PANEL MOD - (114-3036-1) 16

INSTALLATION COCKPIT SPEAKER SILENCE - (114-3037-1) 16

ELECTRICAL INSTALLATION CARGO CONFIGURATION - (114-3038-1) 16

GPS SYSTEM INSTALLATION - (114-3039-1) 17

TCAS SYSTEM INSTALLATION - (114-3040-1) 17

CVR SYSTEM INSTALLATION - (114-3041-1) 17

FDR SYSTEM INSTALLATION - (114-3042-1) 17

STATIC DISCHARGER INSTALLATION - INFORMATION ONLY - (114-3043-1) 17


LANDING GEAR MOTOR CIRCUIT BREAKER - (114-3049-1) 18



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberKIT-INSTL, ARTEX C406-2 ELT - (114-3050-)

18

CHIP DETECTOR CONNECTOR - (114-3610-1) 18

PULLEY BRACKET INSTL - (114-4001-1) 19

AIRSTAIR DOOR STEP INSTALLATION - (114-4002-1 S) 19

RAMP INSTALLATION, SPAR - (114-4003-1 S) 19

ANTENNA, UPPER AFT COMMUNICATION - (114-4004-1 S) 19

ANTENNA, LOWER AFT COMMUNICATION - (114-4005-1 S) 20

ICE LIGHT BRACKET - (114-4006-1 S) 20

CARGO DOOR, CLOSURE AID STOWAGE LATCH - (114-4007-1 S) 20

AMBIENT AIR INTAKE, LOWER LEFT HAND WING LEADING EDGE - (114-4009-1 S) 20

FLAP BUMPER - (114-4010-1 S) 21

FLAP SWITCH COMPARTMENT SEAL - (114-4011-1 S) 21

FLAP SWITCH LINK - (114-4012-1 S) 21

AERODYNAMIC CONFIGURATION - (114-4013-1 S) 21

VORTEX GENERATOR INSTALLATION - (114-4014-1 S) 22

FILLET INSTALLATION, WING AND FUSELAGE - (114-4015-1 S) 22

STABILON FAIRING - (114-4016-1 S) 22

VOICE AND FLIGHT DATA RECORDER SUPPORT STRUCTURE - (114-4017-1 S) 22

FENCE INSTALLATION, INBOARD WING - (114-4018-1 S) 23

LANDING GEAR CENTERING SWITCH, NOSE - (114-4019-1 S) 23

GERMAN CERTIFICATION - (114-4020-1) 23



SPAR RAMP INSTALLATION - (114-4025-1 S) 24

LANDING LIGHT BULB REPLACEMENT INSTALLATION (LH) - (114-4026-1 S) 24

LANDING LIGHT BULB REPLACEMENT INSTALLATION (RH) - (114-4026-2 S) 24

LANDING LIGHT SUPPORT BRACKET CHANGE (LH) - (114-4026-3 S) 24

LANDING LIGHT SUPPORT BRACKET CHANGE (RH) - (114-4026-4 S) 25

DEICE BOOT REINFORCEMENT - (114-4027-1 S) 25

REINFORCEMENT, COMM ANTENNA - (114-4028-1 S) 25

HANDRAIL, ADJUSTABLE INSTALLATION - (114-4030-1 S) 25

AIRSTAIR DOOR - SPARES - (114-4031-1 S) 26

DAMPER ATTACHMENT BRACKET, AIRSTAIR DOOR - (114-4032-1 S) 26

SEAL INSTALLATION AIRSTAIR DOOR - (114-4033-1 S) 26

LANDING LIGHT, HALOGEN LAMP - (114-4034-1 S) 26

GRAVEL RUNWAY PROTECTION INSTALLATION - (114-4035-1 P) 27

GRAVEL RUNWAY LANDING OPTION INSTALLATION - (114-4035-3 P) 27



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberRADOME ABRASION BOOT INSTALLATION - (114-4036-1 S) 27

UPPER WING SKIN REPAIR - (114-4037-1) 27

WING SPAR INSPECTION ACCESS - (114-4038-1 S) 28

SPAR CAP REINFORCEMENT, REAR - (114-4039-1 S) 28

STORM WINDOW SEAL INSTALLATION - (114-4040-1 S) 28

SPAR CAP REINFORCEMENT, REAR - (114-4041-1 S) 28

FLAP RIB REPLACEMENT - (114-4042-1 S) 29

SEAT TRACK REPLACEMENT - (114-4044-1 S) 29

SEAT TRACK REPLACEMENT - (114-4044-3 S) 29

SEAT TRACK REPAIR, OUTBD - (114-4045-1 S) 29

BAGGAGE AFT COMPARTMENT SUPPORT - (114-4046-1 S) 29

BAGGAGE AFT COMPARTMENT SUPPORT - (114-4046-3 S) 30

DAMPENER SUPPORT INSTALLATION, AIRSTAIR DOOR - (114-4047-1 S) 30

COMM ANTENNA, LOWER AFT, REINFORCEMENT INSTALLATION - (114-4048-1) 30

CARGO NET INSTALLATION - (114-4049-1) 30

FLOORBOARD INSTALLATION CARGO - (114-4050-1) 31

RIB ASSEMBLY REINFORCEMENT - (114-4051-1) 31

COLD EXPANSION OF HOLES - (114-4052-1) 31

COLD EXPANSION OF HOLES - INFORMATION ONLY - (114-4053-1) 31

STATIC WICK REMOVAL, STABILION - (114-4054-1) 32

EROSION STRIP INSTALLATION, SURFACE DEICE - (114-4055-1) 32

EROSION STRIP INSTALLATION, SURFACE DEICE - (114-4056-1) 32

SIDE SEAT TRACK REPLACEMENT, INBOARD HALF - INFORMATION ONLY - (114-4057-1) 32

SIDE SEAT TRACK REPLACEMENT, INBOARD HALF - INFORMATION ONLY - (114-4057-3) 33

SIDE SEAT TRACK REPLACEMENT, INBOARD HALF - (114-4058-1) 33

SPAR CAP CHAFING BLOCK INSTALLATION - INFORMATION ONLY - (114-4059-1) 33

EMPENNAGE INSPECTION PANELS, INFO ONLY - (114-4060-0001) 33

EMPENNAGE INSPECTION PANELS, INFORMATION ONLY - (114-4060-1) 34

INBOARD FLAP SKIN IMPROVEMENT - (114-4063-0001) 34



COLD EXPANSION OF FASTERNER HOLES IN REAR SPAR - (114-4067-0001) 35

WINDOW INSTALLATION CABIN - (114-4300-1) 35

COMBINATION PASSENGER/CARGO CONFIGURATION MODIFICATION - (114-5000-1 P) 36

OXYGEN SYSTEM, CABIN - (114-5001-1 P) 36

COWLING AIR INLET REINFORCEMENT, ENGINE - (114-5002-1 S) 36

BRAKE DEICE INSTALLATION - (114-5003-1) 36



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberELEVATOR CONTROL CABLE CLEARANCE CUTOUT - (114-5004-1 S) 36

LANDING GEAR CONTROL SWITCH INSTALLATION - SPARES - (114-5005-1 S) 37

DIFFERENTIAL PRESSURE AND STATIC PLUMBING - (114-5006-1 S) 37

SCUFF COVER, NOSE BAGGAGE COMPARTMENT - (114-5007-1 P) 37


CHAIR ADJUST CABLES, CREW - (114-5009-1 S) 38

CARGO DOOR HANDLE COVER INSTALLATION - (114-5010-1 S) 38

AIR CONDITIONER COMPRESSOR MOUNTING BRACKET - (114-5011-1 S) 38

AILERON TAB CABLE FAIRLEAD - (114-5012-1 S) 38

PRESSURIZATION SENSE LINE DRAIN - (114-5014-1 S) 39

DOWN LOCK PIN INSTALLATION - (114-5015-1 S) 39

FILTER INSTALLATION, ENVIRONMENTAL PLUMBING, WING - (114-5016-1 S) 39

FILTER ENVIRONMENTAL PLUMBING - (114-5016-3 S) 39

FILTER ENVIRONMENTAL PLUMBING - (114-5016-7 S) 40

INLET GUARD INSTALLATION, BLOWER - (114-5017-1 S) 40

ENVIRONMENTAL PLUMBING, LH WING - (114-5018-1 S) 40

ENVIRONMENTAL PLUMBING, LH WING - (114-5018-3 S) 40

MANUAL STEERING INSTALLATION, NOSE LANDING GEAR - (114-5019-1 S) 41


PLACARD, LIMITATION INSTALLATION - (114-5021-1 P) 41

CABIN SEAT, BACKREST STOP INSTALLATION - (114-5022-1 S) 41

SWITCH INSTALLATION, ASYMMETRICAL FLAP - (114-5023-1 S) 42

DUCT INSTALLATION, AIR CYCLE MACHINE - (114-5024-1 S) 42

DEFLECTOR INSTALLATION, CONDENSER SECTION - (114-5025-1 S) 42

PLACARD, ESCAPE ROUTE - (114-5027-1) 42

MANUAL STEERING INSTL, NOSE GEAR - (114-5028-1) 43


MANUAL STEERING INSTALLATION - (114-5029-3 S) 43

EXHAUST LOUVER AND DEFLECTOR INSTALLATION, CONDENSER SECTION - (114-5030-1 S) 43

BRAKE, HYDRAULIC PLUMBING INSTALLATION - (114-5032-1 S) 44

BAGGAGE WEB INSTALLATION FORWARD FULL HEIGHT - (114-5033-1 S) 44

BAGGAGE WEB INSTALLATION, FORWARD FULL HEIGHT WITH PLACARD - (114-5033-3 S) 44

CARGO DOOR RAIN GUTTER INSTALLATION - (114-5034-1 S) 44

DRAIN PROVISION, INSTRUMENT AIR VALVE - (114-5036-1 S) 45

PRESSURE REGULATOR/SHUTOFF VALVE - SPARES - (114-5037-1 S) 45

PRESSURE REGULATOR/SHUTOFF VALVE - SPARES - (114-5037-3 S) 45

GUARD INSTALLATION, PRESSURIZATION CONTROLLER - (114-5038-1 S) 46



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberAIR CREW EYE AND RESPIRATORY PROT PROVISIONS INSTL - (114-5040-1) 46

PILOT ONLY OPERATION, DO NOT OCCUPY SEAT - (114-5042-1 S) 46

PILOT ONLY OPERATION, DO NOT OCCUPY SEAT - (114-5042-3 S) 47

WINDSHIELD LH, KING AIR METAL RETAINER STYLE - (114-5043-1 S) 47

WINDSHIELD RH, KING AIR METAL RETAINER STYLE INSTALLATION - (114-5043-2 S) 48

CARGO CONFIGURATION MODIFICATION - (114-5044-1 P) 48

CARGO CONFIGURATION AND ZERO FUEL WEIGHT - (114-5044-3 P) 48




ZERO FUEL, 15,000 POUNDS MAXIMUM WEIGHT INSTALLATION - (114-5045-1 S) 50




SCREEN, AIR CONDITIONER CONDENSER SECTION - (114-5046-1) 51

INTERIOR LINER INSTALLATION - (114-5047-1) 51

SINGLE PASSENGER SEAT INSTALLATION - (114-5048-1) 51

EXTERIOR MARKING PLACARD - (114-5050-1) 52


A/C OVER PRESSURE SWITCH, SPARES - (114-5053-1) 52

BATTERY VALVE - INFORMATION ONLY - (114-5054-1) 52

OXYGEN MASK & MIC INSTALLATION - (114-5056-1) 53

SWITCH & COVER INSTALLATION - ASYMMETRICAL FLAP - (114-5057-1) 53

UNIVERSAL JOINT REPLACEMENT, ELEVATOR TRIM CONTROL, ELECTRICAL - (114-5058-0001)

53

FIRST AID INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM - (114-5300-1) 54

JAR-OPS CRASH AXE INSTALLATION - (114-5302-1) 54

FIRE EXTINGUISHER INSTALLATION, CABIN - (114-5310-1) 54

FLASHLIGHT INSTALLATION - (114-5311-1) 54

EMERGENCY EXIT LIGHT - (114-5312-1) 55

EMERGENCY EXIT LIGHT - (114-5312-3) 55

EMERGENCY EXIT LIGHT, JAR-OPS - (114-5313-3) 55

HARNESS INSTALLATION-SHOULDER, PILOT AND CO-PILOT - (114-5314-0001) 55



DUCT INSTALLATION, HEAT AND VENT AFT CABIN - (114-5500-1) 56

OXYGEN SYSTEM INSTALLATION CARGO - (114-5600-1) 56

POWER STEERING ACTUATOR - SPARES - (114-8004-1 S) 56



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberLANDING GEAR INDICATOR SWITCH - (114-8005-1 S) 57

POWER STEERING RELIEF VALVE - (114-8006-1 S) 57

MAIN LANDING GEAR DOOR HINGE INSTALLATION - (114-8010-1 S) 57

POWER STEERING POTENTIOMETER - (114-8011-1 S) 57

NOSE GEAR LINK INSTALLATION - (114-8013-1 S) 58

PLACARD INSTALLATION, LANDING GEAR ACCUMULATOR - (114-8014-1 S) 58

NOSE LANDING GEAR INSTALLATION - SPARES - (114-8015-1 S) 58

ANTI-SKID BRAKE PUMP MOTOR INSTALLATION - SPARES - (114-8017-1 S) 58

MAIN LANDING GEAR DOOR HINGE INSTALLATION - (114-8018-1 S) 59

POWER STEERING BELLCRANK LUBRICATION FITTING, INSTALLATION - (114-8019-1 S) 59

ANTI SKID BRAKE PROVISIONS - (114-8020-1) 59

HYDRAULIC FILTER INSTALLATION POWER STEERING - (114-8021-1 S) 59

LANDING GEAR, HYDRAULIC LINE FILTER INSTALLATION - (114-8022-1 S) 60

POWER STEERING PUMP MOTOR ASSEMBLY - (114-8023-1 S) 60

POWER STEERING PUMP MOTOR ASSEMBLY - (114-8023-3 S) 60

GUARD ASSEMBLY, NOSE WHEEL - (114-8025-1 S) 60

NOSE LANDING GEAR BUSHING - (114-8026-1 S) 61

BRAKE ANTI-SKID INSTALLATION FOR AIRCRAFT WITHOUT POWER STEERING - (114-8028-1) 61

BRAKE ANTI-SKID INSTALLATION FOR AIRCRAFT WITH POWER STEERING - (114-8028-3) 61

BRAKE ASSEMBLY - (114-8029-1) 62

WHEEL & BRAKE ASSY - (114-8030-1) 62

QUICK ENGINE CHANGE, PT6A-65B FOR LH ENGINE (WITH ENGINE) - (114-9001-1 S) 62

AIR CONDITIONING COMPRESSOR MOUNTING PROVISIONS - (114-9001-3 S) 63

QUICK ENGINE CHANGE, PT6A-65B - (114-9001-5 S) 63

QUICK ENGINE CHANGE, PT6A-65B, LESS ENGINE - (114-9001-7 S) 63


COWLING REINFORCEMENT, ENGINE - (114-9003-1 S) 64

COWLING REINFORCEMENT, ENGINE - (114-9003-3 S) 64

COWLING GUIDE PIN, FORWARD - (114-9004-1 S) 64

AIR INLET ANTI-ICE DUCT - (114-9005-1) 64

OIL VENT PLUMBING RELOCATION - (114-9006-1 S) 64

AIR SCOOP ADAPTER AND IGNITION EXCITER - (114-9007-1 S) 65

INERTIAL SEPARATOR VANE, AIR INLET - (114-9008-1) 65

SYNCHROPHASER CONTROL BOX - (114-9009-1 S) 65

FIRE DETECTION, ENGINE - (114-9010-1 S) 65

COWLING GUIDE PIN AND AFT LATCH, MID - (114-9011-1 S) 66




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFUEL PRESSURE SWITCH TUBING INSTALLATION - (114-9015-1 S) 66

COWLING INSTALLATION, LEFT ENGINE - (114-9016-1 P) 66

COWLING INSTALLATION, RIGHT ENGINE - (114-9016-3 P) 66

COWLING INSTALLATION (LH AND RH) - (114-9016-5 P) 67

COWLING INSTL, INSTRUCTIONS - (114-9017-1) 67

COWLING REPAIR - (114-9018-1 P) 67

QUICK ENGINE CHANGE-WET WING PT6A-65B WITH LH ENGINE - (114-9019-1 S) 67

QUICK ENGINE CHANGE FOR RH INSTALLATION OF -1 KITTED ENGINE - (114-9019-3 S) 67

QUICK ENGINE CHANGE PT6A-65B WET WING 1900C-1 WITHOUT LH ENGINE - (114-9019-5 S) 68

ICE AND RAIN PROTECTION - (114-9020-1 S) 68

TUBE BREAKAGE WARNING INSTALLATION, BLEED AIR - (114-9021-1 S) 68

BRAKE DEICE MODIFICATION - (114-9022-1 S) 69

DEICE BRUSH BLOCK RELOCATION - (114-9023-1 S) 69

INLET DUCT REINFORCEMENT - (114-9024-1 S) 69

FUEL FIREWALL SHUTOFF VALVE REPLACEMENT - (114-9025-1 S) 69

FUEL FLOW INDICATOR TOTALIZER SYSTEM INSTALLATION - (114-9026-3 S) 70

FUEL FLOW INDICATOR SYSTEM INSTALLATION - (114-9026-5 S) 70

FUEL TOTALIZER INDICATOR SYSTEM INSTALLATION - (114-9026-7 S) 70

FLEX HOSE ASSEMBLY, ENGINE - (114-9027-1 S) 70

ENGINE TRUSS SUPPORT ASSEMBLY - (114-9028-1 S) 71

LANDING GEAR DOOR HINGE - (114-9029-1 S) 71

ENGINE COWLING MODIFICATION - (114-9030-1 S) 71

PLACARD INSTRUCTIONS, FUEL TANK - (114-9031-1 S) 71

DYNAMIC PROPELLER BALANCING PROVISIONS - (114-9032-1 S) 72



ENGINE TRUSS ASSEMBLY - (114-9033-1 S) 73

STARTER GENERATOR REPLACEMENT - (114-9034-1 S) 73

PROPELLER DYNAMIC BALANCING - (114-9035-1 S) 74

ENGINE TRUSS INSTALLATION - SPARES - (114-9036-1 S) 74

ENGINE TRUSS INSTALLATION - SPARES - (114-9036-3 S) 74

TURBINE AND PROP RPM INDICATOR CHANGE INSTALLATION - (114-9037-1 S) 75

ENGINE INSTRUMENT AIR MODIFICATION - (114-9038-1 S) 75







Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberPROP BALANCER, 8500C ANALYZER SYSTEM - (114-9040-1 S) 76

PROP BALANCER, 192A ANALYZER SYSTEM - (114-9040-3 S) 77

PNEUMATIC SYSTEM HEATERS - (114-9041-1 S) 77

PNEUMATIC SYSTEM HEATERS - (114-9041-3 S) 77

TORQUE TRANSMITTER INSTALLATION - SPARES - (114-9042-1 S) 77

HEATERS ELECTRIC PNEUMATIC SYSTEM - (114-9043-1 S) 78

HEATERS ELECTRIC PNEUMATIC SYSTEM - (114-9043-3 S) 78

PROP DEICE HEAVY DUTY BRUSH BLOCK INSTALLATION WITH IMPROVED SLIP RING - (114-9044-1 S) 78

BRUSH BLOCK, HEAVY DUTY, PROP DEICE LESS SLIP RING - (114-9044-3 S) 79

ENGINE TRUSS REPLACEMENT WITH -93 BLEED AIR DUCT - (114-9045-1) 79

ENGINE TRUSS REPLACEMENT 1900, 1900C AIRCRAFT WITHOUT -93 B/A DUCT - (114-9045-3) 79

ENGINE TRUSS REPLACEMENT 1900, 1900C AIRCRAFT WITH 114-9036 - (114-9045-5) 80

FORMER INSTALLATION, LOWER AFT NACELLE - (114-9046-1) 80

PROPELLER SYNCHROPHASER DEACTIVATION - (114-9047-1) 80

EXTERIOR MARKING INSTALLATION - (118-0000-1) 81


RELOCATE AUTOPILOT ELECTRICAL POWER SUPPLY - (118-3001-1 S) 81

ALTIMETER INSTL - (118-3002-1) 82

GROUND COLLISION AVOIDANCE SYSTEM - (118-3003-1) 82

ATTITUDE INDICATOR INSTALLATION, STANDBY GYRO WITH BATTERY PACK - (118-3004-1 M) 82

WING CENTER SECTION RH AFT RIB, CABLE MOD - (118-4010-1) 82

INSPECTION PROVISIONS, MAIN SPAR, LOWER CENTER SECTION - (118-4011-1) 83

INSTALLATION, COLD EXPANSION OF HOLES - (118-4012-1) 83

INSTALLATION, COLD EXPANSION OF HOLES - (118-4012-3) 83

ROD END INSTALLATION, ASYMETRICAL FLAP - (118-4013-1) 84

INSTALLATION, COLD EXPANSION OF HOLES, WET WING - (118-4014-0003)

84

CREW PROTECTIVE BREATHING PROVISIONS - (118-5000-1) 84


AILERON CABLE INSTL, WING - (118-5001-1) 85

KIT 118-8011-0001 - (118-8011-0001) 85

AIR CONDITIONER INSTALLATION - (118-9000-1 S) 85

AIR CONDITIONER INSTALLATION - (118-9000-3 S) 86

COWLING REPAIR - (118-9001-1 S) 86

COWLING PREVENTATIVE MAINTENANCE - (118-9001-3 S) 86

COWLING MODIFICATION REPAIR INSTALLATION - (118-9001-5 S) 87

COWLING REPAIR 1900D - (118-9001-7 S) 87

PNEUMATIC SYSTEM MODIFICATION - (118-9003-1) 87



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberPNEUMATIC SYSTEM REWORK - (118-9003-3) 88



OPERATION PER FAR PART 121 - INFORMATION ONLY - (129-0012-1) 89

AIRCRAFT OWNERSHIP PLATES - (129-0013-1) 89

AIRCRAFT OWNERSHIP PLATES - (129-0013-3) 89

EFIS-84 STAND BY POWER RELAY MODIFICATION - (129-3000-1 S) 89

TCAS AND GPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) - (129-3001-1 S) 90

GPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) - (129-3001-11 S) 90

TCAS (AVIONICS NOT INCLUDED) - (129-3001-3 S) 90

GPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) - (129-3001-5 S) 91

TCAS AND GPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) - (129-3001-7 S) 91

TCAS HARDWARE ONLY (AVIONICS NOT INCLUDED) - (129-3001-9 S) 91

INSTRUMENT PANEL CLOCK - (129-3003-1) 92

COCKPIT SPEAKER SWITCH - (129-3004-1) 92

PROP DEICE BOOT PROTECTION - (129-3006-1) 92

YAW DAMP SWITCH - (129-3008-1) 92

ARTEX ELT, TSOC91A - (129-3009-1) 93

ARTEX ELT, TSOC91A - (129-3009-3) 93

ARTEX ELT, TSOC91A - (129-3009-5) 93

OVERHEAD PANEL MIC SWITCH - (129-3010-1) 93

COVER ASSEMBLY DC GENERATOR CONTROL UNITS - (129-3011-1) 94

EFIS POWER PANEL - (129-3012-1) 94

BRIEFER RELAY BOX WIRING, INFO ONLY - (129-3013-1) 94

ALTIMETER INSTALLATION - INFORMATION ONLY - (129-3014-1) 94

ALTIMETER INSTALLATION - INFORMATION ONLY - (129-3014-3) 95

REPLACEMENT, ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) COMPUTER-INFORMATIONONLY - (129-3015-1)

95

ELT INSTL, DUAL MODE - (129-3401-1) 95

FDR MODIFICATION, JAA CERTIFICATION - (129-3402-1) 95

CVR INSTL FOR JAR-OPS, INFO ONLY - (129-3403-1) 95

ELT, DUAL MODE - (129-3404-1) 96

WIRE CHAFING INFORMATION ONLY - (129-3621-1) 96

WINDOW CABIN GRAVEL RUNWAY OPTION - (129-4001-1 S) 96

P-STATIC PREVENTION - (129-4002-1 S) 96

P-STATIC PREVENTION - (129-4003-1 S) 97

ICE SHIELD INSTALLATION, ALUMINUM - (129-4004-1 S) 97

BULKHEAD REINFORCEMENT, CANTED FS 588.10 INSTALLATION - (129-4005-1 S) 97



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberAIRSTAIR DOOR HANDRAIL IMPROVEMENT - (129-4006-1) 97

AIRSTAIR DOOR HANDRAIL IMPROVEMENT (129-400033-59) - (129-4007-1) 98

ICE SHIELD LH, REPLACEMENT (KEVLAR ) - (129-4008-1) 98

ICE SHIELD LH, REPLACEMENT (KEVLAR ) - (129-4008-3) 98

ICE SHIELD EXTENSION INSTALLATION, KEVLAR (LH) - (129-4009-1) 99

FUEL BAY REPAIR INSTALLATION - (129-4012-1) 99

FUEL BAY REPAIR INSTALLATION (RH) - (129-4013-1) 99

VENT INSTALLATION STABILON - (129-4014-1) 100




ACCESS DOORS, FUEL BAY - (129-4016-1) 101

ACCESS DOORS, FUEL BAY - (129-4016-19) 101

FUEL LEAK REPAIR - (129-4017-1) 101

FLAP SKIN IMPROVEMENT - (129-4018-1) 102








FLAP COVE, INBOARD, FLAP GAP INCREASE (LH) - (129-4019-1) 104

FLAP COVE, INBOARD, FLAP GAP INCREASE (RH) - (129-4019-2) 104

HANDLE SUPPORT ASSEMBLY AIRSTAIR DOOR - (129-4020-1) 104

EMERGENCY EXIT DOOR SEAL IMPROVEMENTS - INFORMATION ONLY - (129-4022-1) 105

STATIC WICK REMOVAL - INFORMATION ONLY - (129-4023-1) 105

SEAT TRACK COVER INSTL - INFORMATION ONLY - (129-4024-1) 105

SEAT TRACK COVER INSTALLATION INFORMATION - (129-4024-3) 105

INSTALLATION OF CONDENSATION DRAINS - (129-4026-1) 106

BIRD STRIKE PROVISIONS - INFORMATION ONLY - (129-4027-1) 106

RADOME DRAIN INSTALLATION - INFORMATION ONLY - (129-4028-1) 106

DE-ICE BOOT INSTL, FAST BOOT - INFORMATION ONLY - (129-4029-1) 107

FAIRING REPAIR, INFORMATION ONLY - (129-4030-1) 107

RH PROPELLER IMPACT SHIELD INSTALLATION - (129-4031-1) 107

STRUCTURAL PROVISIONING FOR GPS AND VHF ANTENNA - (129-4033-1) 107

STRUCTURAL PROVISIONING FOR GPS AND VHF ANTENNA INSTALLATIONS - (129-4033-3) 108



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberLIGHTER TINTED CABIN WINDOW - (129-4034-1) 108

CABIN HEATING IMPROVEMENT - (129-5000-1 S) 108

BLEED AIR HEATING IMPROVEMENT - (129-5001-1 S) 108

PARTITION PAD, LH FORWARD PARTITION - (129-5004-1 M) 108

CABIN EJECTOR NOISE IMPROVEMENT - (129-5005-1 S) 109

REWORK-BEECHCRAFT MODEL 1900D - (129-5006-1) 109

PARTITION BRACKETRY INSTALLATION - (129-5007-1 S) 109

PARTITION BRACKET COVER INSTALLATION - (129-5008-1 S) 109

REPLACEABLE DETENT PIN, ONE THRUST LEVER INSTALLATION - (129-5009-1) 110

REPLACEABLE DETENT PIN, BOTH THRUST LEVER INSTALLATION - (129-5009-3) 110

STORM WINDOW DRIP TRAY AND PLUMBING INSTALLATION - (129-5010-1) 110

ENVIRONMENTAL PLUMBING INSTALLATION, FILTER ASSEMBLY FOR FOG NOZZLE - (129-5011-1) 111

SPEAKER INSTALLATION, HEADLINER AND SIDEWALL - (129-5016-1) 111

PRESSURIZATION CONTROLLER, GUARD INSTALLATION - (129-5017-1) 111

CREW OXYGEN MASK REPLACEMENT - SPARES - (129-5018-1) 112

PLACARD INSTALLATION, FIRE EXTINGUISHER LOCATION FORWARD PARTITION - (129-5019-1) 112

AIR CONDITIONING REFRIGERANT CHANGE - (129-5020-1) 112

AIR CONDITIONING REFRIGERANT CHANGE - (129-5020-3) 113

AIR CONDITIONING REFRIGERANT AND COMPRESSOR CHANGE - (129-5020-5) 114

PLACARD, EMERGENCY EVACUATION INSTALLATION (FORWARD CABIN PARTITION) - (129-5021-1) 114

SPRAY NOZZLE INSTALLATION, AIR CYCLE MACHINE MOD FOR AIRCRAFT WITHOUT 129-5011-1 INSTALLED -(129-5023-1)

115

SPRAY NOZZLE INSTALLATION, AIR CYCLE MACHINE MOD FOR AIRCRAFT WITH 129-5011-1 INSTALLED -(129-5023-3)

115

AIR CONDITIONING COMPRESSOR - SPARES - (129-5024-1) 115

WINDSHIELD REPLACEMENT FOR THE 114-384020-1 WINDSHIELD - (129-5025-1) 116

WINDSHIELD REPLACEMENT FOR THE 114-384020-2 WINDSHIELD - (129-5025-2) 116

STRUT ASSEMBLY AIRSTAIR DOOR - SPARES - (129-5026-1) 116

SWITCH INSTALLATION, ASYMMETRICAL FLAP - (129-5027-1) 117

SWITCH INSTALLATION, ASYMMETRICAL FLAP - (129-5027-3) 117

BLEED AIR TUBE BREAKAGE WARNING SYSTEM - (129-5029-1) 117


LAVATORY SMOKE DETECTOR INSTALLATION - (129-5031-1) 118





LAVATORY TRASH BIN FIRE EXTINGUISHER, INSTALLATION - (129-5033-1) 120



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCOVER, ELECTRIC ELEVATOR TRIM ACTUATOR - (129-5035-1) 120

PRESSURIZATION CONTROLLER - SPARES - (129-5036-1) 120

SPARES, FLAP ACTUATOR - INFORMATION ONLY - (129-5037-1) 120

GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY - (129-5039-11) 121






FIRE EXTINGUISHER RELOCATION AND INSTALLATION - INFORMATION ONLY - (129-5041-1) 122

SEAT INSTALLATION, LH FWD - INFORMATION ONLY - (129-5042-1) 122

SEAT INSTALLATION, RH FWD - INFORMATION ONLY - (129-5042-3) 122

SEAT INSTALLATION, LH AFT - INFORMATION ONLY - (129-5042-5) 123

SEAT INSTALLATION, RH AFT - INFORMATION ONLY - (129-5042-7) 123

ACTUATOR ASSY & INSTL, ELEVATOR TRIM TAB - (129-5043-1) 123



KIT - MODEL 1900D ZERO FUEL WEIGHT INCREASE (15,700 LBS) - (129-5045-1) 124

FLAP SAFETY SWITCH, GREASE FITTING INSTL - (129-5046-0001) 125

INSTALLATION GROUND FINE SWITCH - (129-5200-1) 125

FIRST AID KIT INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM - (129-5300-1) 125

PLACARD INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM - (129-5301-1) 126

FORWARD PARTITIONS - INFORMATION ONLY - (129-5303-1) 126

FORWARD PARTITIONS - INFORMATION ONLY - (129-5303-3) 126

CRASH AXE INSTL, JAR-OPS - (129-5304-1) 126

FRAME CHAFING - INFORMATION ONLY - (129-5306-1) 127

FLASHLIGHT INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM - (129-5312-1) 127

EMERGENCY EXIT LIGHT, HEADLINER - (129-5313-1) 127

EMERGENCY EXIT LIGHT, JAR-OPS - (129-5314-1) 127

BRAKE ASSEMBLY - (129-8002-1) 128

PISTON & SOCKET SPARES, MAIN LANDING GEAR - (129-8003-1) 128

MAIN LANDING GEAR ID PLATE INSTALLATION - (129-8004-0001) 128

BRAKE ANTI-SKID INSTALLATION, AIRCRAFT WITHOUT POWER STEERING - (129-8100-1) 128

BRAKE ANTI-SKID INSTALLATION, WITH POWER STEERING - (129-8100-3) 129

QUICK ENGINE CHANGE - (129-9001-3) 129

PLACARD, WARNING INSTALLATION - (129-9002-1 S) 129

FREON COMPRESSOR QUIL SHAFT, SERVICE EVALUATION - (129-9004-1) 129



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberEXHAUST PIPE, SERVICE EVALUATION - (129-9005-1) 130

ENGINE TRUSS REPAIR - (129-9006-1) 130

BRUSH BLOCK, HEAVY DUTY, PROP DEICE EVALUATION - (129-9007-1 S) 130

BRUSH BLOCK, HEAVY DUTY, PROP DEICE EVALUATION - (129-9007-3 S) 131

GENERATOR WIRING RUB STRIP, AFT COWLING MODIFICATION - (129-9008-1 S) 131

PROP DEICE HEAVY DUTY BRUSH BLOCK - (129-9009-1 S) 131

PROP DEICE HEAVY DUTY BRUSH BLOCK INSTALLATION - LESS SLIP RINGS - (129-9009-3) 132

PNEUMATIC SYSTEM MODIFICATION INSTALLATION - (129-9010-1) 132

PNEUMATIC SYSTEM MODIFICATION REWORK INSTALLATION - (129-9010-3) 132

GROUND IDLE SYSTEM - (129-9011-1) 133

EXHAUST STACK, RH, 25 DEGREE TILT INSTALLATION - (129-9013-1) 133

ICE VANE INSTALLATION, INLET - (129-9016-1) 133

ENGINE TRUSS REPAIR - (129-9017-1) 134

MEGGITT LCD ENCODING ALTIMETER - (129-9018-1) 134

FIRE LOOP CLAMP - (129-9019-1) 134

PROPROPELLER SHAFT SEAL DRAIN VALVE - (129-9021-1) 134

FIRE DETECTOR REINFORCEMENT - (129-9023-1) 135

PROPELLER DE-ICER - (129-9024-1) 135

PROPELLER DE-ICER - INFORMATION ONLY - (129-9024-3) 135

FUEL PUMP DRAIN - (129-9025-1) 135

FUEL SYSTEM INSTALLATION - (129-9026-1) 136

GROUND IDLE SYSTEM ANNUNCIATION REMOVAL - (129-9030-1) 136

ENGINE EXCITER RELOCATION - (129-9100-1) 136

EXHAUST FLANGE - (129-9500-1) 136

EXHAUST FLANGE - (129-9500-3) 137

EXHAUST FLANGE - (129-9500-5) 137

SURFACE DEICE PRESSURE SWITCH - (129-9700-1) 137

FIED SERVICE KIT - (140-5058-000) 137

EXTERIOR PLACARDS - (23-2001-1 S) 138


FUEL (MINIMUM AND UNUSABLE FUEL) PLACARD - (23-2003-1 S) 138

LEADING EDGE REPLACEMENT, WING RIGHT HAND, BONDED - (23-9-11 S) 138

LEADING EDGE REPLACEMENT, WING LEFT HAND, BONDED - (23-9-5 S) 139

LEADING EDGE REPLACEMENT, WING RIGHT HAND, BONDED - (23-9-7 S) 139

LEADING EDGE REPLACEMENT, WING LEFT HAND, BONDED - (23-9-9 S) 139

FIRE EXTINGUISHER REPLACEMENT "RESTRICTED ARTICLE* - (36-5017-1 S) 139




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCONTROL WHEEL CLOCK INSTALLATION (28-VOLT) - (55-3028-3 P) 140


STABILIZER AND FIN SEALING - (90-4102-1 S) 140


SERVO AMPLIFIER INSTALLATION - SPARES - (99-3038-1 P) 141


KIT CATALOG

101-3202-1BULKHEAD CONNECTOR CHANGE (SPARE FOR 207201-1 AND 207200-1) ATA :1900, 1900C, 1900C-1, 1900DTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE AMP FEED-THRU CONNECTORS, ANDASSOCIATED PLUGS, WITH MIL-SPEC CONNECTORS ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 207200-1 CONNECTOR REPLACEMENT, UE-2 THRU UE-57.NOTENOTENOTENOTE:::: 207201-1 CONNECTOR REPLACEMENT, UC-1, UC-16 THRU UC-69, UD-1 THRU UD-7, AND

UE-2 THRU UE-57.NOTENOTENOTENOTE:::: PRO-SEAL 890 SEALER IS REQUIRED BUT NOT PART OF KIT.


101-3227-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN VHS FORMAT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3227-3ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES AND INFORMATION FOR PROPER ELECTRICAL BONDING TO METALS ONALL NON-COMPOSITE AIRCRAFT. VIDEO IN PAL FORMAT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES FOR PROPER ELECTRICAL BONDING TO METALS ON ALL NON-COMPOSITEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5039-1 PCHART HOLDER, BEECHCRAFT CONTROL WHEEL, 720 SERIES ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CHART HOLDER WHICH ALLOWS ADEQUATENIGHT TIME LIGHTING OF MAPS AND CHARTS WITHOUT INTERFERING WITH THE PILOT'S NIGHT VISION.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 1, FOR ADDITIONAL INFORMATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5 TO 1.5MEN : 1 (MAN)


KIT CATALOG

101-5041-1 SSTRESS FREE WINDSHIELD INSTALLATION ATA :AIRLINER 1900, 1900C, 1900D, 1900C-1(C-12J)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON IN-SERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR BOTH WINDSHIELDS.

NOTENOTENOTENOTE:::: THIS IS THE NEW APPLICABILITY FOR THIS KIT.NOTENOTENOTENOTE:::: PR1440B1/2 6 OZ. K SEALER (6 EACH PER KIT), EC1300L 1/2 PINT, & A400 ADHESIVE (2



101-5041-3 SSTRESS FREE WINDSHIELD INSTALLATION ATA :AIRLINER 1900DTHIS IS THE NEW APPLICABILITY FOR THIS KIT.THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE A STRESS FREE WINDSHIELDINSTALLATION ON IN-SERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FOR ONE WINDSHIELD.


NOTENOTENOTENOTE:::: PR1440B1/2 6 OZ. K SEALER (3 EACH PER KIT), EC1300L 1/2 PINT, & A400 ADHESIVE (1EACH PER KIT) REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY, OR THRU RAPID.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : HAZMAT REMOVED FROM KIT, MUST ORDER SEPARATELY.MEN : 1 (1 KIT PER ENGINE) (MEN)

101-5137-1CLOCK INSTALLATION, CONTROL WHEEL ATA :1900C-1WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

101-5156-1 SCONTROL WHEEL REPLACEMENT AND BUILD UP - SPARES ATA :1900 SERIESTHIS KIT WILL FURNISH A REPLACEMENT CONTROL WHEEL FOR THE 720-042-200, 720-042-203 OR50-524592-( ) WHEEL; 720-1001, 720-1002, 720-1401, 720-1402, 720-4401 OR 720-4402 WHEEL ASSEMBLIES.

NOTENOTENOTENOTE:::: THIS KIT CONTAINS A CONTROL WHEEL ASSEMBLY WITH FINGER GRIPS ANDINSTALLATION DRAWING SHOWING ALL THE OPTIONS AVAILABLE FOR DIFFERENTMODELS. ALL OTHER PARTS SUCH AS PLASTIC PARTS, SWITCHES, COILED CORDCONNECTOR, AND ETC. MUST BE ORDERED SEPARATELY.



KIT CATALOG

101-5171-1COMPRESSOR SERVICE FITTING CHANGE ATA :1900, 1900C, 1900C-1TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICE PORTS MOUNTEDVERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPE COMPRESSORS. (FOR R-12SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5171-17COMPRESSOR SERVICE FITTING CHANGE ATA :1900, 1900C, 1900C-1TO MODIFY EXISTING NON-STEP PORT COMPRESSOR FITTINGS TO BE STEP PORT TYPE COMPRESSORFITTINGS FOR USE WITH NEW LIGHT WEIGHT, FM-TYPE COMPRESSORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5171-3COMPRESSOR SERVICE FITTING CHANGE ATA :1900, 1900C, 1900C-1TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICE PORTS MOUNTEDVERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPE COMPRESSORS. (FOR FR-12SERVICE PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5171-5COMPRESSOR SERVICE FITTING CHANGE ATA :1900, 1900C, 1900C-1TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICE PORTS MOUNTEDVERTICALLY IN THE COMPRESSOR FITTINGS OF HEAVY DUTY, GM-TYPE COMPRESSORS. (FOR R-1134ASYSTEMS PORTS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5171-7COMPRESSOR SERVICE FITTING CHANGE ATA :1900, 1900C, 1900C-1TO PROVIDE A NEW COMPRESSOR FITTINGS INSTALLATION WITH SERVICE PORTS MOUNTEDHORIZONTALLY IN THE FITTINGS MOUNTING PLATE OF GM-TYPE COMPRESSORS. (FOR R-12 SYSTEMSONLY).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

101-5171-9COMPRESSOR SERVICE FITTING CHANGE ATA :1900, 1900C, 1900C-1TO PROVIDE STEP PORT COMPRESSOR FITTINGS INSTALLATION WITH SPARE REPLACEMENT LIGHTWEIGHT, GM-TYPE COMPRESSORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

101-5172-1HUMPSEAL INSTALLATION, WINDSHIELD ATA :ALL KING AIRS AND 1900 EXCEPT FORSOME OLDER 1900 MODELS WHICH DONOT USE THE LATEST WINDSHIELDDESIGN.TO INSTALL PPG KIT (DHS-001-1) ON THE LEFT WINDSHIELD FOR IN-SERVICE AIRCRAFT.




101-5172-2HUMPSEAL INSTALLATION, WINDSHIELD ATA :ALL 1900 EXCEPT FOR SOME OLDER 1900MODELS WHICH DO NOT USE THE LATESTWINDSHIELD DESIGN.TO INSTALL PPG KIT (DHS-001-2) ON THE RIGHT WINDSHIELD FOR IN-SERVICE AIRCRAFT.




101-8023-1HYDRAULIC OIL LINE REPAIR ATA :1900, 1900CWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

114-0001-1OPERATION PER FAR PART 121 - INFORMATION ONLY ATA :19001900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-176"OPTIONAL" SB NO. 2727THIS KIT DRAWING LISTS THE MODIFICATIONS REQUIRED ON THE 1900C (TEN TO NINETEENPASSENGERS) TO CONFIGURE IT FOR OPERATION UNDER 14 CFR PART 121 AS OF MARCH 20, 1997.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-0002-3INCREASE GROSS WEIGHT ATA :1900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION FOR A 1,000 POUND INCREASE IN GROSS WEIGHT FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPLICABLE ICAO PILOT’S OPERATINGHANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT HAS BEENINSTALLED. THIS SUPPLEMENT MAY BE OBTAINED FROM ANY COMPANY AUTHORIZEDOUTLET.


114-0100-1CARGO CONFIGURATION (PERMANENT CHANGE) ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES A LIST OF ALL KITS REQUIRED TO CONVERT A 1900C INTO A CARGO AIRCRAFT,EXCEPT SERIALS EQUIPPED WITH OPTIONAL EMERGENCY LIGHTING OR EXECUTIVE INTERIORS.

NOTENOTENOTENOTE:::: THESE CHANGES ARE NOT INTENDED TO BE REVERSED, IF YOU DESIRE THE ABILITY TOCHANGE OPERATION OF AIRCRAFT FROM TOTAL CARGO BACK TO PASSENGER SERVICEAS WORK LOAD OPERATIONS DEMAND. SEE 114-5044-1 P, -3 P, -5 P, -7 P, OR -9 P KITS.


114-2001-1 SEXTERIOR PLACARD ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE EXTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-2002-1 SINTERIOR PLACARD ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A STANDARD REPLACEMENT SET OFPRESSURE SENSITIVE INTERIOR DECALS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3001-1FUEL TOTALIZER INSTL ATA :1900CWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3002-1 SPOWER DC DISTRIBUTION PANEL, FASTENER INSTALLATION ATA :1900C UB-1 THRU UB-15SB NO. 2089, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THREAD SEALER ON THE DC POWERDISTRIBUTION PANEL CIRCUIT BREAKER AND LOADMASTER SHUNT ATTACHING SCREWS AND TOMAINTAIN HORIZONTAL ALIGNMENT FOR POWER PANEL COMPONENTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

114-3003-1 SANNUNCIATOR DELAY, ENVIRONMENTAL SYSTEM ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-5, UB-7 THRU UB-24, UB-27

THRU UB-31, UB-35, UB-37 THRU UB-51SB NO. 2093 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DELAY IN THE ENVIRONMENTAL SYSTEMWARNING ANNUNCIATOR.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-3004-1 SFIRE EXTINGUISHER/DETECTOR SWITCH, ENGINE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-56SB NO. 2154 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FOUR TOGGLE SWITCHES IN THE PLACE OF AFIRE EXTINGUISHER/DETECTOR ROTARY TYPE SWITCH.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

114-3006-1 SINVERTER COOLING FAN ATA :1900 UA-31900C UB-1 THRU UB-60SB NO. 2164 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL EXTERNAL INVERTER COOLING FANS FORCOOLING WHILE THE AIRPLANE IS STATIONARY.

NOTENOTENOTENOTE:::: AIRPLANES EQUIPPED WITH PC-17 INVERTERS REQUIRE INSTALLATION OF KIT114-3006-3 S IN CONJUNCTION WITH THIS KIT.


114-3006-3 SINVERTER RELOCATION, PC-17 ATA :1900 UA-31900C UB-1 THRU UB-74SB NO. 2164 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE PC-17 INVERTERS FOR IMPROVEDINVERTER COOLING. USE WITH KIT 114-3006-1 S WITH FACTORY EQUIPPED EXTERNAL FANS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3007-1 SFLIGHT DATA RECORDER ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-55, UB-57 THRU UB-741900C-1 UC-1 AND AFTER"OPTIONAL" SB NO. 2259, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLIGHT DATA RECORDER ON IN-SERVICEAIRPLANES.

NOTENOTENOTENOTE:::: KIT 114-4017-1 S PROVIDES STRUCTURE FOR THE FLIGHT DATA AND VOICE RECORDERINSTALLATION AND MUST BE INSTALLED PRIOR TO OR IN CONJUNCTION WITH THIS KIT.



KIT CATALOG

114-3007-3 SFLIGHT DATA RECORDER INSTALLATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-55, UB-57 THRU UB-41900C-1 UC-1 AND AFTER"OPTIONAL" SB NO. 2259, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLIGHT DATA RECORDER ON IN-SERVICEAIRPLANES.

NOTENOTENOTENOTE:::: KIT 114-4017-1 PROVIDES STRUCTURE FOR THE FLIGHT DATA AND VOICE RECORDERINSTALLATION AND MUST BE INSTALLED IN CONJUNCTION WITH THIS KIT.


114-3008-1 SVOICE RECORDER INSTALLATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-55, UB-57 THRU UB-741900C-1 UC-1 AND AFTER"OPTIONAL" SB NO. 2259, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A VOICE RECORDER ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: KIT 114-4017-1 S MUST BE INSTALLED PRIOR TO OR IN CONJUNCTION WITH THIS KIT.WT. CHANGE : 31 LBS; ARM: 472 IN.; MOMENT: 14632 IN.-LBSEST. MAN/HRS: : 110MEN : 2 (MEN)

114-3009-1 SHIGH SPEED WARNING INSTALLATION ATA :1900C UB-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HIGH SPEED WARNING SYSTEM.WT. CHANGE : 6.0 LBS.; ARM: 75.0 IN.; MOMENT: 450 IN.-LBSEST. MAN/HRS: : 80MEN : 1 (MAN)

114-3009-3 SHIGH SPEED WARNING INSTALLATION ATA :1900CTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPEED WARNING DEVICE IN THE AVIONICSNOSE COMPARTMENT: A CIRCUIT BREAKER, TEST SWITCH AND A WARNING HORN AND A WARNINGLIGHT IN THE AIRCRAFTS ANNUNCIATOR PANEL.WT. CHANGE : 6.0 LBS.; ARM: 75.0 IN.; MOMENT: 450 IN.-LBSEST. MAN/HRS: : 80MEN : 1 (MAN)


KIT CATALOG

114-3010-1 SPOWER STEERING WIRING MODIFICATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-51, UB-53 AND UB-54SB NO. 2160 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO UPDATE THE POWER STEERING WIRING TO THELATEST CONFIGURATION TO IMPROVE THE SYSTEM’S OPERATION.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

114-3011-1 SEMERGENCY LOCATOR TRANSMITTER, IMPROVED REMOTE SWITCH ATA :19001900C UB-16 THRU UB-45SB NO. 2118, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE EMERGENCY LOCATOR TRANSMITTERREMOTE SWITCH.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

114-3012-1 SFLAP SWITCH BY-PASS ATA :1900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" ON HOW TO FABRICATE AND INSTALL A BY-PASS ASSEMBLYMETRICAL FLAP SWITCH, ALLOWING FLAPS TO BE RETRACTED BY GROUND MAINTENANCE PERSONNEL.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3013-1 SINDICATOR LIGHT INSTALLATION, LANDING GEAR POSITION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERSB NO. 2314THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE LANDING GEAR POSITIONINDICATOR LIGHT ASSEMBLY, (KORRY PART NUMBER 308-607-0843-004) WITH AN (EATON PART NUMBER351-33790-002) INDICATOR LIGHT ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

114-3014-1 SGYRO, DC INSTALLATION ATA :1900, 1900C, 1900C-1"OPTIONAL" SB NO. 2400THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR THE REPLACEMENT OF THE EXISTINGCOPILOT’S AIR DRIVEN GYRO WITH AN ELECTRIC DC GYRO. CASTLEBERRY (PART NUMBER: 510-21B OR510-32A) ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS ONLY APPLICABLE TO AIRCRAFT EQUIPPED WITH FRONT-MOUNTED GYROSREQUIRING 3½ X 3¼ IN. MOUNTING HOLE PATTERN (USE 510-32A) AND FRONT MOUNTEDGYRO REQUIRING 3 X 3 IN. MOUNTING HOLES (USE 510-21B).


114-3014-3 SGYRO, DC INSTALLATION ATA :1900, 1900C"OPTIONAL" SB NO. 2400THIS KIT PROVIDES "INFORMATION ONLY" NECESSARY FOR THE REPLACEMENT OF THE EXISTINGCOPILOT AIR DRIVEN GYRO WITH AN ELECTRIC DC GYRO. SEE ON -1 S KIT WITH PARTS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-3015-1 SSIGN INSTALLATION, NO SMOKE/FASTEN SEAT BELT ATA :1900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERSB NO. 2317 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE NO SMOKE/FASTEN SEATBELT ORDINANCE SIGNS WITH A SIGN THAT HAS IMPROVED SERVICE LIFE AND LAMP REPLACEMENT.THIS KIT REPLACES SIGNS ON THE CABIN PARTITION AND REMOVES SIGN ON LH FORWARD CABINWT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

114-3016-1 SPOWER STEERING, DECOTO, FAILURE ANNUNCIATION ACCESSIMPROVEMENT

ATA :

1900C-1 UC-1 AND AFTERSB NO. 2306 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO IMPROVE ACCESS TO POWER STEERINGAMPLIFIER AND RELAY PANEL ASSEMBLY AND ADDS PROVISIONS FOR POWER STEERING DISENGAGEANNUNCIATION.WT. CHANGE : N/AEST. MAN/HRS: : 5.5MEN : 1 (MAN)


KIT CATALOG

114-3017-1 SANTENNA INSTALLATION, MARKER BEACON ATA :1900C, 1900C-1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR THE REPLACEMENT OF 100-384120ANTENNA MARKER BEACON WITH 101-384179 ANTENNA MARKER BEACON.WT. CHANGE : N/AEST. MAN/HRS: : 10 TO 12MEN : 1 (MAN)

114-3018-1POWER STEERING ACTUATOR HARNESS ATA :1900C-1 UC-1 THRU UC-119THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO RELOCATE POWER STEERING ACTUATORHARNESS CONNECTORS FROM THE NOSE GEAR BRACE ASSEMBLY TO THE AFT RH NOSE WHEEL WELLAREA. THIS KIT IS USED IN CONJUNCTION WITH THE INSTALLATION OF 114-388018-17 POWER STEEWT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-3019-1 SCONTROL SWITCH, VAPOR CYCLE AIR CONDITIONER ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO ADD AN ADDITIONAL POSITION TO THECABIN TEMP MODE CONTROL SWITCH THAT PERMITS USE OF A FREON CYCLE AIR CONDITIONERREGARDLESS OF AIR CYCLE BYPASS VALVE POSITION.

NOTENOTENOTENOTE:::: LEFT HAND WING ENVIRONMENTAL PLUMBING KIT 114-5018-1 S OR -3 S MUST BEINSTALLED PRIOR TO THE INSTALLATION OF THE KIT.


114-3020-1 SCOCKPIT VOICE RECORDER INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-108, UC-149, UC-169 AND

UC-170THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A COCKPIT VOICE RECORDER ONIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS IS AN "UNDER FLOOR INSTALLATION". 114-3008 KIT IS ABOVE FLOOR.WT. CHANGE : N/AEST. MAN/HRS: : 48MEN : 1 (MAN)


KIT CATALOG

114-3020-11 SCOCKPIT VOICE RECORDER INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-108, UC-149, UC-169, UC-170THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A COCKPIT VOICE RECORDER ONIN-SERVICE AIRCRAFT IN WHICH MODIFICATION OF THE EXISTING AUDIO AMPLIFIER IS POSSIBLE INORDER TO MEET HOT MIKE REQUIREMENTS. (FOR AIRPLANES REQUIRING RELOCATION OF TH

NOTENOTENOTENOTE:::: THIS KIT IS REQUIRED FOR INITIAL INSTALLATIONS MADE AFTER OCTOBER 11, 1991.WT. CHANGE : 32 LBS.; MOMENT: 11,043 IN.-LBS.EST. MAN/HRS: : 70 TO 90MEN : 1 (MAN)


UC-170THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A COCKPIT VOICE RECORDER ONIN-SERVICE AIRCRAFT REQUIRING REPLACEMENT OF THE EXISTING AUDIO AMPLIFIER WITH A NEWAUDIO AMPLIFIER IN ORDER TO MEET HOT MIKE REQUIREMENTS. (FOR AIRPLANES NOT REQUIRI



UC-170THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A COCKPIT VOICE RECORDER ONIN-SERVICE AIRCRAFT REQUIRING REPLACEMENT OF THE EXISTING AUDIO AMPLIFIER WITH A NEWAUDIO AMPLIFIER IN ORDER TO MEET HOT MIKE REQUIREMENTS. (FOR AIRPLANES NOT REQUIRI



UC-170THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A COCKPIT VOICE RECORDER ONIN-SERVICE AIRCRAFT REQUIRING REPLACEMENT OF THE EXISTING AUDIO AMPLIFIER WITH A NEWAUDIO AMPLIFIER IN ORDER TO MEET HOT MIKE REQUIREMENTS. (FOR AIRPLANES REQUIRING R



KIT CATALOG

114-3020-9 SCOCKPIT VOICE RECORDER INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-108, UC-149, UC-169, AND

UC-170THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A COCKPIT VOICE RECORDER ONIN-SERVICE AIRCRAFT REQUIRING REPLACEMENT OF THE EXISTING AUDIO AMPLIFIER WITH A NEWAUDIO AMPLIFIER IN ORDER TO MEET HOT MIKE REQUIREMENTS. (FOR AIRPLANES REQUIRING R

NOTENOTENOTENOTE:::: THIS KIT IS REQUIRED FOR INITIAL INSTALLATIONS MADE AFTER OCTOBER 11, 1991WT. CHANGE : 32 LBS.; MOMENT: 11,043 IN.-LBS.EST. MAN/HRS: : 70 TO 90MEN : 1 (MAN)

114-3021-1 SWIRE HARNESS SUPPORT, UPPER AFT NACELLE ATA :1900C-1THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL CLAMPS IN UPPER AFT NACELLE AREA TOIMPROVE ROUTING AND CLAMPING OF WIRE HARNESS ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-3022-1 SFLIGHT DATA RECORDER INSTALLATION ATA :1900C1900C-1THIS KIT PROVIDES "INFORMATION ONLY" ON HOW TO CHANGE FROM FAIRCHILD TO SUNDSTRANDFLIGHT DATA RECORDER ON ANY AIRCRAFT WITH THE FAIRCHILD RECORDER, PART NUMBER 17-M703-247.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3023-1FLAP BIAS SENSING ATA :1900C-1WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3024-1 MFDR ACCELEROMETER RELOCATION MODIFICATION ATA :1900CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE FLIGHT DATA RECORDERACCELEROMETER FROM FS 331. 65 TO FS 296. 00.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

114-3026-1 STURN AND BANK INDICATOR INSTALLATION ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74"OPTIONAL" SB NO. 2391THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE A 3 INCH TURN AND BANKINDICATOR WITH A 2 INCH TURN AND BANK INDICATOR IN THE PILOT’S INSTRUMENT PANEL ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

114-3027-1 SENVIRONMENTAL PROTECTION IMPROVEMENT, FUEL QUANTITYSYSTEM

ATA :

1900 UA-31900C UB-1 THRU UB-74THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL IN-LINE ENVIRONMENTAL WIRESPLICES ON EXISTING FUEL QUANTITY HARNESS WIRING FOR IMPROVED FUEL QUANTITY INDICATIONRELIABILITY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

114-3028-1 SCIRCUIT BREAKER PANEL ASSEMBLY ATTACHMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1591900C-1 (C-12J) UD-1 THRU UD-6"MANDATORY" SB NO. 2406THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO ELIMINATE THE POSSIBILITY OF ANINTERNAL BUS BAR IN THE 114-381023 DC POWER PANEL FROM BECOMING GROUNDED THRU A SCREWAND INSERT USED TO ATTACH THE 114-361059 CIRCUIT BREAKER PANEL. AIRCRAFT WITH A-2000DWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2.5MEN : 1 (MAN)

114-3029-1STATIC DISCHARGER INSTL ATA :1900CWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-3030-1 SPRESSURIZATION CONTROL DIAL ILLUMINATION ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A POST LIGHT IN THE PEDESTALFOR IMPROVED ILLUMINATION OF THE PRESSURIZATION CONTROL DIAL ON IN-SERVICE AIRCRAFT WITHSINGLE WIDE PEDESTAL EXTENSION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

114-3032-1 SHOT MIKE CVR MODIFICATION ATA : 231900C UB-1 THRU UB-74 WITH 114-3020-1 KIT

INSTALLED1900C-1 UC-1 THRU UC-108, UC-149, UC-169, UC-170

WITH 114-3020-1 KIT INSTALLED"RECOMMENDED" SB NO. 23-3094THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD A HOT MIKE TO INSERVICE AIRCRAFTTHAT HAVE 114-3020-1 S COCKPIT VOICE RECORDER KITS INSTALLED. THIS KIT INSTALLATION INCLUDESREWIRING AUDIO AMPLIFIERS PROVIDED WITH KIT TO MEET HOT MIKE REQUIREMENTWT. CHANGE : + 1 LB. @ 186.0 IN.EST. MAN/HRS: : 6 TO 9MEN : 1 (MAN)

114-3033-1 SHOT MIKE CVR MODIFICATION ATA :1900C UB-1 THRU UB-74 WITH 114-3020-1 KIT

INSTALLED1900C-1 UC-1 THRU UC-108, UC-149, UC-170 WITH

114-3020-1 KIT INSTALLEDTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD A HOT MIKE TO IN-SERVICEAIRCRAFT THAT HAVE 114-3020-1 S COCKPIT VOICE RECORDER KITS INSTALLED. THIS KIT INSTALLATIONINCLUDES REWIRING EXISTING AUDIO AMPLIFIERS TO MEET HOT MIKE REQUIREMENTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

114-3034-1 SSTATIC DISCHARGER INSTALLATION ATA :1900 UA-31900C UB-1 THRU UB-741900C -1 UC-1 THRU UC-1741900C -1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" ON WHAT IS REQUIRED TO INSTALL NEW STATICDISCHARGERS, DESIGNED TO PROVIDE LONGER SERVICE LIFE ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)


KIT CATALOG

114-3035-1GPWS REWORK PROVISIONING INSTALLATION ATA :1900D UE-62 THRU UE-92 EQUIPPED WITH GPWS

PROVISIONS, EXCEPT UE-63, UE-69, UE-71THRU UE-73 AND UE-77.

"MANDATORY" SB NO. 2570, AUGUST, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY IN-SERVICE AIRCRAFT IFEQUIPPED WITH GROUND PROXIMITY WARNING SYSTEM PROVISIONS.

NOTENOTENOTENOTE:::: ADHESIVE SEALER "EA934NA QT" OR "EA9394NA QT" OR EQUIVALENT WILL BE REQUIREDFOR USE WITH THIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


114-3036-1LANDING GEAR MOTOR CIRCUIT BREAKER PANEL MOD ATA :1900C UB-1 THRU UB-35"RECOMMENDED" SB NO. 2616THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE LANDING GEAR LIMITERWITH CIRCUIT BREAKER PROTECTION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "METALSET A4 11 OZ" OR METALSET A4 6 OZ" OR OTHER SIZE WILL BE REQUIRED FORINSTALLATION OF THIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


114-3037-1INSTALLATION COCKPIT SPEAKER SILENCE ATA :1900DWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3038-1ELECTRICAL INSTALLATION CARGO CONFIGURATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES "INFORMATION ONLY" FOR CONVERSION TO CARGO CONFIGURATION OF IN-SERVICEAIRCRAFT, EXCEPT SERIALS EQUIPPED WITH OPTIONAL EMERGENCY LIGHTING OR EXECUTIVEINTERIOR. NO PARTS ARE SUPPLIED WITH THIS KIT. IT IS NOT A STAND ALONE KIT. IT MUST BEWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMERT SUPPORTMEN : N/A


KIT CATALOG

114-3039-1GPS SYSTEM INSTALLATION ATA :1900C-1 (C-12J)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3040-1TCAS SYSTEM INSTALLATION ATA :1900C-1 (C-12J)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3041-1CVR SYSTEM INSTALLATION ATA :1900C-1 (C-12J)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3042-1FDR SYSTEM INSTALLATION ATA :1900C (C-12J)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-3043-1STATIC DISCHARGER INSTALLATION - INFORMATION ONLY ATA :1900 UA-31900C UB-1 THRU UC-741900C-1 UC-180 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-100 THRU UE-326THIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO INSTALL NEW STATIC DISCHARGERS DESIGNEDTO PROVIDE LONGER SERVICE LIFE FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-3044-1PITOT HEAT INDICATOR ATA :1900C UB-1 THRU UC-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION FOR PITOT HEAT INDICATOR INSTALLATION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "M7885/4-4-2" AND "MS20426AD4" RIVETS REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


114-3049-1LANDING GEAR MOTOR CIRCUIT BREAKER ATA :1900C UB-36 THRU UB-74 (SEE NOTE)1900C-1 UC-1 THRU UC-174 (SEE NOTE)1900C-1 (C12-J) UD-1 THRU UD-6 (SEE NOTE)THIS KIT PROVIDES INFORMATION TO INSTALL AN 80-AMP LANDING GEAR POWER CIRCUIT BREAKERALONG WITH A SECOND LANDING GEAR MOTOR RELAY ON IN-SERVICE 1900 AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS APPLICABLE TO THE FOLLOWING AIRCRAFT SERIALS: UB-1 THRU UB-35WITHOUT POWER STEERING AND WITH KIT 114-3036-1 INSTALLED, UB-36 THRU UB-74WITHOUT POWER STEERING, UC-1 THRU UC-174, UD-1 THRU UD-6


114-3050-KIT-INSTL, ARTEX C406-2 ELT ATA :

1900 UA-1 TO UA-31900C UB-1 TO UB-741900C UC-1 TO UC-1641900C (C-12J) UD-1 TO UD-61900D UE-1 TO UE-19 AND UE-24 TO UE-30THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF THE ARTEX MODEL C406-2EMERGENCY LOCATOR TRANSMITTER (ELT) SYSTEM BY REPLACING THE ELT SHELF, ELT, ELT ANTENNAAND ADDING A COCKPIT SWITCH.MEN : N/A

114-3610-1CHIP DETECTOR CONNECTOR ATA :1900 UA-2 AND UA-31900C UC-1 THRU UC-1741900C UB-1 THRU UB-741900D UE-1 UE-366THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE CHIP DETECTOR ON IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-4001-1PULLEY BRACKET INSTL ATA :1900 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A RIGHT RUDDER PULLEY ANDBRACKET ON THE FRAME AT STATION FUSELAGE STATION 213.25 ON IN-SERVICE MODEL 1900 SERIESAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4002-1 SAIRSTAIR DOOR STEP INSTALLATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-24, UB-27 THRU UB-31,

UB-34, UB-35SB NO. 2079 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED DOOR STEP ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 15MEN : 1 (MAN)

114-4003-1 SRAMP INSTALLATION, SPAR ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-38SB NO. 2071 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RAMP IN THE CABIN AISLE OVER THECENTER SECTION MAIN SPAR.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : 1 (MAN)

114-4004-1 SANTENNA, UPPER AFT COMMUNICATION ATA :19001900CSB NO. 2074 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMM 3 ANTENNA.WT. CHANGE : N/AEST. MAN/HRS: : 24MEN : 1 (MAN)


KIT CATALOG

114-4005-1 SANTENNA, LOWER AFT COMMUNICATION ATA :1900 UA-1 THRU UA-31900C UB-1, UB-4 THRU UB-9, UB-11, UB-13 THRU

UB-18, UB-22, UB-24 THRU UB-26, UB-30,UB-32 THRU UB-38

SB NO. 2074 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COMM ANTENNA.WT. CHANGE : N/AEST. MAN/HRS: : 16MEN : 1 (MAN)

114-4006-1 SICE LIGHT BRACKET ATA :19001900CSB NO. 2069 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED ICE LIGHT BRACKET.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-4007-1 SCARGO DOOR, CLOSURE AID STOWAGE LATCH ATA :1900C UB-1 THRU UB-38SB NO. 2048 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CARGO DOOR CLOSURE AIDSTOWAGE LATCH.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : 1 (MAN)

114-4009-1 SAMBIENT AIR INTAKE, LOWER LEFT HAND WING LEADING EDGE ATA :1900CSB NO. 2120 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED LOWER LEFT HAND AMBIENTAIR LOUVER IN THE CENTER SECTION WING.

NOTENOTENOTENOTE:::: "DEVCON F" FILLER AND "890B" SEALANT REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 1 LBS; ARM: 179.1 MOMENT: 181EST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

114-4010-1 SFLAP BUMPER ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74SB NO. 2123 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FLAP BUMPERS TO REDUCE THE POSSIBILITYOF FLAP VIBRATION.WT. CHANGE : N/AEST. MAN/HRS: : 18MEN : 1 (MAN)

114-4011-1 SFLAP SWITCH COMPARTMENT SEAL ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-72THIS KIT PROVIDES PARTS AND INFORMATION TO SEAL THE FLAP SWITCH COMPARTMENT TO REDUCETHE POSSIBILITY OF MOISTURE ENTERING THE COMPARTMENT.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)

114-4012-1 SFLAP SWITCH LINK ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-60SB NO. 2136 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED FLAP SWITCH LINK BUSHINGS ANDROLLERS.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

114-4013-1 SAERODYNAMIC CONFIGURATION ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERTHIS KIT PROVIDES A LIST OF KITS TO BE INSTALLED TO ENHANCE PERFORMANCE CHARACTERISTICS.WT. CHANGE : N/AEST. MAN/HRS: : 280 TO 320MEN : 1 (MAN)


KIT CATALOG

114-4014-1 SVORTEX GENERATOR INSTALLATION ATA :1900 UA-31900C UB-1 THRU UB-60FOR AIRCRAFT THAT HAVE 114-4013-1 S AERODYNAMICS CONFIGURATION KIT INSTALLED. THIS KIT IS APART OF THE AERODYNAMICS CONFIGURATION KIT, WHICH MUST BE INSTALLED PRIOR TO THIS KITINSTALLATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 10MEN : 1 (MAN)

114-4015-1 SFILLET INSTALLATION, WING AND FUSELAGE ATA :1900 UA-31900C UB-1 THRU UB-60FOR AIRCRAFT THAT HAVE 114-4013-1 S AERODYNAMICS CONFIGURATION KIT INSTALLED. THIS KIT IS APART OF THE AERODYNAMICS CONFIGURATION KIT, WHICH MUST BE INSTALLED PRIOR TO THIS KITINSTALLATION.WT. CHANGE : N/AEST. MAN/HRS: : 180 TO 240MEN : 1 (MAN)

114-4016-1 SSTABILON FAIRING ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-55SB NO. 2167 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FAIRINGS ON THE LH AND RH SIDE OF THEAFT FUSELAGE AT THE STABILON LEADING EDGE.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-4017-1 SVOICE AND FLIGHT DATA RECORDER SUPPORT STRUCTURE ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE SUPPORT STRUCTURE FOR A VOICERECORDER AND/OR A FLIGHT DATA RECORDER.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-4018-1 SFENCE INSTALLATION, INBOARD WING ATA :1900 UA-31900C UB-1 THRU UB-60FOR AIRCRAFT THAT HAVE 114-4013-1 S AERODYNAMICS CONFIGURATION KIT INSTALLED. THIS KIT IS APART OF THE AERODYNAMICS CONFIGURATION KIT, WHICH MUST BE INSTALLED PRIOR TO THIS KITINSTALLATION.WT. CHANGE : N/AEST. MAN/HRS: : 12 TO 20MEN : 1 (MAN)

114-4019-1 SLANDING GEAR CENTERING SWITCH, NOSE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-67SB NO. 2170 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CENTERING SWITCH,IMPROVED WIRE ROUTING AND A PROTECTIVE BOOT TO PREVENT DUST CONTAMINATION ONAIRPLANES EQUIPPED WITH POWER STEERING.WT. CHANGE : N/AEST. MAN/HRS: : 7MEN : 1 (MAN)

114-4020-1GERMAN CERTIFICATION ATA :1900C, 1900WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4023-1 SAIRSTAIR DOOR REINFORCEMENT ATA :1900, 1900C, 1900C-1SB NO. 2216 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE LOWER HINGE ON THEAIRSTAIR DOOR.WT. CHANGE : N/AEST. MAN/HRS: : 26MEN : 1 (MAN)

114-4023-3 SAIRSTAIR DOOR REINFORCEMENT ATA :1900, 1900CSB NO. 2216 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LOWER CLOSURE REINFORCEMENTS ON THEAIRSTAIR DOOR.WT. CHANGE : N/AEST. MAN/HRS: : 26MEN : 1 (MAN)


KIT CATALOG

114-4025-1 SSPAR RAMP INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERSB NO. 2086 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL 118-400021-1 SPAR RAMPINSTALLATION THAT WILL IMPROVE THE ACCESS TO THE COMPONENTS BELOW THE FLOOR ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-4026-1 SLANDING LIGHT BULB REPLACEMENT INSTALLATION (LH) ATA :1900C-1 UC-1 AND AFTER"OPTIONAL" SB NO. 2368THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE LANDING LIGHT SUPPORTBRACKET ASSEMBLY THAT WILL IMPROVE THE METHOD OF BULB REPLACEMENT ON IN-SERVICEAIRCRAFT "LH SIDE ONLY".WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

114-4026-2 SLANDING LIGHT BULB REPLACEMENT INSTALLATION (RH) ATA :1900C-1 UC-1 AND AFTER"OPTIONAL" SB NO. 2368THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE LANDING LIGHT SUPPORTBRACKET ASSEMBLY THAT WILL IMPROVE THE METHOD OF BULB REPLACEMENT ON IN-SERVICEAIRCRAFT "RH SIDE ONLY".WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

114-4026-3 SLANDING LIGHT SUPPORT BRACKET CHANGE (LH) ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER"OPTIONAL" SB NO. 2368THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE LANDING LIGHT SUPPORTBRACKET ASSEMBLY THAT WILL IMPROVE THE METHOD OF BULB REPLACEMENT ON IN-SERVICEAIRCRAFT "LH SIDE ONLY".WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

114-4026-4 SLANDING LIGHT SUPPORT BRACKET CHANGE (RH) ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER"OPTIONAL" SB NO. 2368THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE LANDING LIGHT SUPPORTBRACKET ASSEMBLY THAT WILL IMPROVE THE METHOD OF BULB REPLACEMENT ON IN-SERVICEAIRCRAFT "RH SIDE ONLY".WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

114-4027-1 SDEICE BOOT REINFORCEMENT ATA :1900, 1900C, 1900C-1, 1900D ALL SERIALS: UA, UB, UC, UD, UE"OPTIONAL" SB NO. 2392THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ESTANE PATCH ON OUTBOARDWING DEICE BOOTS TO PROTECT THE SURFACE OF DEICE BOOTS FROM SCUFFING OR ABRADING BYFOREIGN OBJECTS SUCH AS FUEL HOSES.

NOTENOTENOTENOTE:::: ONE KIT MAY BE ABLE TO COVER 10 AIRCRAFT AND IT IS RECOMMENDED THAT YOUREFRIGERATE SEALANTS AND ACCELERATOR, ESPECIALLY THE ACCELERATOR, ONLYMIX WHAT YOU NEED, CLOSE CAN, AND RE-REFRIGERATE FOR MAXIMUM USAGE ASTHESE ARE 6 MONTH SHELF LIFE ITEMS.


114-4028-1 SREINFORCEMENT, COMM ANTENNA ATA :19001900C UB-2 THRU UB-741900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW REINFORCEMENT PARTS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-4030-1 SHANDRAIL, ADJUSTABLE INSTALLATION ATA :1900 UA-1 THRU UA-41900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1001900C-1 (C12-J) UD-1 THRU UD-6SB NO. 2316 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION NECESSARY TO INSTALL A TURNBUCKLE ASSEMBLYFOR ADJUSTMENT OF THE AIRSTAIR DOOR HANDRAIL CABLE TENSIONS.WT. CHANGE : N/AEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

114-4031-1 SAIRSTAIR DOOR - SPARES ATA :1900 UA-1 THRU UA-41900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1001900C-1 (C12-J) UD-1 THRU UD-6THIS KIT FURNISHES THE SPARE REPLACEMENT FOR 114-514068-1 SUPPORT ASSEMBLY AND FOR THE101-514014-3 BOLT.WT. CHANGE : N/AEST. MAN/HRS: : 2.5MEN : 1 (MAN)

114-4032-1 SDAMPER ATTACHMENT BRACKET, AIRSTAIR DOOR ATA :1900, 1900C, 1900C, 1900C-1 (C12-J)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE DAMPER ATTACHMENTBRACKET ON THE AIRSTAIR DOOR. AIRCRAFT PRIOR TO UC-9 REQUIRE KIT 114-4023-3 S TO BEINSTALLED PRIOR TO OR CONCURRENT WITH THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-4033-1 SSEAL INSTALLATION AIRSTAIR DOOR ATA :1900, 1900C, 1900C-1, 1900C-1 (C-12J)THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE DOOR SEAL AND RETAINERS FROM THEDOOR AND INSTALL DOOR SEAL AND NEW RETAINERS ON THE DOOR FRAME.WT. CHANGE : N/AEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

114-4034-1 SLANDING LIGHT, HALOGEN LAMP ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1391900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2368, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HALOGEN LANDING LIGHT LAMPS IN PLACEOF EXISTING LANDING LIGHT LAMP FOR IMPROVED SERVICE LIFE OF LAMPS.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

114-4035-1 PGRAVEL RUNWAY PROTECTION INSTALLATION ATA :1900CTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL GRAVEL GUARDS ON INBOARD FLAPS, BELLYANTI-COLLISION LIGHT AND COM 2 ANTENNAS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24 TO 30MEN : 1 (MAN)

114-4035-3 PGRAVEL RUNWAY LANDING OPTION INSTALLATION ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL GRAVEL GUARDS ON INBOARD FLAPS, BELLYANTI-COLLISION LIGHT AND COM 2 ANTENNA.

NOTENOTENOTENOTE:::: FOR GRAVEL WINDOW FOR CABIN AREA, SEE KIT 129-4001-1 SNOTENOTENOTENOTE:::: WILL REQUIRE FLIGHT MANUAL SUPPLEMENT PART NUMBER 129-590000-31 WHEN YOU

INSTALL THIS KIT ON ANY AIRCRAFT. NOT PART OF KIT, RECOMMEND ORDERING ATSAME TIME YOU ORDER THIS KIT.

NOTENOTENOTENOTE:::: THIS KIT REPLACES -1 S KIT AND PROVIDES LONGER GRAVEL PROTECTION SHIELDSTHAN THE KIT IT REPLACED.

WT. CHANGE : + 6 LBS.; MOMENT: + 2052 IN.-LBS.EST. MAN/HRS: : 24 TO 30MEN : 1 (MAN)

114-4036-1 SRADOME ABRASION BOOT INSTALLATION ATA :1900, 1900C, 1900C-1, 1900C-1 (C-12J)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ABRASION BOOT ON THE RADOME.WT. CHANGE : N/AEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

114-4037-1UPPER WING SKIN REPAIR ATA :1900WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-4038-1 SWING SPAR INSPECTION ACCESS ATA :1900 UA-2, UA-31900C UB-1 THRU UB-74THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO GAIN ACCESS FOR WING SPARINSPECTIONS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)

114-4039-1 SSPAR CAP REINFORCEMENT, REAR ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900/1900C MAINTENANCE MANUAL, CHAPTER 4, A39, PAGE 2, TOP RH SIDE OF PAGE, "INSPECTION" 5LINES UP FROM "REINFORCEMENT KIT".THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL REAR SPAR REINFORCEMENTS.

NOTENOTENOTENOTE:::: SEE 1900 AIRLINER COMMUNIQUE NO. 28, REV. I FOR ADDITIONAL INFORMATION ON KIT.WT. CHANGE : 3.0 LBS; MOMENT: 977 IN.-LBSEST. MAN/HRS: : 60 TO 70MEN : 1 (MAN)

114-4040-1 SSTORM WINDOW SEAL INSTALLATION ATA :ALL 1900 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL AND REPAIR THE LH AND RHSTORM WINDOW SEAL ON ALL AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5 TO 1.5MEN : 1 (MAN)

114-4041-1 SSPAR CAP REINFORCEMENT, REAR ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900/1900C MAINTENANCE MANUAL, CHAPTER 4-00-00, A39, PAGE 2, "INSPECTION" (TOP RH SIDE OFPAGE 2ND LINE UP FROM "REINFORCEMENT KIT".)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL REAR SPAR REINFORCEMENTS.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED BUT WILL NOT BE FURNISHED AS PART OFTHE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY"EC2216A/B" SEALER QT OR "EC2216A/B 2 OZ" SEALER KIT AND FILLER PART NUMBER"METALSET A4 6 OZ" OR "METALSET A4 11 OZ" WHICHEVER YOU DESIRE AS KIT DRAWINGONLY STATES AS REQUIRED QUANTITY FOR ADHESIVE SEALER AND FILLER.

NOTENOTENOTENOTE:::: SEE 1900 AIRLINER COMMUNIQUE NO. 28, REV. I, APRIL 1993 FOR ADDITIONALINFORMATION.

WT. CHANGE : 3.0 LBS; MOMENT: 977 IN.-LBSEST. MAN/HRS: : 60 TO 72MEN : 1 (MAN)


KIT CATALOG

114-4042-1 SFLAP RIB REPLACEMENT ATA :1900 UA-2, UA-31900C UB-1THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO GAIN ACCESS TO AND REPLACEMENT OF35-165050-84 FLAP RIBS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8MEN : 1 (MAN)

114-4044-1 SSEAT TRACK REPLACEMENT ATA :1900 SERIESTHIS KIT PROVIDES "INFORMATION ONLY" ON REPLACEMENT OF THE INBOARD HALF OF THE RHOUTBOARD SEAT TRACK.WT. CHANGE : 2.67 LBS; MOMENT: 310 IN.-LBSEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

114-4044-3 SSEAT TRACK REPLACEMENT ATA :1900 SERIESTHIS KIT PROVIDES "INFORMATION ONLY" ON REPLACEMENT OF THE INBOARD HALF OF THE LHOUTBOARD SEAT TRACK.WT. CHANGE : 2.67 LBS; MOMENT: 310 IN.-LBSEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

114-4045-1 SSEAT TRACK REPAIR, OUTBD ATA :1900, 1900C, 1900C-1, 1900C-1(C-12J)WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4046-1 SBAGGAGE AFT COMPARTMENT SUPPORT ATA :1900C UB-1 THRU UB-18"OPTIONAL" SB NO. 2427THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ADDITIONAL AFT BAGGAGECOMPARTMENT SUPPORT. THIS KIT IS USED IN CONJUNCTION WITH SB NO. 2427.WT. CHANGE : + 15 LBS; MOMENT: + 7574 IN.-LBSEST. MAN/HRS: : 25MEN : 2 (MEN)


KIT CATALOG

114-4046-3 SBAGGAGE AFT COMPARTMENT SUPPORT ATA :1900C UB-19 THRU UB-57"OPTIONAL" SB NO. 2457THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL ADDITIONAL AFT BAGGAGECOMPARTMENT SUPPORT. THIS KIT IS USED IN CONJUNCTION WITH SB NO. 2427.WT. CHANGE : +6 LBS; MOMENT: + 3199 IN.-LBSEST. MAN/HRS: : 25MEN : 2 (MEN)

114-4047-1 SDAMPENER SUPPORT INSTALLATION, AIRSTAIR DOOR ATA :1900C-1 UC-1 AND AFTERTHIS KIT PROVIDES THE EQUIPMENT AND INFORMATION TO INSTALL THE IMPROVED SUPPORTASSEMBLY AND THE ATTACHING HARDWARE FOR THE IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

114-4048-1COMM ANTENNA, LOWER AFT, REINFORCEMENT INSTALLATION ATA :1900C-1 UC-1 THRU UC-721900C-1 (C-12J) UD-1 THRU UD-6"RECOMMENDED" SB NO. 2579THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DOUBLER AND STIFFENERS AT THE COMMANTENNA BASE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309 QT" OR "EA9309NA QT" ADHESIVE NON-ASBESTOS MATERIAL AND "NAPTHA-TT-N-95A" CLEANER WILL BE REQUIRED FOR INSTALLATION OF THIS KIT. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


114-4049-1CARGO NET INSTALLATION ATA :1900C UB-1 AND AFTER1900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PART NUMBERS AND INSTRUCTIONS FOR INSTALLING CARGO NETS ANDSUPPORTING STRUCTURE FOR THE IN-SERVICE AIRCRAFT. THIS KIT IS NOT A STAND ALONE KIT. IT MUSTBE INSTALLED AS A PART OF 114-0100-1 1900C CARGO CONFIGURATION KIT.

NOTENOTENOTENOTE:::: WEIGHT AND BALANCE INFORMATION, SEE RAYTHEON CARGO CONFIGURATIONDRAWING 114-0100-1.



KIT CATALOG

114-4050-1FLOORBOARD INSTALLATION CARGO ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO ADD A CARGO FLOORBOARD INSTALLATION.THIS IS NOT A STAND ALONE KIT AND MUST BE INSTALLED AS PART OF KIT 114-0100-1 CARGOCONFIGURATION KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4051-1RIB ASSEMBLY REINFORCEMENT ATA : 571900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UC-61900D UE-1 THRU UE-236"RECOMMENDED" SB NO. 57-3066THIS KIT PROVIDES INFORMATION TO REINFORCE THE LH RIB ASSEMBLY AT WING STATION 83.00 FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MIL-C-9084 TYPE VIIIB (181-150 C9084 72), EA9394 (EA9394 QT), EA956 (EA956 QT)REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


114-4052-1COLD EXPANSION OF HOLES ATA :1900 UA-2, UA-31900C UB-1 THRU UB-74THIS KIT PROVIDES PARTS AND INFORMATION FOR THE REPLACEMENT OF FASTENERS AND COLDEXPANDING THE HOLES IN THE CENTER SECTION REAR SPAR, AS REQUIRED FOR THE 30,000 HOURWING INSPECTION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "CR3242-4" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 2 LBS; MOMENT: 653 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4053-1COLD EXPANSION OF HOLES - INFORMATION ONLY ATA :ALL 1900 SERIESTHIS KIT PROVIDES "INFORMATION ONLY" AND PROCESS FOR THE COLD EXPANSION OF CRITICALHOLES IN ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-4054-1STATIC WICK REMOVAL, STABILION ATA :ALL 1900 SERIESTHIS KIT PROVIDES "INFORMATION ONLY" FOR THE REMOVAL OF STATIC WICKS FROM THE STABILIONSON ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4055-1EROSION STRIP INSTALLATION, SURFACE DEICE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" TO INSTALL AN EROSION STRIP ALONG THE LENGTH OF THEPNEUMATIC DEICER(S) LEADING EDGE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4056-1EROSION STRIP INSTALLATION, SURFACE DEICE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-74THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLING INSPECTION DOOR PROVISIONS AT THEFRONT SPAR ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MS20426AD4", "MS20426AD3", AND "MS20426B4" REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 1 LB MOMENT:291 IN.-LBS.EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4057-1SIDE SEAT TRACK REPLACEMENT, INBOARD HALF - INFORMATIONONLY

ATA :

19001900CTHIS KIT PROVIDES INFORMATION TO REPLACE THE INBOARD HALF OF THE RIGHT HAND SIDE SEATTRACK.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-4057-3SIDE SEAT TRACK REPLACEMENT, INBOARD HALF - INFORMATIONONLY

ATA :

19001900CTHIS KIT PROVIDES INFORMATION TO REPLACE THE INBOARD HALF OF THE LEFT HAND SIDE SEATTRACK.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4058-1SIDE SEAT TRACK REPLACEMENT, INBOARD HALF ATA :ALL 1900 SERIES ALL AIRCRAFT BUILT PRIOR TO UE-389THIS KIT PROVIDES INFORMATION TO ADD A DRAIN HOLE IN THE FRAME WEB AT FS 288.00 FOR ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MS20470AD5 RIVETS REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


114-4059-1SPAR CAP CHAFING BLOCK INSTALLATION - INFORMATION ONLY ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-1 THRU UE-422THIS KIT PROVIDES INFORMATION ONLY TO INSTALL A SPAR CAP CHAFING BLOCK TO ALL INSERVICEAIRCRAFTWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4060-0001EMPENNAGE INSPECTION PANELS, INFO ONLY ATA :1900 UA-2 THRU UA-3, UB-1 THRU UB-74, UC-1

THRU UC-174, UD-1 THRU UD-6 AND UE-1AND AFTER

THIS KIT PROVIDES INFORMATION TO FABRICATE AND INSTALL ACCESS PANELS TO THE VERTICAL ANDHORIZONTAL STABILIZER ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FAA REF. LETTER 2002-11-102, 81-10 FORM RECORD OF COMPLIANCE.WT. CHANGE : WT: +3.6 LB MOMENT: +2329 IN-LBEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

114-4060-1EMPENNAGE INSPECTION PANELS, INFORMATION ONLY ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES INFORMATION TO FABRICATE AND INSTALL ACCESS PANELS TO THE VERTICAL ANDHORIZONTAL STABILIZER ON INSERVICE AIRCRAFT.WT. CHANGE : +3.6 LBS MOMENT: +2329 IN-LBEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-4063-0001INBOARD FLAP SKIN IMPROVEMENT ATA :1900 UC-1 THROUGH UC-1741900 UA-3 THAT HAVE REPLACED THE

101-160001-17 FLAP WITH A LATER PARTNUMBER AS SPARES

1900C UB-1 THROUGH UB-42 THAT HAVEREPLACED THE 101-160001-17 FLAP WITHA LATER PART NUMBER AS SPARES.

1900C UD-1 THROUGH UD-61900C(C-12J) UB-43 THROUGH UB-741900D UE-1 THROUGH UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 0.032 INCH THICK SKINS ON LEFT HANDINBOARD FLAPS. THIS KIT IS FOR FLAPS THAT DO NOT HAVE THE FLAP ASYMMETRIC SWITCH ROD ENDADJUSTABLE LINKAGE.

THIS KIT DOES NOT APPLY TO THE LEFT INBOARD FLAP PART NUMBER 101-160001-17 THAT WASINSTALLED IN PRODUCTION ON 1900 SERIAL UA-3 AND 1900C SERIALS UB-1 THRU UB-42.

NOTENOTENOTENOTE:::: UB-43 THROUGH UB-74MEN : N/A

114-4063-0003INBOARD FLAP SKIN IMPROVEMENT ATA :1900 UA-3 THAT HAVE REPLACED THE

101-160001-31 FLAP WITH A LATER PARTNUMBER AS SPARES.

1900C UB-1 THROUGH UB-42 THAT HAVEREPLACED THE 101-160001-31 FLAP WITHA LATER PART NUMBER AS SPARES.

1900C UB-43 THROUGH UB-74 AND UC-1THROUGH UC-174

1900C(C-12J) UD-1 THROUGH UD-61900D UE-1 THROUGH UE-375KIT PROVIDES PARTS AND INFORMATION TO INSTALL 0.032 INCH THICK SKINS ON RIGHT HAND INBOARDFLAPS.

THIS KIT IS FOR FLAPS THAT DO NOT HAVE THE FLAP ASYMMETRIC SWITCH ROD END ADJUSTABLELINKAGE.

THIS KIT DOES NOT APPLY TO THE RIGHT INBOARD FLAP PART NUMBER 101-160001-31 THAT WASINSTALLED IN PRODUCTION ON 1900 SERIAL UA-3 AND 1900C SERIALS UB-1 THRU UB-42.MEN : N/A


KIT CATALOG

114-4063-0004INBOARD FLAP SKIN IMPROVEMENT ATA :1900 UA-3 THROUGH UB-42 THAT HAVE

REPLACED THE 101-160001-31 FLAP WITHA LATER PART NUMBER AS SPARES.

1900C 1900C SERIALS UB-1 THROUGH UB-42THAT HAVE REPLACED THE 101-160001-31FLAP WITH A LATER PART NUMBER ASSPARES.

1900C UB-43 THROUGH UB-74 AND UC-1THROUGH UC-174

1900C(C-12J) UD-1 THROUGH UD-61900D UE-1 THROUGH UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 0.032 INCH THICK SKINS ON RIGHT HANDINBOARD FLAPS.

THIS KIT IS FOR FLAPS MODIFIED BY KIT 118-4013 TO USE THE FLAP ASYMMETRIC SWITCH ROD ENDADJUSTABLE LINKAGE.

THIS KIT DOES NOT APPLY TO THE RIGHT INBOARD FLAP PART NUMBER 101-160001-31 THAT WASINSTALLED IN PRODUCTION ON 1900 SERIAL UA-3 AND 1900C SERIALS UB-1 THRU UB-42.MEN : N/A

114-4067-0001COLD EXPANSION OF FASTERNER HOLES IN REAR SPAR ATA : 571900 UA-2 AND UA-31900C UB-1 THRU UB-7457-3816THIS KIT PROVIDES PARTS AND INFORMATION FOR THEREPLACEMENT OF FASTENERS AND COLD EXPANDING THEW.S 80.00 TO W.S 124.00. FOR IN-SERVICE AIRCRAFTMODEL 1900 AND MODEL 1900C. SERIALS ELIGIBLE:UA-2 AND UA-3, UB-1 THRU UB-74.NOTE: THIS KIT MUST HAVE KIT 114-4052-1 INSTALLEDPRIOR TO OR IN CONJUNCTION WITH THIS KIT.

7/18/7 1900 KIT, DO NOT CANCEL ORDERS VSBLOCKED FOR SALES UNTIL WE GET A RESPONSE FOR DENISE LOPEZ. 5/21/07

NOTENOTENOTENOTE:::: NOTE: THIS KIT MUST HAVE KIT 114-4052-1 INSTALLED PRIOR TO OR IN CONJUNCTIONWITH THIS KIT.

MEN : N/A

114-4300-1WINDOW INSTALLATION CABIN ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES "INFORMATION ONLY" NECESSARY TO CONVERT THE AIRCRAFT FROM PASSENGERTYPE TO CARGO TYPE. THIS KIT IS NOT A STAND ALONE KIT. IT MUST BE INSTALLED AS A PART OF114-0100-1 CARGO CONFIGURATION KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-5000-1 PCOMBINATION PASSENGER/CARGO CONFIGURATION MODIFICATION ATA :1900CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MAKE OPTIONAL LOCATIONS FOR THEINSTALLATION OF THE AFT CARGO PARTITIONS. THIS INCREASES CARGO SPACE BY REDUCINGPASSENGER AREA.

NOTENOTENOTENOTE:::: FOR WEIGHT AND BALANCE INFORMATION SEE RAYTHEON CARGO CONFIGURATIONDRAWING 114-0100-1.


114-5001-1 POXYGEN SYSTEM, CABIN ATA :1900C UB-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CABIN OXYGEN SYSTEM REQUIRED FORFLIGHT WITH PASSENGERS ABOVE 15,000 FT.WT. CHANGE : 69.4 LBS. @141.7 ARMEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5002-1 SCOWLING AIR INLET REINFORCEMENT, ENGINE ATA :ALL 1900 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION TO REINFORCE THE ENGINE COWLINGS.WT. CHANGE : N/AEST. MAN/HRS: : 10MEN : 1 (MAN)

114-5003-1BRAKE DEICE INSTALLATION ATA :1900CTHIS KIT PROVIDES ITEMS REQUIRED TO INSTALL A BRAKE DEICE SYSTEM ON IN-SERVICE 1900CAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

114-5004-1 SELEVATOR CONTROL CABLE CLEARANCE CUTOUT ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-46SB NO. 2070 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK THE BULKHEAD AT F.S. 588.10 TO IMPROVEELEVATOR CONTROL CABLE CLEARANCE.WT. CHANGE : N/AEST. MAN/HRS: : 2MEN : 1 (MAN)


KIT CATALOG

114-5005-1 SLANDING GEAR CONTROL SWITCH INSTALLATION - SPARES ATA :19001900C"OPTIONAL" SB NO. 2412THIS KIT IS A SPARES REPLACEMENT FOR 101-384137-1 SWITCH.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5006-1 SDIFFERENTIAL PRESSURE AND STATIC PLUMBING ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-50SB NO. 2075 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO CONNECT THE DIFFERENTIAL PRESSURE GAGE TOTHE ALTERNATE STATIC LINE TO PROVIDE A MORE RELIABLE DIFFERENTIAL PRESSURE READING.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 1 (MAN)

114-5007-1 PSCUFF COVER, NOSE BAGGAGE COMPARTMENT ATA :1900C UB-1 THRU UB-37THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED SCUFF COVER FOR THE NOSEBAGGAGE COMPARTMENT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5008-1 SELEVATOR TRIM TAB CABLE GUARD ATA :1900C UB-1 THRU UB-62SB NO. 2028, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CABLE GUARD ON THEELECTRIC ELEVATOR TRIM ACTUATOR.

NOTENOTENOTENOTE:::: KIT 90-5065-1 S MUST BE INSTALLED IN CONJUNCTION WITH THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : 4.5MEN : 1 (MAN)


KIT CATALOG

114-5009-1 SCHAIR ADJUST CABLES, CREW ATA :19001900CSB NO. 2119 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE LONGITUDINAL POSITIONING CABLES ONBOTH CHAIRS.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-5010-1 SCARGO DOOR HANDLE COVER INSTALLATION ATA :1900C UB-1 THRU UB-38SB NO. 2117 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A COVER OVER THE CARGO DOOR INSIDEHANDLE.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-5011-1 SAIR CONDITIONER COMPRESSOR MOUNTING BRACKET ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-47SB NO. 2128 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED AIR CONDITIONERCOMPRESSOR MOUNTING BRACKET, HOSE ASSEMBLIES AND DRIVE BELT TO REDUCE BELT WEAR.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 1 (MAN)

114-5012-1 SAILERON TAB CABLE FAIRLEAD ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-30, UB-32 THRU UB-36,

UB-38, UB-41SB NO. 2124 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AILERON TAB CABLE FAIRLEAD ON A WINGRIB CABLE CUTOUT.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

114-5014-1 SPRESSURIZATION SENSE LINE DRAIN ATA :1900C UB-1 THRU UB-67SB NO. 2185 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DRAIN VALVE IN THE PRESSURIZATIONSENSE LINE.WT. CHANGE : N/AEST. MAN/HRS: : 5MEN : 1 (MAN)

114-5015-1 SDOWN LOCK PIN INSTALLATION ATA :19001900CSB NO. 2245 OR SUBSEQUENTTHIS KIT PROVIDES "INFORMATION ONLY" TO FABRICATE AND INSTALL DOWN-LOCK ASSEMBLIES (NOSEAND MAIN GEARS). ALL MATERIAL OR HARDWARE WILL HAVE TO BE PURCHASED LOCALLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5016-1 SFILTER INSTALLATION, ENVIRONMENTAL PLUMBING, WING ATA :19001900C1900C-1THIS KIT PROVIDES "INFORMATION ONLY" NECESSARY TO FABRICATE PARTS REQUIRED TO REPLACEFILTERS ON BLEED-AIR SYSTEM. NO MATERIAL OR HARDWARE ARE FURNISHED WITH THIS KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5016-3 SFILTER ENVIRONMENTAL PLUMBING ATA :1900C-1 UC-6 AND AFTER1900C-1 (C-12J) UD-3 THRU UD-6CO G05541THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE FILTERS ON THE BLEED AIRSYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-5016-7 SFILTER ENVIRONMENTAL PLUMBING ATA :1900 UA-31900C UB-1 AND AFTER1900C-1 UC-1 THRU UC-51900C-1 (C-12J) UD-1 AND UD-2CO G05541THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL FILTERS ON THE BLEED AIRSYSTEM ON AIRCRAFT WITH PROVISIONS FOR AIRTIGHT POWER STEERING INSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5017-1 SINLET GUARD INSTALLATION, BLOWER ATA :1900, 1900CSB NO. 2232 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN INLET GUARD ON ELECTRO-MECH BLOWER ASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5018-1 SENVIRONMENTAL PLUMBING, LH WING ATA :1900, 1900CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A TEMPERATURE SENSOR AND APRESSURE SWITCH ON THE ENVIRONMENTAL SYSTEM PLUMBING. KIT 114-5016 SHOULD BE INSTALLEDIN CONJUNCTION WITH THIS KIT FOR MAXIMUM SYSTEM RELIABILITY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5018-3 SENVIRONMENTAL PLUMBING, LH WING ATA :1900 UA-31900C UB-1 THRU UB-53SB NO. 2257 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A TEMPERATURE SENSOR AND APRESSURE SWITCH ON THE ENVIRONMENTAL SYSTEM PLUMBING. KIT 114-5016 SHOULD BE INSTALLEDIN CONJUNCTION WITH THIS KIT FOR MAXIMUM SYSTEM RELIABILITY.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-5019-1 SMANUAL STEERING INSTALLATION, NOSE LANDING GEAR ATA :19001900C UB-14 THRU UB-74THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT AIRLINERS FROM POWERSTEERING TO MANUAL STEERING.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5019-3 SMANUAL STEERING INSTALLATION, NOSE LANDING GEAR ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-13SB NO. 2163 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT POWER STEERING TO MANUALSTEERING.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5021-1 PPLACARD, LIMITATION INSTALLATION ATA :1900C-1 UC-4, UC-6, UC-8, UC-23THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BAGGAGE WEIGHT PLACARDS THAT SHOWLIMITATIONS IN BOTH POUNDS AND KILOGRAMS. EXPORT AIRCRAFT ONLY.WT. CHANGE : N/AEST. MAN/HRS: : 1.5MEN : 1 (MAN)

114-5022-1 SCABIN SEAT, BACKREST STOP INSTALLATION ATA :1900, 1900CTHIS KIT PROVIDES "INFORMATION ONLY" ON HOW TO FABRICATE AND INSTALL OR REINFORCE THEBACKREST STOPS ON THE CABIN SEATS. ALL DETAILS YOU CAN PROCURE LOCALLY.WT. CHANGE : N/AEST. MAN/HRS: : 10MEN : 1 (MAN)


KIT CATALOG

114-5023-1 SSWITCH INSTALLATION, ASYMMETRICAL FLAP ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-531900C-1 (C-12J) UD-1 THRU UD-61900 COMMUNIQUE NO. 20 AND SB NO. 2326THIS KIT PROVIDES PARTS AND INFORMATION FOR THE REPLACEMENT OF THE AN276-2 OR C100101ROD ENDS AND NAS354-4-150 ROD IN THE ASYMMETRICAL SWITCH INSTALLATION WITH THE HARDWAREFOR IMPROVED SERVICE.

NOTENOTENOTENOTE:::: 114-5023-1 (LH) OR 114-5023-2 (RH) KITS MAY BE INSTALLED SEPARATELY OR TOGETHER.ONE KIT GOOD FOR EITHER SIDE.


114-5024-1 SDUCT INSTALLATION, AIR CYCLE MACHINE ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1001900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES "INFORMATION ONLY" ON THE MODIFICATIONS THAT ARE INTENDED TO INCREASETHE DURABILITY OF THE 114-550120-1 DUCT ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 16MEN : 1 (MAN)

114-5025-1 SDEFLECTOR INSTALLATION, CONDENSER SECTION ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1001900C-1 (C-12J) UD-1 THRU UD-6AIRLINER COMMUNIQUE NO. 19THIS KIT PROVIDES "INFORMATION ONLY" FOR THE FABRICATION AND INSTALLATION OF A DEFLECTORASSEMBLY TO PROTECT THE CONDENSER COIL FORM DEBRIS AND HAIL DAMAGE. ITEMS REQUIRED FORINSTALLATION MAY BE PROCURED LOCALLY.WT. CHANGE : N/AEST. MAN/HRS: : 16MEN : 1 (MAN)

114-5027-1PLACARD, ESCAPE ROUTE ATA :1900C, 1900, 1900C-1WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-5028-1MANUAL STEERING INSTL, NOSE GEAR ATA :1900C1900DWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5029-1 SMANUAL STEERING INSTALLATION, NOSE LANDING GEAR ATA :1900C-1 UC-1 AND AFTER1900D UE-1 AND AFTER"OPTIONAL" SB NO. 2263, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO CONVERT AIRLINERS FROM POWERSTEERING TO MANUAL STEERING.WT. CHANGE : WT: -18 LBS; MOMENT: -983 IN.-LBSEST. MAN/HRS: : 14MEN : 2 (MEN)

114-5029-3 SMANUAL STEERING INSTALLATION ATA :1900C-1 UC-1 AND AFTER1900D UE-1 AND AFTER"OPTIONAL" SB NO. 2263, REV. 1THIS KIT PROVIDES "INFORMATION ONLY" ON WHAT IS REQUIRED TO CONVERT AIRLINERS FROM POWERSTEERING TO MANUAL STEERING. PARTS REQUIRED TO PERFORM THE MODIFICATION MAY BEOBTAINED BY SEPARATELY PROCURING 114-5019-1 S KIT PLUS THE ADDITIONAL PARTS NOTED ON THWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 14MEN : 2 (MEN)

114-5030-1 SEXHAUST LOUVER AND DEFLECTOR INSTALLATION, CONDENSERSECTION

ATA :

1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1431900C-1 (C-12J) UD-1 THRU UD-61900D UE-1"OPTIONAL" SB NO. 2353THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A COOLING AIR EXHAUST LOUVERAND COMPATIBLE CONDENSER DEFLECTOR ASSEMBLY. THIS MODIFICATION IS INTENDED TO IMPROVECONDENSER BLOWER LIFE AND REDUCE BLOWER EXIT LOUVER FATIGUE AND CONDENSER FIN DAWT. CHANGE : WT: + 3.6 LBS @ 276.39 IN.-LBSEST. MAN/HRS: : 21MEN : 2 (MEN)


KIT CATALOG

114-5032-1 SBRAKE, HYDRAULIC PLUMBING INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-25THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO SECURE HYDRAULIC PLUMBING BYADDITIONAL BRACKET AND CLAMPING.WT. CHANGE : N/AEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

114-5033-1 SBAGGAGE WEB INSTALLATION FORWARD FULL HEIGHT ATA :1900C UB-1 AND AFTER1900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FULL HEIGHT BAGGAGE WEB IN THEFORWARD CABIN BAGGAGE COMPARTMENT FOR IN-SERVICE AIRCRAFT. THE -1 KIT DOES NOT INCLUDETHE 114-530248-1 BAGGAGE RETENTION PLACARD.WT. CHANGE : N/AEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

114-5033-3 SBAGGAGE WEB INSTALLATION, FORWARD FULL HEIGHT WITHPLACARD

ATA :

1900C UB-1 AND AFTER1900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FULL HEIGHT BAGGAGE WEB IN THEFORWARD CABIN BAGGAGE COMPARTMENT FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT INCLUDES RETENTION INSTRUCTION PLACARD.WT. CHANGE : N/AEST. MAN/HRS: : 8 TO 12MEN : N/A

114-5034-1 SCARGO DOOR RAIN GUTTER INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CARGO DOOR RAIN GUTTER ON IN-SERVICEAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)


KIT CATALOG

114-5036-1 SDRAIN PROVISION, INSTRUMENT AIR VALVE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-74 WITH 114-9020

INSTALLED1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6 WITH 101-381015-1 OR -5

INSTALLEDTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO ADD A DRAIN TO VENT ANY ACCUMULATEDMOISTURE FROM INSIDE THE INSTRUMENT AIR VALVE IN THE WING LEADING EDGE LOCATION. THIS KITIS OF NO USEFUL BENEFIT TO OLDER AIRCRAFT WITH VALVES LOCATED ADJACENT TO THEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : N/A

114-5037-1 SPRESSURE REGULATOR/SHUTOFF VALVE - SPARES ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTER1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE JANITROL PRESSUREREGULATOR SHUTOFF VALVE FOR PART NUMBERS 114-380042-5, -6, -9, -11, -13, -15, OR -17, WITH DUKESVALVE PART NUMBER 114-380042-19. ONE KIT IS REQUIRED PER VALVE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : N/A

114-5037-3 SPRESSURE REGULATOR/SHUTOFF VALVE - SPARES ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE JANITROL PRESSUREREGULATOR/SHUT-OFF VALVE, PART NUMBER'S: 114-380042-5, -7, -9, -11, -13, -15, OR -17 OR THE DUKESVALVE 114-380042-19, WITH THE LATEST DUKES VALVE ON IN-SERVICE AIRCRAFT.WT. CHANGE : SEE KIT DRAWING NOTE 4 FOR CORRECT INFORMATION PENDING SYSTEM BEING REPLACED.EST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)


KIT CATALOG

114-5038-1 SGUARD INSTALLATION, PRESSURIZATION CONTROLLER ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-4THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO ADD A PROTECTIVE GUARD OVER THEFACE OF THE PRESSURIZATION CONTROLLER. THIS MOD IS INTENDED TO IMPROVE SYSTEM RELIABILITYBY REDUCING THE INCIDENCE OF DAMAGE TO THE SENSITIVE CONTROLLER ON IN-SERVICE AIRWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5 TO .8MEN : 1 (MAN)

114-5040-1AIR CREW EYE AND RESPIRATORY PROT PROVISIONS INSTL ATA :1900C-1 (C-12J) UD-1 THRU UD-6WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5042-1 SPILOT ONLY OPERATION, DO NOT OCCUPY SEAT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL DO NOT OCCUPY COVER TUBESOVER EXISTING SEAT BELTS ON 10 CABIN SEATS ON INSERVICE AIRCRAFT SO THAT IT MAY BEOPERATED WITH A MINIMUM CREW OF ONE PILOT IN ACCORDANCE WITH THE FAA APPROVED AIRPLAN

NOTENOTENOTENOTE:::: THIS DEVICE MAY BE USED TO RENDER ANY SEAT IN THE CABIN INOPERATIVE.NOTENOTENOTENOTE:::: SEE 114-5042-3 S KIT FOR "INFORMATION ONLY".

WT. CHANGE : + 2 LBS.; @ 164 IN.EST. MAN/HRS: : .5MEN : 1 (MAN)


KIT CATALOG

114-5042-3 SPILOT ONLY OPERATION, DO NOT OCCUPY SEAT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" ON WHAT IS NECESSARY TO INSTALL "DO NOT OCCUPY"COVER TUBES OVER EXISTING SEAT BELTS ON 10 CABIN SEATS ON IN-SERVICE AIRCRAFT SO THAT ITMAY BE OPERATED WITH A MINIMUM CREW OF ONE PILOT IN ACCORDANCE WITH THE FAA APPRO

NOTENOTENOTENOTE:::: SEE 114-5042-1 S KIT IF YOU DESIRE KIT WITH 10 |P`DO NO OCCUPY|P' SEAT BELT COVERTUBES WHICH MEET FAR 23.853 FLAMMABILITY REQUIREMENTS.

NOTENOTENOTENOTE:::: THIS DEVICE MAY BE USED TO RENDER ANY SEAT IN THE CABIN INOPERATIVE.WT. CHANGE : + 2 LBS.; @ 164 IN.EST. MAN/HRS: : .5MEN : 1 (MAN)

114-5043-1 SWINDSHIELD LH, KING AIR METAL RETAINER STYLE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1751900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTER1900 AIRLINER COMMUNIQUE NO. 43, REV. I, OCTOBER, 1996THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL KING AIR METAL RETAINERWINDSHIELD IN PLACE OF THE 114-384020-1 AIRLINER FIBERGLASS RETAINER WINDSHIELD ON THEPILOT SIDE OF IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: STARTED USING NEW SURFACE SEALED COATED -17 WINDSHIELD IN THIS KIT AT KITSERIAL NUMBER: 463. CUSTOMER MAY DESIRE A -1 S AND -2 S WITH NEW COATEDWINDSHIELD.

NOTENOTENOTENOTE:::: IF YOU ARE CHANGING BOTH PILOT AND COPILOT WINDSHIELD, KIT 101-5041-1 SCONTAINS ENOUGH MATERIAL TO INSTALL BOTH WINDSHIELDS (EQUALS 2 EACH101-5041-3 S).

NOTENOTENOTENOTE:::: THIS WINDSHIELD KIT IS A REPLACEMENT FOR 101-384025-7 WINDSHIELD FOR U.K. BIRDGUARD WHEN REST OF 1900C CHAPTER 56-10-10 DETAILS ARE INSTALLED.

NOTENOTENOTENOTE:::: KIT 101-5041-3 S WILL BE REQUIRED FOR INSTALLATION OF THIS KIT BUT IS NOT PART OFTHIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY (NOTE:101-5044-1 S KIT IS PART OF 101-5041-3 S KIT).

WT. CHANGE : + 12 LBS @ STA 108 = + 1296 MOMENTEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)


KIT CATALOG

114-5043-2 SWINDSHIELD RH, KING AIR METAL RETAINER STYLE INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1751900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTER1900 AIRLINER COMMUNIQUE NO. 43, REV. I, OCTOBER, 1996THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL KING AIR METAL RETAINERWINDSHIELD IN PLACE OF THE AIRLINER 114-384020-2 FIBERGLASS RETAINER WINDSHIELD ON THECOPILOT SIDE ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS WINDSHIELD IS A REPLACEMENT FOR 101-384025-8 WINDSHIELD FOR UK BIRDGUARD WHEN THE REST OF 1900C IPC CHAPTER 56-10-10 DETAILS ARE ALSOINSTALLED.

NOTENOTENOTENOTE:::: IF ORDERING BOTH 114-5043-1 S AND 114-5043-2 S KITS, YOU COULD ORDER 1 EACH101-5041-1 S KIT (EQUALS 2 EA. 101-5041-3 S KITS) TO ACCOMPLISH INSTALLATION OFBOTH WINDSHIELDS.

NOTENOTENOTENOTE:::: KIT 101-5041-3 S WILL BE REQUIRED FOR INSTALLATION OF THIS KIT BUT IS NOT PART OFTHE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : + 12 LBS @ STA 108 = +1296 MOMENTEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

114-5044-1 PCARGO CONFIGURATION MODIFICATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-175THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT FOR CARGOONLY.

NOTENOTENOTENOTE:::: THIS INSTALLATION ENABLES YOU TO REVERSE THE OPERATION OF YOUR AIRCRAFTFROM TOTAL CARGO TO TOTAL PASSENGER OPERATION AS YOUR OPERATION DEMANDSEASON CHANGES OR TO MEET SPECIAL CHARTER OPERATION DEMANDS.

NOTENOTENOTENOTE:::: IF YOU DESIRE TO ADD INCREASE TO ZERO FUEL WEIGHT AT THE SAME TIME SEE -3 P,-5 P, -7 P OR -9 P KIT WHICH COVERS YOUR AIRCRAFT SERIAL NUMBER.

WT. CHANGE : -250 LBS.; MOMENT: -85781 IN.-LBS.EST. MAN/HRS: : 72 TO 96MEN : 2 (MEN)

114-5044-3 PCARGO CONFIGURATION AND ZERO FUEL WEIGHT ATA :1900C UB-1 THRU UB-74 FOR FAA POH

OPERATIONTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT FOR CARGO ONLYOPERATION AND TO ADD INCREASE TO THE ZERO FUEL WEIGHT TO 15,000 POUNDS.

NOTENOTENOTENOTE:::: MUST FURNISH AIRCRAFT SERIAL NUMBER WHEN ORDERING THIS KIT TO ENSURE YOUGET THE MOST CURRENT AND CORRECT POH FOR YOUR PARTICULAR AIRCRAFT.

NOTENOTENOTENOTE:::: IF YOU DESIRE ONLY THE COMPLETE CARGO CONFIGURATION MODIFICATION, SEE -1 PKIT.



KIT CATALOG

114-5044-5 PCARGO CONFIGURATION AND ZERO FUEL WEIGHT ATA :1900C-1 UB-1 THRU UB-74 FOR ICAO POH





114-5044-7 PCARGO CONFIGURATION AND ZERO FUEL WEIGHT ATA :1900C-1 UC-1 THRU UC-175 FOR FAA POHTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT FOR CARGO ONLYOPERATION AND TO ADD INCREASE TO THE ZERO FUEL WEIGHT TO 15,000 POUNDS.




114-5044-9 PCARGO CONFIGURATION AND ZERO FUEL WEIGHT ATA :1900C-1 UC-1 THRU UC-175 FOR ICAO POH






KIT CATALOG

114-5045-1 SZERO FUEL, 15,000 POUNDS MAXIMUM WEIGHT INSTALLATION ATA :1900C UB-1 THRU UB-74 FOR FAA POH

OPERATIONTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD SUPPLEMENT TO POH ON THEINCREASE IN MAXIMUM ZERO FUEL WEIGHT, AND TO INSTALL ZERO FUEL MAXIMUM WEIGHT DECAL.

NOTENOTENOTENOTE:::: IF YOU HAVE ORDERED KIT 114-5044-3 P, YOU WILL NOT HAVE TO ORDER THIS KIT AS ITIS PART OF THE 114-5044-3 P KIT.

NOTENOTENOTENOTE:::: FOR ICAO AIRCRAFT SEE -3 S KIT AND FOR 1900C-1 AIRCRAFT SEE -5 S OR -7 S KITS.NOTENOTENOTENOTE:::: MUST FURNISH AIRCRAFT SERIAL NUMBER WHEN ORDERING THIS KIT TO ENSURE YOU

GET THE CORRECT POH SUPPLEMENT FOR YOUR SPECIFIC AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)

114-5045-3 SZERO FUEL, 15,000 POUNDS MAXIMUM WEIGHT INSTALLATION ATA :1900C UB-1 THRU UB-74 FOR ICAO POH


NOTENOTENOTENOTE:::: IF YOU HAVE ORDERED KIT 114-5044-5 P, YOU DO NOT NEED TO ORDER THIS AS IT ISPART OF THE 114-5044-5 P KIT.

NOTENOTENOTENOTE:::: MUST FURNISH AIRCRAFT SERIAL NUMBER WHEN ORDERING THIS KIT TO ENSURE YOUGET THE MOST CURRENT AND CORRECT POH SUPPLEMENT FOR YOUR PARTICULARAIRCRAFT.

NOTENOTENOTENOTE:::: FOR FAA AIRCRAFT SEE -1 S KIT AND FOR 1900C-1 AIRCRAFT SEE -5 S OR -7 S KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)

114-5045-5 SZERO FUEL, 15,000 POUNDS MAXIMUM WEIGHT INSTALLATION ATA :1900C-1 UC-1 THRU UC-175 FOR FAA POH


NOTENOTENOTENOTE:::: FOR ICAO AIRCRAFT SEE -7 S KIT AND FOR 1900C AIRCRAFT SEE -1 S OR -3 S KITS.NOTENOTENOTENOTE:::: IF YOU HAVE ORDERED KIT 114-5044-7 P, YOU WILL NOT HAVE TO ORDER THIS KIT AS IT

IS PART OF THE 114-5044-7 P KIT.NOTENOTENOTENOTE:::: MUST FURNISH AIRCRAFT SERIAL NUMBER WHEN ORDERING THIS KIT TO ENSURE YOU

GET THE MOST CURRENT AND CORRECT POH SUPPLEMENT FOR YOUR PARTICULARAIRCRAFT.



KIT CATALOG

114-5045-7 SZERO FUEL, 15,000 POUNDS MAXIMUM WEIGHT INSTALLATION ATA :1900C-1 UC-1 THRU UC-175 FOR ICAO POH


NOTENOTENOTENOTE:::: IF YOU HAVE ORDERED KIT 114-5044-9 P, YOU WILL NOT HAVE TO ORDER THIS KIT AS ITIS PART OF THE 114-5044-9 P KIT.

NOTENOTENOTENOTE:::: MUST FURNISH AIRCRAFT SERIAL NUMBER WHEN ORDERING THIS KIT TO ENSURE YOUGET THE MOST CURRENT AND CORRECT POH SUPPLEMENT FOR YOUR PARTICULARAIRCRAFT.

NOTENOTENOTENOTE:::: FOR FAA AIRCRAFT SEE -5 S KIT AND FOR 1900C AIRCRAFT SEE -1 S OR -3 S KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)

114-5046-1SCREEN, AIR CONDITIONER CONDENSER SECTION ATA :1900 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 114-550023-1 OR 114-550234-1 OR114-550234-3 SCREEN WITH A 114-550234-5 SCREEN IN THE AIR CONDITIONER CONDENSER FUNNELINLET.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

114-5047-1INTERIOR LINER INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU U-174THIS KIT PROVIDES "INFORMATION ONLY" TO REPLACE THE INTERIOR ABOVE WL 105.5 BETWEEN FS183.25 AND FS 451.00. THIS IS NOT A STAND ALONE KIT. IT MUST BE INSTALLED AS A PART OF 114-0100-1CARGO CONFIGURATION KIT.WT. CHANGE : TBDEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5048-1SINGLE PASSENGER SEAT INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES "INFORMATION ONLY" TO INSTALL A SEAT TRACK ON RH SIDEWALL AT FS 143.00 TOFS 163.975. IT ALSO SHOWS THE POSITION FOR A SEAT WITH SHOULDER HARNESS LOCATED BEHINDTHE CO-PILOT FOR IN-SERVICE AIRCRAFT. THIS KIT IS NOT A STAND ALONE KIT. ITWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-5050-1EXTERIOR MARKING PLACARD ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6PENDING "MANDATORY" SB NO. 2741THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE EXTERIOR MARKINGSREGARDING DOOR OPENING PROCEDURES FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA3960 EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


114-5050-3EXTERIOR MARKING PLACARD ATA :1900 UA-1 THRU UA-3PENDING "MANDATORY" SB NO. 2741THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE EXTERIOR MARKINGSREGARDING DOOR OPENING PROCEDURES FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA3960 EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


114-5053-1A/C OVER PRESSURE SWITCH, SPARES ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES A SPARES REPLACEMENT FOR THE 114-555067-1 AIR CONDITIONER OVER PRESSURESWITCH ON ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5054-1BATTERY VALVE - INFORMATION ONLY ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-349THIS KIT PROVIDES "INFORMATION ONLY" FOR THE INSTALLATION OF THE 101-381009-1 VALVEASSEMBLY FOR THE BATTERY AIR INLET ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-5056-1OXYGEN MASK & MIC INSTALLATION ATA :1900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF CREW OXYGEN MASK MIC SELECTSWITCHES, NEW CREW OXYGEN MASKS, SMOKE GOGGLES AND CONTAINERS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

114-5057-1SWITCH & COVER INSTALLATION - ASYMMETRICAL FLAP ATA : 271900 UA-31900C UC-1 THRU UC-174, UB-1 THRU UB-741900C (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-439SB NO. 27-3528 - RSD A1016THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENVIRONMENTALLY SEALED SWITCH, ANDALSO INSTALL A COVER OVER THE SWITCH FOR THE FLAP ASYMMETRICAL SWITCH INSTALLATION FORINSERVICE AIRCRAFT. ONE KIT PROVIDES PARTS FOR BOTH THE LEFT AND RIGHT WINGS.

NOTENOTENOTENOTE:::: "222" LOCTITE THREADLOCKER ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPARATELY FROM ANY AUTHORIZED COMPANY OUTLET.


114-5058-0001UNIVERSAL JOINT REPLACEMENT, ELEVATOR TRIM CONTROL,ELECTRICAL

ATA :

1900 SERIES UA-2 AND UA-3, UB-1 THRU UB-74, UC-1THRU UC-174, UD-1 THRU UD-6, AND UE-1THRU UE-439. THIS KIT WAS PROTOTYPEDON UE-46

THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 114-524022-23 UNIVERSAL JOINT FORTHE ELECTRIC ELEVATOR TRIM CONTROL INSTALLATION WITH A COVERED UNIVERSAL JOINT FOR IN-SERVICE AIRCRAFT MODEL 1900. MODEL 1900C. AND MODEL 1900D.

NOTENOTENOTENOTE:::: IN ADDITION, COMPLIANCE WITH 14 CFR PART 23.25 AND PART 3.74 MUST BEMAINTAINED. (WEIGHT LIMIT VERSUS AIRCRAFT LOADING).



KIT CATALOG

114-5300-1FIRST AID INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174PENDING "OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE FIRST AID KIT FORCOMPLIANCE WITH FIRST AID REQUIREMENTS OF 14 CFR PART 121 ON REFERENCE AIRCRAFT.

NOTENOTENOTENOTE:::: INFORMATION KIT 114-0001-1 WILL FURNISH LIST: 14 CFR PART 121 KITS AND ETC.NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, FOLLOWING AS REQUIRED ITEMS: "EA9309

QT" ADHESIVE AND "17X005 PT" 1900 GRAY ACRYLIC LACQUER PAINT. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : +6 LBS; MOMENT: 1026 IN.-LBSEST. MAN/HRS: : 2MEN : 1 (MAN)

114-5302-1JAR-OPS CRASH AXE INSTALLATION ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A CRASH AXE WITH COVER TO THE RIGHTHAND COCKPIT PARTITION FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "242" LOCKTITE AND "EA939RNA" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : WT: 2.86 LBS; MOMENT: TBDEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

114-5310-1FIRE EXTINGUISHER INSTALLATION, CABIN ATA :1900C-1 UC-1 THRU UC-75THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE FIRE EXTINGUISHERFROM THE CABIN DOOR TO THE FWD SIDE OF THE FWD BAGGAGE PARTITION TO ELIMINATEINTERFERENCE OF LARGER BOTTLE ON THE CABIN DOOR WHEN USED ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5311-1FLASHLIGHT INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174PENDING "OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE FLASHLIGHT HOLDER.WT. CHANGE : 2 LBS; MOMENT 244 IN -LBSEST. MAN/HRS: : 1.5MEN : 1 (MAN)


KIT CATALOG

114-5312-1EMERGENCY EXIT LIGHT ATA :1900C UB-24 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL EMERGENCY EXIT LIGHTS INEXISTING LIGHT PANELS TO INCREASE AWARENESS OF EMERGENCY EXITS LOCATION ON ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 1.3 LBS.; MOMENT: 393 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5312-3EMERGENCY EXIT LIGHT ATA :1900C UB-1 THRU UB-23THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL EMERGENCY EXIT LIGHTS INEXISTING LIGHT PANELS TO INCREASE AWARENESS OF EMERGENCY EXITS LOCATION ON ALL IN-SERVICE AIRCRAFT. THIS KIT IS FOR LIGHT COVERS THAT ARE HELD IN PLACE WITH VELCRO.

NOTENOTENOTENOTE:::: "EA9309" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 1.3 LBS.; MOMENT: 393 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5313-3EMERGENCY EXIT LIGHT, JAR-OPS ATA :1900 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL EMERGENCY EXIT LIGHTS INEXISTING HEADLINER PANELS.

NOTENOTENOTENOTE:::: "XMH8680" ADHESIVE, "MS2047AD4","MS20470AD5" RIVETS REQUIRED, BUT NOTFURNISHED WITH KIT. PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZEDOUTLET.THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED FLIGHT MANUAL REVISION (ORSUPPLEMENT) HAS BEEN INCORPORATED. PROCURE SEPARATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

WT. CHANGE : WT: 5 LBS; MOMENT 1341 IN-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

114-5314-0001HARNESS INSTALLATION-SHOULDER, PILOT AND CO-PILOT ATA :1900 UA-2 & UA-31900D UB-1 THRU UB-47THIS KIT PROVIDES INFORMATION FOR THE INSTALLATION OF GUARDED ROTARY SEAT BELT BUCKLESON THE PILOT AND COPILOT SEATS. 1900 & 1900C AIRCRAFT.

MEN : N/A


KIT CATALOG

114-5314-0003HARNESS INSTALLATION-SHOULDER, PILOT AND CO-PILOT ATA :1900C UB-48 THRU UB-74 AND UC-1 THRU UC-1411900C-1(C-12J) UD-1 THRU UD-6THIS KIT PROVIDES INFORMATION FOR THE INSTALLATION OF GUARDED ROTARY SEAT BELT BUCKLESON THE PILOT AND COPILOT SEATS.MEN : N/A

114-5314-0005HARNESS INSTALLATION-SHOULDER, PILOT AND CO-PILOT ATA :1900C UC-142 THRU UC-1741900D UE-1 THRU UE-439THIS KIT PROVIDES INFORMATION FOR THE INSTALLATION OF GUARDED ROTARY SEAT BELT BUCKLESON THE PILOT AND COPILOT SEATS.

MEN : N/A

114-5500-1DUCT INSTALLATION, HEAT AND VENT AFT CABIN ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT THE AIRCRAFT FROMPASSENGER TYPE TO CARGO TYPE. THIS IS NOT A STAND ALONE KIT. IT MUST BE INSTALLED AS A PARTOF 114-0100-1 CARGO CONFIGURATION KIT.WT. CHANGE : TBDEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-5600-1OXYGEN SYSTEM INSTALLATION CARGO ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT CONTAINS INFORMATION ONLY REQUIRED TO MODIFY THE EXISTING OXYGEN SYSTEMINSTALLATION INTO A CARGO CONFIGURATION OXYGEN SYSTEM. THIS KIT IS NOT A STAND ALONE KIT.IT MUST BE INSTALLED AS PART OF 114-0100-1 CARGO CONFIGURATION KIT.WT. CHANGE : TBDEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-8004-1 SPOWER STEERING ACTUATOR - SPARES ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-22THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THEHYDRAULIC ACTUATOR 114-380045-1.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-8005-1 SLANDING GEAR INDICATOR SWITCH ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-36, UB-38 THRU UB-45SB NO. 2126 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED GEAR TRANSIT SWITCH ANDBRACKET.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-8006-1 SPOWER STEERING RELIEF VALVE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-46SB NO. 2131 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE HYDRAULIC RELIEF VALVE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

114-8010-1 SMAIN LANDING GEAR DOOR HINGE INSTALLATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-69SB NO. 2163 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LANDING GEAR DOOR HINGES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 2 (MEN)

114-8011-1 SPOWER STEERING POTENTIOMETER ATA :1900C UB-1 THRU UB-65SB NO. 2171 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE NOSE LANDING GEAR POWERSTEERING POTENTIOMETER.WT. CHANGE : N/AEST. MAN/HRS: : 13MEN : 1 (MAN)


KIT CATALOG

114-8013-1 SNOSE GEAR LINK INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-67THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE EXISTING NOSE GEARSTEERING LINK ASSEMBLY WITH A NEW LINK ASSEMBLY THAT UTILIZES A COVER BOOT FORENVIRONMENTAL PROTECTION OF THE LINK ASSEMBLY. THE NEW LINK ASSEMBLY DOES NOTINCORPORATE A

NOTENOTENOTENOTE:::: THIS KIT REPLACES 114-4019-1 S.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-8014-1 SPLACARD INSTALLATION, LANDING GEAR ACCUMULATOR ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTERSB NO. 2238 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PLACARD SHOWING HOW TO SERVICE THEHYDRAULIC LANDING GEAR ACCUMULATOR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-8015-1 SNOSE LANDING GEAR INSTALLATION - SPARES ATA :19001900C1900C-11900C-1 (C-12J)SB NO. 2102, REV. 3 OR SUBSEQUENTTHIS KIT IS THE SPARES REPLACEMENT FOR 114-820023-1 AND 114-820023-5 SHOCK ABSORBERASSEMBLIES.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-8017-1 SANTI-SKID BRAKE PUMP MOTOR INSTALLATION - SPARES ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER1900C-1 UC-1 THRU UC-64THIS KIT PROVIDES FOR SPARES REPLACEMENT OF 114-388004-1 OR 68-459 MOTOR AND PUMPASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

114-8018-1 SMAIN LANDING GEAR DOOR HINGE INSTALLATION ATA :1900CTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE MAIN LANDING GEAR DOOR HINGES.WT. CHANGE : N/AEST. MAN/HRS: : 16MEN : 2 (MEN)

114-8019-1 SPOWER STEERING BELLCRANK LUBRICATION FITTING, INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-74SB NO. 2354 OR SUBSEQUENTTHIS KIT PROVIDES "INFORMATION ONLY" FOR THOSE AIRCRAFT EQUIPPED WITH POWER STEERING.THE MODIFICATIONS NOTED IN KIT DRAWING ARE INTENDED TO IMPROVE THE SERVICE LIFE ANDPOWER STEERING OPERATION.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

114-8020-1ANTI SKID BRAKE PROVISIONS ATA :1900C-1 UC-43 AND UC-44 ONLYTHIS KIT PROVIDES INFORMATION ONLY FOR THE INSTALLATION OF PROVISIONS FOR ANTI-SKID BRAKESYSTEM ON MODEL 1900C-1 AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT MUST BE INSTALLED IN CONJUNCTION WITH THE INSTALLATION OF KIT 114-8017ON THESE TWO AIRCRAFT ONLY.


114-8021-1 SHYDRAULIC FILTER INSTALLATION POWER STEERING ATA :1900C-1 UC-1 THRU UC-181SB NO. 2404THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HYDRAULIC FILTER UNIONS IN THEPRESSURE AND RETURN LINES OF THE OPTIONAL POWER STEERING SYSTEM. THIS MOD IS INTENDEDTO PREVENT SYSTEM MALFUNCTIONS DUE TO CIRCULATING CONTAMINATION.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

114-8022-1 SLANDING GEAR, HYDRAULIC LINE FILTER INSTALLATION ATA :1900 UA-2 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-181THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF ADDITIONAL FILTERS WITHIN THELINES OF THE LANDING GEAR HYDRAULIC SYSTEM. THIS MOD IS INTENDED TO IMPROVE THERELIABILITY OF GEAR ACTUATION BY PREVENTING CIRCULATION CONTAMINATION FROM REACHING TWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

114-8023-1 SPOWER STEERING PUMP MOTOR ASSEMBLY ATA :1900THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE 114-388021-1 PUMP MOTORASSEMBLY WITH A 118-380005-1 PUMP ASSEMBLY ON IN-SERVICE AIRCRAFT EQUIPPED WITH THEOPTIONAL DECOTO POWER STEERING SYSTEM.

NOTENOTENOTENOTE:::: 114-388021-1 ASSEMBLY CONSISTS OF A -3 PUMP AND A -5 MOTOR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)

114-8023-3 SPOWER STEERING PUMP MOTOR ASSEMBLY ATA :1900 SERIESTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE 114-388021-1 PUMP MOTORASSEMBLY WITH A 118-380005-1 PUMP ASSEMBLY ON IN-SERVICE AIRCRAFT EQUIPPED WITH THEOPTIONAL DECOTO POWER STEERING SYSTEM AND THE HYDRO-AIRE ANTI-SKID BRAKE SYSTEM.

NOTENOTENOTENOTE:::: 114-388021-1 ASSEMBLY CONSISTS OF -3 PUMP AND -5 MOTOR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)

114-8025-1 SGUARD ASSEMBLY, NOSE WHEEL ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A GUARD ASSEMBLY ON THENOSE WHEEL ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : +2 LBS. @ 31.5 IN.EST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)


KIT CATALOG

114-8026-1 SNOSE LANDING GEAR BUSHING ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" TO REPLACE 114-820113-1 BUSHING IN THE NOSE GEAR TOPBRACE.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR USE, BUT ARE NOT FURNISHED ASPART OF KIT. ZINC CHROMATE PRIMER PART NUMBER TT-P1757 AND RETAININGCOMPOUND PART NUMBER LOCTITE 609. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOUCAN PROCURE LOCALLY.


114-8028-1BRAKE ANTI-SKID INSTALLATION FOR AIRCRAFT WITHOUT POWERSTEERING

ATA :

1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION FOR THE INSTALLATION OF ANTI-SKID BRAKE SYSTEMFOR IN-SERVICE AIRCRAFT WITHOUT POWER STEERING SYSTEM INSTALLED:

NOTENOTENOTENOTE:::: REQUIRED FOR KIT INSTALLATION BUT NOT FURNISHED WITH KIT: "EC-1239B1/2 QT","EC-1239B2 QT" OR "EC-1239B4 QT", OR "890B1/2 QT" CEMENT; "PR1440B1/2" OR"PR1440B1/2 6 OZ K" OR "PR1440B2 6 OZ KT" OR "PR1440B4 6 OZ TU" OR "PR1440 B-4"SEALER; "EC1300L GL" OR "EC1300L PT" OR "EC1300L QT" OR "EC1300L 1/2 PT" ADHESIVE;"EC847 QT" CEMENT; "PS890" SEALER OR EQUIVALENT AND 114-590000-15 FLIGHTMANUAL SUPPLEMENT.

WT. CHANGE : + 35 LBS.; MOMENT: + 3444 IN.-LBS.EST. MAN/HRS: : 300 TO 400MEN : 2 (MEN)

114-8028-3BRAKE ANTI-SKID INSTALLATION FOR AIRCRAFT WITH POWERSTEERING

ATA :

1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174THIS KIT PROVIDES PARTS AND INFORMATION FOR THE INSTALLATION OF ANTI-SKID BRAKE SYSTEMFOR IN-SERVICE AIRCRAFT WITH POWER STEERING SYSTEM INSTALLED.

NOTENOTENOTENOTE:::: FOR AIRCRAFT WITHOUT POWER STEERING SEE -1 KIT.NOTENOTENOTENOTE:::: REQUIRED FOR KIT INSTALLATION BUT NOT FURNISHED WITH KIT: "EC-1239B1/2 QT" OR

"EC-1239B2 QT" OR "EC-1239B4 QT" OR "890B1/2 QT" CEMENT; "PR1440B1/2" OR"PR1440B1/2 6 OZ K" OR "PR1440B2 6 OZ KT" OR "PR1440B4 6 OZ TU" OR "PR14401 B-4"SEALER; "EC1300L GL" OR "EC1300L PT" OR "EC1300L 1/2 PT" ADHESIVE; "EC847 QT"CEMENT; "PS890" SEALER OR EQUIVALENT AND 114-590000-15 FLIGHT MANUALSUPPLEMENT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : + 35 LBS.; MOMENT: + 3444 IN.-LBS.EST. MAN/HRS: : 300 TO 400MEN : 2 (MEN)


KIT CATALOG

114-8029-1BRAKE ASSEMBLY ATA :1900 UA-1 THRU UA-3*1900C UB-1 THRU UB-74*1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6*1900D UE-1 THRU UE-199PENDING "OPTIONAL" SB OR 1900 COMMUNIQUETHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN 114-388024-1 BRAKE ASSEMBLY.

NOTENOTENOTENOTE:::: *THESE MODELS HAD THE 114-8002-3, 114-8003-3, 114-8008-3 BRAKE ASSEMBLYINSTALLED WHEN THE AIRCRAFT WAS DELIVERED. IF CERTAIN CRITERIA ARE MET, THE114-8008-3 MAY HAVE BEEN INSTALLED ON AIRCRAFT AS A SPARES REPLACEMENT. DONOT INSTALL THE 114-388024-1 BRAKE ASSEMBLY ON AIRCRAFT IF 114-8002-3,114-8003-3, OR 114-8007-3 ARE INSTALLED IN ANY OF THE 4 BRAKE LOCATIONS.114-388024-1 BRAKE ASSEMBLY MAY BE USED AS SPARES REPLACEMENT FOR114-8008-3, AND MAY BE INSTALLED ON AIRCRAFT THAT HAS ONE OR MORE 114-8008-3BRAKE ASSEMBLY INSTALLED. DO NOT INTERMIX 114-388024-1 WITH 114-8008-3 BRAKEASSEMBLY.

NOTENOTENOTENOTE:::: 1 KIT PER BRAKE.WT. CHANGE : + 7 LBS; MOMENT: + 220 IN.-LBSEST. MAN/HRS: : 1 TO 2MEN : 1 (MAN)

114-8030-1WHEEL & BRAKE ASSY ATA :1900C, 1900, 1900C-1, 1900C-1 (C-12J),1900DWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9001-1 SQUICK ENGINE CHANGE, PT6A-65B FOR LH ENGINE (WITH ENGINE) ATA :1900 UA-1 THRU UA-31900C UB-31 AND AFTER SEE 114-9001-5 S KIT

WITH ENGINE AND -3 S FOR RHINSTALLATION ON ENGINES EQUIPPEDWITH -5 S KIT.

1900C UB-31 AND AFTER KIT LH ENGINEWITHOUT ENGINE SEE 114-9001-7 S KIT.

1900C-1 UC-2 AND AFTER SEE 114-9019/SERIESKITS.

1900D UE-1 AND AFTER SEE 129-9001-1 S KIT.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PT6A-65B ENGINE.

NOTENOTENOTENOTE:::: FOR THE RH ENGINE, KIT 114-9001-3 S IS REQUIRED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 2 (MEN)


KIT CATALOG

114-9001-3 SAIR CONDITIONING COMPRESSOR MOUNTING PROVISIONS ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERQUICK ENGINE CHANGE AIR CONDITIONING MOUNTING PROVISIONS FOR CONVERSION OF 114-9001-1 SAND/OR 114-9001-5 S KITS LH ENGINE FOR USAGE AS RH PT6A-65B QUICK ENGINE CHANGEINSTALLATION KIT.THIS KIT SHOULD BE PURCHASED IN CONJUNCTION WITH THE PURCHASE OF EITHER A 114-9001-1 S OR-5 S QEC KIT. PROOF OF PURCHASE OF EITHER OF THESE KITS SHOULD BE FURNISHED WHEN EVERTHIS KIT IS ORDERED.

NOTENOTENOTENOTE:::: ENGINE ASSEMBLY IS NOT FURNISHED WITH THIS KIT, IT IS FURNISHED AS PART OF THE114-9001-1 S AND -5 S KITS.

NOTENOTENOTENOTE:::: FOR SERVICE BULLETIN NO. 2128 AIR CONDITIONING COMPRESSOR MOUNTINGBRACKET KIT SEE KIT 114-5011-1 S.


114-9001-5 SQUICK ENGINE CHANGE, PT6A-65B ATA :1900C UB-31 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PT6A-65B ENGINE.

NOTENOTENOTENOTE:::: FOR THE RH ENGINE, KIT 114-9001-3 S IS REQUIRED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9001-7 SQUICK ENGINE CHANGE, PT6A-65B, LESS ENGINE ATA :1900 UA-4 AND AFTER1900C UB-31 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR QUICK ENGINE CHANGE PROVISIONS. THIS KIT DOESNOT PROVIDE A PT6A-65B ENGINE.

NOTENOTENOTENOTE:::: FOR RIGHT HAND ENGINE INSTALLATION, A -3 S KIT WILL BE REQUIRED.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9002-1 SENGINE HOT SECTION INSPECTION REPLACEMENT PARTS ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERTHIS KIT PROVIDES INSPECTION REPLACEMENT PARTS FOR THE HOT SECTION ON AIRPLANESEQUIPPED WITH PT6A-65B ENGINES.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

114-9003-1 SCOWLING REINFORCEMENT, ENGINE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-32"MANDATORY" SB NO. 2073THIS KIT PROVIDES PARTS AND INFORMATION TO REINFORCE THE ENGINE COWLINGS.WT. CHANGE : N/AEST. MAN/HRS: : 10MEN : 1 (MAN)

114-9003-3 SCOWLING REINFORCEMENT, ENGINE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-32"MANDATORY" SB NO. 2073THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE AIR INLET DUCTS AND REINFORCE THEENGINE COWLINGS.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)

114-9004-1 SCOWLING GUIDE PIN, FORWARD ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-40SB NO. 2076 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL INCREASED STRENGTH ENGINE COWLINGGUIDE PINS AND THEIR RECEPTACLESWT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-9005-1AIR INLET ANTI-ICE DUCT ATA :1900C, 1900WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9006-1 SOIL VENT PLUMBING RELOCATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-52SB NO. 2064 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE OIL VENT SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : 36MEN : 1 (MAN)


KIT CATALOG

114-9007-1 SAIR SCOOP ADAPTER AND IGNITION EXCITER ATA :1900 UA-31900C UB-1 THRU UB-28, UB-30 AND UB-32SB NO. 2062, REV. 1 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN AIR SCOOP ADAPTER AND RELOCATE THEIGNITION EXCITER TO REDUCE THE POSSIBILITY OF THE ENGINE FUEL LINES COMING IN CONTACT WITHENGINE COMPONENTS.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-9008-1INERTIAL SEPARATOR VANE, AIR INLET ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-50SB NO. 2082 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED VANE ASSEMBLIES IN THEINERTIAL SEPARATORS OF THE AIR INLETS TO BOTH ENGINESWT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)

114-9009-1 SSYNCHROPHASER CONTROL BOX ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-25SB NO. 2115 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED SYNCHROPHASER CONTROLBOX.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 1 (MAN)

114-9010-1 SFIRE DETECTION, ENGINE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-53SB NO. 2113 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED ENGINE FIRE DETECTIONSYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : 22MEN : 1 (MAN)


KIT CATALOG

114-9011-1 SCOWLING GUIDE PIN AND AFT LATCH, MID ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-62SB NO. 2122 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ENGINE COWLING GUIDE PINS AND THEIRRECEPTACLES AFT OF THE EXHAUST STACK, AND TO REINFORCE THE AFT LOWER LATCH ACCESS HOLEON THE MID COWLING.WT. CHANGE : N/AEST. MAN/HRS: : 20MEN : 1 (MAN)

114-9014-1EXHAUST STACK INSTALLATION ATA :1900C, 1900WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9015-1 SFUEL PRESSURE SWITCH TUBING INSTALLATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-62SB NO. 2161 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR AN IMPROVED LOW FUEL PRESSURE WARNINGSYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9016-1 PCOWLING INSTALLATION, LEFT ENGINE ATA :1900, 1900CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A COWLING ON THE LEFT HANDENGINE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMERT SUPPORTMEN : N/A

114-9016-3 PCOWLING INSTALLATION, RIGHT ENGINE ATA :1900, 1900CTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A COWLING ON THE RIGHT HANDENGINE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMERT SUPPORTMEN : N/A


KIT CATALOG

114-9016-5 PCOWLING INSTALLATION (LH AND RH) ATA :1900C UC-1 THRU UC-3THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY LH AND RH FIREWALL ONINSERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9017-1COWLING INSTL, INSTRUCTIONS ATA :1900C, 1900WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9018-1 PCOWLING REPAIR ATA :1900 SERIESTHIS KIT PROVIDES "INFORMATION ONLY" ON DRAWING OF TYPICAL REPAIR METHODS WHICH COULD BEUSED TO REPAIR AIRLINER COWLING INSTALLATIONS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9019-1 SQUICK ENGINE CHANGE-WET WING PT6A-65B WITH LH ENGINE ATA :1900C-1 UC-2 AND AFTER (WET-WING AIRCRAFT

ONLY)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR INSTALLING A PT6A-65B ENGINE ON IN-SERVICE AIRCRAFT, FOR LEFT HAND ENGINE INSTALLATION.

NOTENOTENOTENOTE:::: FOR EARLIER 1900 SEE 114-9001/SERIES KITS AND FOR 1900D SEE 129-9001-1 S.NOTENOTENOTENOTE:::: FOR RH ENGINE INSTALLATION 1EA 114-9019-3 S KIT WILL ALSO BE REQUIRED.NOTENOTENOTENOTE:::: FOR LH Q.E.C. LESS ENGINE KIT SEE 114-9019-5 S KIT.


114-9019-3 SQUICK ENGINE CHANGE FOR RH INSTALLATION OF -1 KITTED ENGINE ATA :1900C-1 UC-2 AND AFTER (WET-WING AIRCRAFT

ONLY)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY A -1 S OR -5 S KITTED ENGINEFOR RIGHT HAND ENGINE INSTALLATION, FOR LEFT HAND ENGINE INSTALLATION.

NOTENOTENOTENOTE:::: THIS KIT COMES WITHOUT ENGINE AND PROVIDES AIR CONDITIONER AND ASSOCIATEDPARTS AND ACCESSORIES FOR THE RIGHT HAND ENGINE.



KIT CATALOG

114-9019-5 SQUICK ENGINE CHANGE PT6A-65B WET WING 1900C-1 WITHOUT LHENGINE

ATA :

1900C-1 UC-2 AND AFTER (WET-WING AIRCRAFTONLY)

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR INSTALLING A PT6A-65B CUSTOMERENGINE OBTAINED FROM P AND W CANADA OR ETC. FOR USE ON IN-SERVICE AIRCRAFT, FOR LEFTHAND ENGINE INSTALLATION.

NOTENOTENOTENOTE:::: THIS KIT COMES WITHOUT ENGINE AND PROVIDES AIR CONDITIONER AND ASSOCIATEDPARTS AND ACCESSORIES FOR THE RIGHT HAND ENGINE.

NOTENOTENOTENOTE:::: TO USE ENGINE ON RH SIDE YOU WOULD ALSO HAVE TO PROCURE 114-9015-3 S KIT INADDITION TO THIS KIT. SEE 114-9019-1 S FOR KIT WITH LH ENGINE.

NOTENOTENOTENOTE:::: FOR EARLIER 1900’S SEE 114-9001/SERIES KITS AND FOR 1900D SEE 129-9001-1 S THEMODEL 1900C-1. AND AFTER, FOR LEFT HAND ENGINE INSTALLATION.


114-9020-1 SICE AND RAIN PROTECTION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-74SB NO. 2258 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION FOR RELOCATION OF THE BLEED AIR SHUT-OFF VALVEFOR ICE AND RAIN PROTECTION.WT. CHANGE : N/AEST. MAN/HRS: : 6MEN : 2 (MEN)

114-9021-1 STUBE BREAKAGE WARNING INSTALLATION, BLEED AIR ATA :1900, 1900CTHIS KIT PROVIDES TYPICAL REPAIR "INFORMATION ONLY" WHICH COULD BE USED TO REPAIR BLEEDAIR DUCT FAILURE INDICATION SYSTEM INSTALLATIONS.

NOTENOTENOTENOTE:::: IF ALL MATERIAL REQUIRED TO ACCOMPLISH THESE REPAIRS IS NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

114-9022-1 SBRAKE DEICE MODIFICATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-54SB NO. 2264 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NEEDED TO RELOCATE THE BRAKE DEICE SHUTOFFVALVE TO A LOCATION WHICH ALLOWS IN-SERVICE REPLACEMENT OF THE VALVE WITHOUT REMOVALOF THE ENGINE COWLING.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

114-9023-1 SDEICE BRUSH BLOCK RELOCATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE PROP DEICE BRUSH BLOCK TO ALOCATION THAT WILL REDUCE THE DIRT AND GRIME ON THE BRUSH BLOCK.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)

114-9024-1 SINLET DUCT REINFORCEMENT ATA :1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" TO REINFORCE THE AIR INLET DUCT FLOOR THAT WILLINCREASE THE DUCT STRENGTH ON ANY AIRLINER EQUIPPED WITH 114-9016-1 P AND -3 P KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

114-9025-1 SFUEL FIREWALL SHUTOFF VALVE REPLACEMENT ATA :1900 UA-1 THRU UA-31900C UB-1 AND AFTERSB NO. 2307 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE FIREWALL SHUTOFF VALVEWITH AN IMPROVED FIREWALL SHUTOFF VALVE, FOR ONE SIDE ONLY.WT. CHANGE : N/AEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

114-9026-3 SFUEL FLOW INDICATOR TOTALIZER SYSTEM INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2355 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A FOXBORO FUEL TOTALIZER ANDFUEL FLOW INDICATOR SYSTEM ON IN-SERVICE AIRCRAFT.WT. CHANGE : + 2.3 LBS @ 72.61"EST. MAN/HRS: : 16MEN : 1 (MAN)

114-9026-5 SFUEL FLOW INDICATOR SYSTEM INSTALLATION ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-741900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2355 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A FOXBORO FUEL FLOWINDICATOR SYSTEM ON INSERVICE AIRCRAFT.WT. CHANGE : + 1.3 LBS @ 35.38"EST. MAN/HRS: : 14MEN : 1 (MAN)

114-9026-7 SFUEL TOTALIZER INDICATOR SYSTEM INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2355 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A FOXBORO FUEL TOTALIZERSYSTEM ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT 114-9026-5 S INSTALLING FOXBORO FUEL FLOW INDICATOR SYSTEM MUST HAVEBEEN INSTALLED PRIOR TO INSTALLATION OF THIS KIT.

WT. CHANGE : + 1.1 LBS @ 124.55"EST. MAN/HRS: : 6MEN : 1 (MAN)

114-9027-1 SFLEX HOSE ASSEMBLY, ENGINE ATA :1900, 1900CTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FLEX HOSE ASSEMBLY ON AIRCRAFT WITH D3STYLE EXHAUST STACKS FOR AIRCRAFT WITH PERFORMANCE KIT (114-4013-1) INSTALLED ONLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

114-9028-1 SENGINE TRUSS SUPPORT ASSEMBLY ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERTHIS KIT PROVIDES REQUIRED "INFORMATION ONLY" ON HOW TO BUILD AN ENGINE TRUSS SUPPORTASSEMBLY THAT IS TO BE USED DURING ENGINE BUILDUP IN THE FIELD. THIS SUPPORT IS TO INSURETHAT THE FIREWALL ATTACH POINTS MAINTAIN THEIR ALIGNMENT AFTER BUILD-UP.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

114-9029-1 SLANDING GEAR DOOR HINGE ATA :1900, 1900C ALLTHIS KIT PROVIDES REQUIRED "INFORMATION ONLY" TO FABRICATE AND INSTALL SCREW RETAINEDMAIN LANDING DOOR HINGE PINS. IF MATERIAL REQUIRED FOR THIS INSTALLATION IS NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9030-1 SENGINE COWLING MODIFICATION ATA :1900C-1 UC-1 THRU UC-9, UC-11 THRU UC-14,

UC-17, UC-19, UC-20, UC-22 THRU UC-32,UC-34 THRU UC-36, UC-38, UC-40 THRUUC-54

SB NO. 2319 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY ENGINE COWLING ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9031-1 SPLACARD INSTRUCTIONS, FUEL TANK ATA :1900 UA-2, UA-319000C UB-1 THRU UB-74THIS KIT PROVIDES A REPLACEMENT VINYL DECAL, TO CHANGE THE LEFT AND RIGHT FUEL TANKCAPACITY TO SHOW BOTH GALLONS AND LITERS IN ACCORDANCE WITH ICAO REQUIREMENTS, FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 1 (MAN)


KIT CATALOG

114-9032-1 SDYNAMIC PROPELLER BALANCING PROVISIONS ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1501900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2375 AND 1900 COMMUNIQUE NO. 25THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL PROVISIONS FOR DYNAMICALLYBALANCING THE PROPELLER ASSEMBLY. INSTALLED PROVISIONS ARE FOR USE WITH THE CHADWICK-HELMUTH MODEL 8500 OR 192A SYSTEMS.

NOTENOTENOTENOTE:::: KIT 114-9023 MUST BE INSTALLED PRIOR TO OR IN CONJUNCTION WITH INSTALLATIONOF THIS 114-9032-1 S KIT.

NOTENOTENOTENOTE:::: FOR ALTERNATE PROP BALANCE INSTALLATION, FOR GROUND USE ONLY, WITHCONTROL BOX AND CONNECTORS INSTALLED UNDER THE FLOOR BOARD, SEE KIT114-9032-3 S WITH PARTS OR 114-9032-5 S "INFORMATION ONLY" KIT. BALANCING USINGADDED PROP RPM SENSORS. THE EQUIPMENT INTERCONNECT IS THRU A SINGLECONNECTOR LOCATED IN THE FORWARD RH COCKPIT SIDEWALL.

NOTENOTENOTENOTE:::: THIS KIT INSTALLS WIRING AND COMPONENTS REQUIRED FOR PROPELLER.NOTENOTENOTENOTE:::: BATTERY CHARGER UNITS 8412(120SYS) AND 8413(440SYS) NOT INCLUDED WITH KIT AS

1 OPERATOR CAN USE 1 BATTERY CHARGER FOR HIS ENTIRE FLEET SUPPORT NEEDS.WT. CHANGE : WT: + 10.9 LBS; MOMENT: +2272 IN.-LBSEST. MAN/HRS: : 16MEN : 1 (MAN)

114-9032-3 SDYNAMIC PROPELLER BALANCING PROVISIONS ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1501900C-1 (C-12J) UD-1 THRU UD-61900 AIRLINER COMMUNIQUE NO. 25THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL PROVISIONS FOR DYNAMICALLYBALANCING THE PROPELLER ASSEMBLY. INSTALLED PROVISIONS ARE FOR USE WITH THE CHADWICK-HELMUTH MODEL 8500 OR 192A SYSTEMS UTILIZING APPROPRIATE WIRING HARNESS PROVIDED BY

NOTENOTENOTENOTE:::: THIS KIT INSTALLS WIRING AND COMPONENTS REQUIRED FOR PROPELLER BALANCINGUTILIZING EXISTING PROP SYNCHROPHASER SENSOR PICK-UPS. THIS KIT'S EQUIPMENTINTERCONNECT IS THRU AN EXISTING CONNECTOR ON THE PROP SYNCHROPHASERCONTROL BOX AND CONNECTORS INSTALLED UNDER THE CABIN FLOOR. THIS KIT ISFOR GROUND USE ONLY.

NOTENOTENOTENOTE:::: FOR "INFORMATION ONLY" KIT SEE 114-9032-5 S AND FOR KIT THAT CAN BE USED BOTHIN FLIGHT OR ON THE GROUND SEE 114- 9032-1 S KIT.

NOTENOTENOTENOTE:::: BATTERY CHARGER UNITS 8412(120SYS) AND 8413(440SYS) NOT INCLUDED WITH KIT AS1 OPERATOR CAN USE 1 BATTERY CHARGER FOR SUPPORT OF HIS ENTIRE FLEET.

WT. CHANGE : WT: + 7.2 LBS; MOMENT: + 1635 IN.-LBSEST. MAN/HRS: : 12 TO 14MEN : 1 (MAN)


KIT CATALOG

114-9032-5 SDYNAMIC PROPELLER BALANCING PROVISIONS ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1501900C-1 (C-12J) UD-1 THRU UD-6AIRLINER COMMUNIQUE NO. 25THIS KIT PROVIDES "INFORMATION ONLY" ON WHAT IS REQUIRED TO INSTALL PROVISIONS FORDYNAMICALLY BALANCING THE PROPELLER ASSEMBLY. THE INSTALLED PROVISIONS WOULD BE FORUSE WITH THE CHADWICK-HELMUTH MODEL 8500 OR 192A SYSTEM, UTILIZING APPROPRIATE WIRING HA

NOTENOTENOTENOTE:::: SEE 114-9032-3 S KIT FOR WITH PARTS AND/OR 114-9032-1 S KIT FOR KIT THAT CAN BEUSED BOTH IN FLIGHT OR ON THE GROUND AND ABOUT BATTERY CHARGERS.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES "INFORMATION ONLY" TO ACCOMPLISH INSTALLATION OF THE114-9032-3 S KIT CONFIGURATION. NO HARDWARE IS FURNISHED WITH THE KIT.HARDWARE IS TO BE PROCURED LOCALLY. CHADWICK-HELMUTH OR FABRICATED BYOPERATOR AS SHOWN AND NOTED ON THIS DRAWING. "THIS KIT IS FOR GROUND USEONLY!"


114-9033-1 SENGINE TRUSS ASSEMBLY ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 AND AFTERSB NO. 2255 OR SUBSEQUENTTHIS KIT PROVIDES "INFORMATION ONLY" FOR INSPECTION OF THE ENGINE TRUSS ASSEMBLY FORCRACKS AND REPAIR.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

114-9034-1 SSTARTER GENERATOR REPLACEMENT ATA : 271900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 AND AFTER"OPTIONAL" SB NO. 2389THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE EXISTING STARTER GENERATORWITH A 23078-019 STARTER GENERATOR AND TO MODIFY THE AIR SCOOP TO IMPROVE COOLING AIRFLOW.

NOTENOTENOTENOTE:::: KIT INSTALLS IMPROVED STARTER GENERATOR USED ON 1900D, UE-1 AND AFTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 10MEN : 1 (MAN)


KIT CATALOG

114-9035-1 SPROPELLER DYNAMIC BALANCING ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1511900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2375THIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO MODIFY THE COWLING AND WHERE TO ROUTEWIRING FOR DYNAMIC PROPELLER BALANCING USING CHADWICK HELMUTH MODEL 8500 OR 192ASYSTEMS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

114-9036-1 SENGINE TRUSS INSTALLATION - SPARES ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1561900C-1 (C-12J) UD-1 THRU UD-6"MANDATORY" SB NO. 2255, REV. 6 AND 1900 AIRLINER COMMUNIQUE NO. 25THIS KIT PROVIDES FOR SPARES REPLACEMENT OF THE LEFT OR RIGHT 118-910025-1, -37, AND -121ENGINE TRUSS ASSEMBLY ON IN-SERVICE AIRCRAFT WITHOUT THE 118-910033-93 BLEED AIR DUCTINSTALLED.

NOTENOTENOTENOTE:::: TRUSS FOR THIS KIT NO LONGER AVAILABLE, IF YOU REQUIRE THIS KIT, SEE 114-9045-3KIT. PLEASE NOTE, MOST AIRCRAFT NOW HAVE ABOVE DUCT ON AIRCRAFT AND IF SOWILL NEED TO SEE 114-9045-1 OR -5 KIT DEPENDING ON AIRCRAFT SERIAL NUMBER ANDTRUSS CURRENTLY ON AIRCRAFT. YOU CAN NOT INSTALL NEW 129-910047-1 OR -13TRUSS ON AIRCRAFT, WITHOUT FIRST INSTALLATION OF 114-9045 KIT. SEE SERVICEBULLETIN NO. 2255, REV. VIII FOR LATEST TRUSS INFORMATION AND DELETION OF THISKIT.

WT. CHANGE : 6 LBS, MOMENT:1535 IN.-LBS.EST. MAN/HRS: : 6MEN : 2 (MEN)

114-9036-3 SENGINE TRUSS INSTALLATION - SPARES ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1561900C-1 (C-12J) UD-1 THRU UD-6"MANDATORY" SB NO. 2255, REV. 6, APRIL, 1994, AND 1900 AIRLINER COMMUNIQUE NO. 25THIS KIT PROVIDES FOR SPARES REPLACEMENT OF THE LEFT OR RIGHT 118-910025-1, -37, AND -121ENGINE TRUSS ASSEMBLY ON INSERVICE AIRCRAFT WITH THE 118-910033-93 BLEED AIR DUCTINSTALLED.

NOTENOTENOTENOTE:::: TRUSS FOR THIS KIT NO LONGER AVAILABLE, TOOLING REWORKED TO MANUFACTURETHE NEW PRODUCTION TRUSS. SEE 114-9045-1, -3, OR -5 KITS ON SSTX AND ORDER THEKIT FOR YOUR AIRCRAFT AND ETC.

WT. CHANGE : 6 LBS.: MOMENT: 1535 IN.-LBS.EST. MAN/HRS: : 6MEN : 2 (MEN)


KIT CATALOG

114-9037-1 STURBINE AND PROP RPM INDICATOR CHANGE INSTALLATION ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE EXISTING TURBINE ANDPROPELLER TACHOMETERS WITH P AND G INSTRUMENTS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 10MEN : 1 (MAN)

114-9038-1 SENGINE INSTRUMENT AIR MODIFICATION ATA :1900 UA-2, UA-3 WITH 114-90161900C UB-1 THRU UB-74 WITH 114-90161900C-1 UC-1 THRU UC-1561900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2398THIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE HOT AIR TO THE INSTRUMENT AIR LINE LHSIDE ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 16MEN : 1 (MAN)

114-9038-3 SENGINE INSTRUMENT AIR MODIFICATION ATA :1900 UA-2, UA-3 WITH 114-90161900C UB-1 THRU UB-74 WITH 114-90161900C-1 UC-1 THRU UC-1561900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2398THIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE HOT AIR TO THE INSTRUMENT AIR LINE RHSIDE ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 16MEN : 1 (MAN)


KIT CATALOG

114-9038-5 SENGINE INSTRUMENT AIR MODIFICATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-157 AND AFTER1900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2398THIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE HOT AIR TO THE INSTRUMENT AIR LINE LHSIDE ON IN-SERVICE AIRCRAFT WITH 118-910033-93 DUCT ASSEMBLY INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 16MEN : 1 (MAN)

114-9038-7 SENGINE INSTRUMENT AIR MODIFICATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-157 AND AFTER1900C-1 (C-12J) UD-1 THRU UD-6SB NO. 2398THIS KIT PROVIDES PARTS AND INFORMATION TO PROVIDE HOT AIR TO THE INSTRUMENT AIR LINE RHSIDE ON INSERVICE AIRCRAFT WITH 118-910033-93 DUCT ASSEMBLY INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 16MEN : 1 (MAN)

114-9039-1 SENGINE INSTRUMENT AIR MODIFICATION ATA :1900C-1 UC-49, UC-61, UC-83, UC-94, UC-95, UC-99,

UC-136THIS KIT PROVIDES "INFORMATION ONLY" TO INSTALL AN ORIFICE, A DRAIN HOLE, AND ADDITIONALTHERMAL INSULATION TO THE INSTRUMENT AIR PLUMBING ON AIRCRAFT PREVIOUSLY MODIFIED PERKITS 114-9038-1 OR 114-9038-3.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

114-9040-1 SPROP BALANCER, 8500C ANALYZER SYSTEM ATA :1900 SERIES ALLAIRLINER COMMUNIQUE NO. 25THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL MODEL 1900C BALANCERSYSTEM EQUIPMENT REQUIRED FOR DYNAMIC PROPELLER BALANCING ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE KIT 114-9040-3 S FOR MODEL 192A BALANCING EQUIPMENT.WT. CHANGE : N/AEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)


KIT CATALOG

114-9040-3 SPROP BALANCER, 192A ANALYZER SYSTEM ATA :1900 SERIES ALLAIRLINER COMMUNIQUE NO. 25THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL MODEL 192A BALANCER SYSTEMEQUIPMENT REQUIRED FOR DYNAMIC PROPELLER BALANCING ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE KIT 114-9040-1 S FOR MODEL 8500C BALANCING EQUIPMENT.WT. CHANGE : N/AEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

114-9041-1 SPNEUMATIC SYSTEM HEATERS ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ELECTRICALLY HEATEDINSTRUMENT AIR PNEUMATIC REGULATOR, DEICE VALVE, AND HEATER FOR THE VACUUM EJECTOR ONIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT. THIS KIT CONTAINS 2 HEATERS, 1 REGULATOR, 1 DEICE VALVE,AND REQUIRED INSTALLATION HARDWARE AND WIRING.


114-9041-3 SPNEUMATIC SYSTEM HEATERS ATA :1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ELECTRICALLY HEATEDINSTRUMENT AIR PNEUMATIC REGULATOR, DEICE VALVE, AND HEATER FOR THE VACUUM EJECTOR ONIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT. THIS KIT CONTAINS 2 HEATERS, 1 REGULATOR, 1 DEICE VALVE,AND REQUIRED INSTALLATION HARDWARE AND WIRING.


114-9042-1 STORQUE TRANSMITTER INSTALLATION - SPARES ATA : 251900 UA-1 THRU UA-31900C UB-1 THRU UB-41SB NO. 2465THIS KIT CONTAINS THE PARTS NECESSARY TO INSTALL A REPLACEMENT TORQUE TRANSMITTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

114-9043-1 SHEATERS ELECTRIC PNEUMATIC SYSTEM ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6"RECOMMENDED" SB NO. 2539THIS KIT PROVIDES PARTS AND INFORMATION FOR THE INSTALLATION OF ELECTRIC HEATEDINSTRUMENT AIR PNEUMATIC REGULATOR AND ASSOCIATED WIRING TO IMPROVE THE RELIABILITY OFTHE PNEUMATIC SYSTEM BY PREVENTING THE FREEZING OF ANY MOISTURE IN THE PNEUMATICREGULAT

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT. FOR MODEL 1900D SEE 114-9043-3 S KIT.NOTENOTENOTENOTE:::: FMS 114-590021-145 NOT INCLUDED IN KIT, NEED TO ORDER SEPARATELY.


114-9043-3 SHEATERS ELECTRIC PNEUMATIC SYSTEM ATA :1900D UE-1 AND AFTER"RECOMMENDED" SB NO. 2539THIS KIT PROVIDES PARTS AND INFORMATION FOR THE INSTALLATION OF ELECTRIC HEATEDINSTRUMENT AIR PNEUMATIC REGULATOR AND ASSOCIATED WIRING TO IMPROVE THE RELIABILITY OFTHE PNEUMATIC REGULATOR ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ONE KIT PER AIRCRAFT. FOR 1900 AND 1900C AIRCRAFT, SEE KIT 114-9043-1 S.WT. CHANGE : N/AEST. MAN/HRS: : 40 TO 48MEN : 1 (MAN)

114-9044-1 SPROP DEICE HEAVY DUTY BRUSH BLOCK INSTALLATION WITHIMPROVED SLIP RING

ATA :

1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6"RECOMMENDED" SB NO. 2571THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HEAVY DUTY BRUSH BLOCKS AND SLIP RINGSFOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE -3 KIT FOR LESS SLIP RING KIT.NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 2 FOR ADDITIONAL INFORMATION.



KIT CATALOG

114-9044-3 SBRUSH BLOCK, HEAVY DUTY, PROP DEICE LESS SLIP RING ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6"MANDATORY" SB NO. 2571 (SEE -1 S FOR KIT WITH IMPROVED SLIP RINGS ALSO)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HEAVY DUTY BRUSH BLOCKS LESS SLIP RINGCHANGE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 2 FOR ADDITIONAL INFORMATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

114-9045-1ENGINE TRUSS REPLACEMENT WITH -93 BLEED AIR DUCT ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-166"MANDATORY" SB 2255, REV. 9THIS KIT PROVIDES A SPARES REPLACEMENT FOR THE LEFT OR RIGHT 118-910025-1, -37 AND -121ENGINE TRUSS ON THE ABOVE IN-SERVICE AIRCRAFT WITH 118-910033-93 BLEED AIR DUCT INSTALLEDPER KIT, 114-9038-1 AND -3, REFERENCE SB NO. 2398WT. CHANGE : + 11 LBS.; MOMENT: + 2815 IN.-LBS.EST. MAN/HRS: : 10MEN : 1 (PER ENGINE) (MEN)

114-9045-3ENGINE TRUSS REPLACEMENT 1900, 1900C AIRCRAFT WITHOUT -93 B/ADUCT

ATA :

1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-166"MANDATORY" SB NO. 2255, REV. 9THIS KIT PROVIDES A SPARES REPLACEMENT FOR THE LEFT OR RIGHT 118-910025-1, 118-910025-37 AND-121 ENGINE TRUSS ASSEMBLY ON THE IN-SERVICE AIRCRAFT WITHOUT 118-910033-93 BLEED AIR DUCTINSTALLED.

NOTENOTENOTENOTE:::: * 1 KIT PER ENGINEWT. CHANGE : + 11 LBS.; MOMENT: + 2815 IN.-LBS.EST. MAN/HRS: : 10MEN : 1 (PER ENGINE) * (MEN)


KIT CATALOG

114-9045-5ENGINE TRUSS REPLACEMENT 1900, 1900C AIRCRAFT WITH 114-9036 ATA :1900 UA-2, UA-3*1900C UB-1 THRU UB-74*1900C-1 UC-1 THRU UC-156*, UC-157 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6*1900D UE-1 THRU UE-166"MANDATORY" SB NO. 2255, REV. 9(WITH KIT 114-9036-1 S OR 114-9036-3 S AND KIT 114-9038-1 S INSTALLED).THIS KIT PROVIDES A SPARES REPLACEMENT FOR THE LEFT OR RIGHT 129-910032-79 ENGINE TRUSSASSEMBLY ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: * 1 KIT PER ENGINEWT. CHANGE : + 5 LBS.; MOMENT: + 1280 IN.-LBS.EST. MAN/HRS: : 10MEN : 1 (PER ENGINE) * (MEN)

114-9046-1FORMER INSTALLATION, LOWER AFT NACELLE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-2 THRU UE-298THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FORMER IN THE AFT LOWER NACELLE THATPROVIDES ADDITIONAL CONTACT AREA FOR THE AFT END OF THE MAIN LANDING GEAR DOORS ON IN-SERVICE AIRCRAFT.WT. CHANGE : ARM: MOMENT: NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

114-9047-1PROPELLER SYNCHROPHASER DEACTIVATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-150THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO DEACTIVATE THE PROPELLERSYNCHROPHASER ON IN-SERVICE AIRCRAFT WHICH DO NOT HAVE PROPELLER DYNAMIC BALANCINGKIT 114-9032-1, -3, OR -5 INSTALLED.WT. CHANGE : WT: ARM: MOMENT: NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

118-0000-1EXTERIOR MARKING INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174"OPTIONAL" SB NO. 2727THIS KIT PROVIDES FOR CONTRASTING EXTERIOR EMERGENCY EXIT MARKINGS AND TWO INCHCONTINUOUS COLOR BANDS AROUND AIRSTAIR DOOR AND EACH EMERGENCY EXIT.

NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT, WILL NEED COLOR AS REQUIRED - U4386 QT, U4378 QT, U4315QT, OR U4533 QT (2099 QT). IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.

NOTENOTENOTENOTE:::: YOU MAY NEED ONE OF THE FOLLOWING 4 PAINTS, DEPENDING ON THE COLOR OF THEBANDS, AND EXTERNAL MARKINGS THAT SHOW THE MEANS OF OPENING THEEMERGENCY EXITS. MUST CONTRAST WITH THE SURROUNDING FUSELAGE AREA.


118-0000-3EXTERIOR MARKING INSTALLATION ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-174"OPTIONAL" SB NO. 2727THIS KIT PROVIDES FOR CONTRASTING EXTERIOR EMERGENCY EXIT MARKINGS AND TWO INCHCONTINUOUS COLOR BANDS AROUND AIRSTAIR DOOR AND EACH EMERGENCY EXIT.


NOTENOTENOTENOTE:::: YOU MAY NEED ONE OF THE FOLLOWING 4 PAINTS, DEPENDING ON THE COLOR OF THEBANDS, AND EXTERNAL MARKINGS THAT SHOW THE MEANS OF OPENING THEEMERGENCY EXITS. MUST CONTRAST WITH THE SURROUNDING FUSELAGE AREA.


118-3001-1 SRELOCATE AUTOPILOT ELECTRICAL POWER SUPPLY ATA :1900C-1 ALLTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR THE RELOCATION OF THE EXISTINGAUTOPILOT CIRCUIT BREAKERS FOR THE GEN NO. 2 BUS TO THE NO. 2 AVIONICS BUS ON IN-SERVICEAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)


KIT CATALOG

118-3002-1ALTIMETER INSTL ATA :1900C-1 UC-3, UC-9, UC-11, UC-12, UC-13,

UC-14, UC-22, UC-37, UC-38 AND UC-39THIS KIT PROVIDES INFORMATION NECESSARY TO REPLACE EXISTING ALTIMETER LOCATED ONCOPILOT SIDE OF THE INSTRUMENT PANEL. PARTS REQUIRED MAY BE PURCHASED FROM RAYTHEONAIRCRAFT OR MAY BE OBTAINED LOCALLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

118-3003-1GROUND COLLISION AVOIDANCE SYSTEM ATA :1900C-1 (C-12J) UD-1 THRU UD-6THIS KIT CONTAINS PARTS AND INFORMATION TO PROVIDE FOR INSTALLATION OF A GROUND COLLISIONAVOIDANCE SYSTEM IN THE FOLLOWING AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

118-3004-1 MATTITUDE INDICATOR INSTALLATION, STANDBY GYRO WITH BATTERYPACK

ATA :

1900C-1 UC-69, UC-73, UC-80, UC-109, UC-111,UC-115, UC-121, UC-131, UC-163, UC-172,UC-173

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A J.E.T. AI-804AF STANDBY GYROWITH PS-835C BATTERY PACK ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALODINE 1200 IS REQUIRED BUT NOT FURNISHED WITH THIS KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT 114-590021-123 IS REQUIRED TO MAKE THIS KITINSTALLATION COMPLETE, BUT IS NOT PART OF THE KIT.

WT. CHANGE : + 13 LBS. @ 77.62"EST. MAN/HRS: : 36 TO 48MEN : 1 (MAN)

118-4010-1WING CENTER SECTION RH AFT RIB, CABLE MOD ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" TO ELIMINATE POSSIBLE AILERON CABLE INTERFERENCE ONTHE RIGHT HAND AFT WING RIBS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EC2084 SEALER 5 OZ OR EQUIVALENT AND EA9309NA OR EA9309 QT SEALANT WILL BEREQUIRED FOR USE. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



KIT CATALOG

118-4011-1INSPECTION PROVISIONS, MAIN SPAR, LOWER CENTER SECTION ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLING INSPECTION DOOR PROVISIONS AT THEFRONT SPAR ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MS20426AD3, MS20426B3 RIVETS REQUIRED BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


118-4012-1INSTALLATION, COLD EXPANSION OF HOLES ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION FOR THE REPLACEMENT OF FASTENERS AND COLDEXPANDING THE HOLES IN THE CENTER SECTION REAR SPAR, AS REQUIRED FOR THE 30,000 HOURWING INSPECTION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CR3242-4 RIVET REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 2 LBS.; MOMENT: 652 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

118-4012-3INSTALLATION, COLD EXPANSION OF HOLES ATA :1900D UE-2 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR THE REPLACEMENT OF FASTENERS AND COLDEXPANDING THE HOLES IN THE CENTER SECTION REAR SPAR, AS REQUIRED FOR THE 17,500 HOURWING INSPECTION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CR3242-4 RIVET REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 2 LBS.; MOMENT: 652 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

118-4013-1ROD END INSTALLATION, ASYMETRICAL FLAP ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74, UC-1 THRU UC-1741900C (C-12J) UD-1 THRU UD-81900D UE-1 THRU UE-427THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 101-521030 INBOARD FLAP LINK IN THEFLAP (ASYMETRIC) SAFETY SWITCH SYSTEM ON INSERVICE AIRCRAFT. THIS KIT PROVIDES PARTS FORBOTH THE LEFT AND RIGHT SIDES OF THE AIRPLANE.

NOTENOTENOTENOTE:::: "MS20470AD-7" OR "132369AD4-7" RIVET REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZED OUTLET.


118-4014-0003INSTALLATION, COLD EXPANSION OF HOLES, WET WING ATA :

1900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900DTHIS KIT PROVIDES PARTS AND INFORMATION FOR THE REPLACEMENT OF FASTENERS AND COLDEXPANDING THE HOLES IN THE CENTER SECTION REAR SPAR FROM W.S. 80.00 TO W.S. 124.00

NOTENOTENOTENOTE:::: THIS KIT MUST HAVE KIT 118-4012-1/-3 INSTALLED PRIOR TO OR IN CONJUCTION WITHTHIS KIT

MEN : N/A

118-5000-1CREW PROTECTIVE BREATHING PROVISIONS ATA :1900C UB-1 THRU UB-58"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF CREW OXYGEN MASK MIC SELECTSWITCHES, ADDITIONAL CREW OXYGEN PRESSURE REGULATOR, NEW CREW OXYGEN MASKS, SMOKEGOGGLES AND CONTAINERS.

NOTENOTENOTENOTE:::: MS20426AD3 RIVET AND MS20470AD4 RIVET REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 5 LBS; MOMENT: 691 IN.-LBSEST. MAN/HRS: : 25MEN : 1 (MAN)


KIT CATALOG

118-5000-3CREW PROTECTIVE BREATHING PROVISIONS ATA :1900C UB-59 THRU UB-741900C-1 UC-1 THRU UC-174"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF CREW OXYGEN MASK MIC SELECTSWITCHES, ADDITIONAL CREW OXYGEN PRESSURE REGULATOR, NEW CREW OXYGEN MASKS, SMOKEGOGGLES AND CONTAINERS.

NOTENOTENOTENOTE:::: MS20426AD3 RIVET AND MS20470AD4 RIVET REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


118-5001-1AILERON CABLE INSTL, WING ATA :1900C-1, 1900C-1 (C-12J) ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AILERON WING CABLE ASSEMBLIES THATCANNOT BE CROSS CONNECTED. WHEN THIS KIT IS INSTALLED, ALL SIX OF THE WING CABLES MUST BEREPLACED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

118-8011-0001KIT 118-8011-0001 ATA :1900 UA-31900 (C-12J) UD-1 THRU UD-61900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-1 THRU UE-439THIS KIT PROVIDES INFORMATION ONLY TO INSTALL FLANGE BUSHINGS IN MAIN LANDING GEARSOCKET, LOWER AND UPPER TORQUE KNEES AND BRACE ASSY.MEN : N/A

118-9000-1 SAIR CONDITIONER INSTALLATION ATA :1900C UB SERIES EQUIPPED WITH 114-9016 KITS1900C-1 UC-2 AND AFTER"OPTIONAL" SB NO. 2345THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE MOUNT ASSEMBLY THATWILL PROVIDE ADDITIONAL CLEARANCE WITH THE GENERATOR INLET DUCT. ADDITIONAL FREON (R12RACON 15 LBS) MAY BE REQUIRED WHEN ACCOMPLISHING THIS CHANGE.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

118-9000-3 SAIR CONDITIONER INSTALLATION ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER THAT DO NOT HAVE

114-9016 KITS"OPTIONAL" SB NO. 2345THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE MOUNT ASSEMBLY THAT WILL PROVIDEADDITIONAL CLEARANCE WITH THE GENERATOR INLET DUCT. ADDITIONAL FREON (R12 RACON 15 LBS)MAY BE REQUIRED WHEN ACCOMPLISHING THIS INSTALLATION.WT. CHANGE : N/AEST. MAN/HRS: : 12MEN : 1 (MAN)

118-9001-1 SCOWLING REPAIR ATA :1900 UA-1 AND AFTER WITH 114-9016 KIT

INSTALLED1900C UB-1 AND AFTER WITH 114-9016 KIT

INSTALLED1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER"OPTIONAL" SB NO. 2369THIS KIT PROVIDES TYPICAL REPAIRS WHICH COULD BE USED ON AIRCRAFT COWLING INSTALLATIONS.FOR MATERIALS TO BE USED TO ACCOMPLISH THESE REPAIRS, REFER TO THE 1900 STRUCTURALREPAIR MANUAL.WT. CHANGE : TO BE DETERMINED BY REPAIREST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

118-9001-3 SCOWLING PREVENTATIVE MAINTENANCE ATA :1900 UA-1 AND AFTER WITH 114-9016 KIT


INSTALLED1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER"OPTIONAL" SB NO. 2369THIS KIT PROVIDES TYPICAL REPAIRS WHICH COULD BE USED ON AIRCRAFT COWLING MAINTENANCE.FOR MATERIALS TO BE USED TO ACCOMPLISH THESE REPAIRS, REFER TO THE 1900 STRUCTURALREPAIR MANUAL.WT. CHANGE : TO BE DETERMINED BY REPAIREST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

118-9001-5 SCOWLING MODIFICATION REPAIR INSTALLATION ATA :1900 UA-1 AND AFTER WITH 114-9016 KIT


INSTALLED1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER"OPTIONAL" SB NO. 2369THIS KIT PROVIDES PARTS AND INFORMATION WHICH COULD BE USED FOR THE REPAIR ANDPREVENTATIVE MODIFICATION INFORMATION KITS FOR COWLINGS ON IN-SERVICE AIRCRAFT.WT. CHANGE : TO BE DETERMINED BY REPAIREST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

118-9001-7 SCOWLING REPAIR 1900D ATA :1900D UE-1 AND AFTER"OPTIONAL" SB NO. 2369THIS KIT PROVIDES TYPICAL REPAIRS WHICH COULD BE USED ON AIRCRAFT COWLING INSTALLATIONS.FOR MATERIALS TO BE USED TO ACCOMPLISH THESE REPAIRS, REFER TO THE 1900 STRUCTURALREPAIR MANUAL.WT. CHANGE : TO BE DETERMINED BY REPAIREST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

118-9003-1PNEUMATIC SYSTEM MODIFICATION ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTERPENDING SB NO. 2539THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE CURRENT PNEUMATICSYSTEM ON IN-SERVICE AIRCRAFT. FOR REWORK INSTALLATION SEE -3 KIT.

NOTENOTENOTENOTE:::: FOLLOWING ITEMS NOT FURNISHED WITH KIT BUT REQUIRED. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "ALODINE 1000" CHEM-FILM COATING,"002X3W 150 FT RL "OR" 002X3W 300 FT RL "ALUMINUM PRESSURE SENSITIVE TAPE AND"EA934NA QT" OR "EA9394NA QT" NON-ASBESTOS ADHESIVE.

NOTENOTENOTENOTE:::: YOU WILL ALSO REQUIRE 24 "SF" OF INSULATION PART NUMBER "BS272HH1" PER KIT TOCOMPLETE KIT INSTALLATION ON YOUR AIRCRAFT. (3 EACH 4’ X 2’ SHEETS OFINSTALLATION)

NOTENOTENOTENOTE:::: CAN USE "MEK" AS ALT FOR PN: "MIL-C-38736" SOLVENT FOR CLEANING PURPOSES FORTHIS KIT.

WT. CHANGE : WT: 3 LBS; MOMENT: 786 IN.-LBSEST. MAN/HRS: : 28 TO 32MEN : 1 (MAN)


KIT CATALOG

118-9003-3PNEUMATIC SYSTEM REWORK ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTERPENDING SB NO. 2539THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REWORK THE CURRENT PNEUMATICSYSTEM ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOLLOWING ITEMS NOT FURNISHED WITH KIT BUT REQUIRED. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "ALODINE 1000" CHEM-FILM COATING,"002X3W 150 FT RL "OR" 002X3W 300 FT RL "ALUMINUM PRESSURE SENSITIVE TAPE AND"EA934NA QT" OR "EA9394NA QT" NON-ASBESTOS ADHESIVE.

NOTENOTENOTENOTE:::: FOR MODIFICATION INSTALLATION SEE 118-9003-1 KIT.NOTENOTENOTENOTE:::: CAN USE "MEK" AS ALT FOR PN: "MIL-C-38736" SOLVENT FOR CLEANING PURPOSES THIS

KIT.NOTENOTENOTENOTE:::: YOU WILL ALSO REQUIRE 24 "SF" OF INSULATION PART NUMBER "BS272HH1" PER KIT TO

COMPLETE KIT INSTALLATION ON YOUR AIRCRAFT. (3 EACH 4’ X 2’ SHEETS OFINSTALLATION)


129-0011-1EXTERIOR MARKING INSTALLATION ATA :1900D UE-1 THRU UE-262"OPTIONAL" SB NO. 2727THIS KIT PROVIDES FOR CONTRASTING EXTERIOR EMERGENCY EXIT MARKINGS AND TWO INCHCONTINUOUS COLOR BANDS AROUND AIRSTAIR DOOR AND EACH EMERGENCY EXIT. YOU MAY NEEDONE OF THE FOLLOWING 4 PAINTS, DEPENDING ON THE COLOR OF THE BANDS, AND EXTERNALMARKINGS THA



129-0011-3EXTERIOR MARKING INSTALLATION ATA :1900D UE-1 THRU UE-262"OPTIONAL" SB NO. 2727THIS KIT PROVIDES FOR TWO INCH CONTINUOUS COLOR BANDS AROUND AIRSTAIR DOOR ANDEMERGENCY EXITS. YOU MAY NEED ONE OF THE FOLLOWING 4 PAINTS, DEPENDING ON THE COLOR OFTHE BANDS, AND EXTERNAL MARKINGS THAT SHOW THE MEANS OF OPENING THE EMERGENCY EXITS.MUST




KIT CATALOG

129-0012-1OPERATION PER FAR PART 121 - INFORMATION ONLY ATA :1900D UE-1 AND AFTER"OPTIONAL" SB NO. 2727THIS KIT DRAWING LISTS THE MODIFICATIONS REQUIRED (TEN TO NINETEEN PASSENGERS) TOCONFIGURE IT FOR OPERATION UNDER PART 121 AS OF MARCH 20, 1997.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-0013-1AIRCRAFT OWNERSHIP PLATES ATA :1900C, 1900, 1900C-1, 1900D TO BE DETERMINED BY RACC.THIS KIT PROVIDES INFORMATION REQUIRED TO INSTALL, REPLACE, AND/OR REMOVE OWNERSHIPPLACARDS ON LEASED OR FINANCED AIRCRAFT, MODELS 1900, 1900C AND 1900D.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-0013-3AIRCRAFT OWNERSHIP PLATES ATA :1900 TO BE DETERMINED BY RACC.1900C1900C-1THIS KIT PROVIDES INFORMATION REQUIRED TO INSTALL, REPLACE AND/OR REMOVE OWNERSHIPPLACARDS ON MORTGAGED AIRCRAFT, MODELS 1900, 1900C AND 1900D.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-3000-1 SEFIS-84 STAND BY POWER RELAY MODIFICATION ATA :1900D UE-1 THRU UE-9THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY IN-SERVICE AIRCRAFT WITH EFIS-84 STAND BYPOWER SUPPLY INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)


KIT CATALOG

129-3001-1 STCAS AND GPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) ATA :1900D UE-(TBD) REFERENCE AIRCRAFT WITHOUTTHIS KIT PROVIDES HARDWARE PARTS AND THE INFORMATION NECESSARY TO INSTALL TRANSPONDERCOLLISION AVOIDANCE SYSTEM (TCAS) AND GROUND PROXIMITY WARNING SYSTEM (GPWS) ONAIRCRAFT EQUIPPED WITH 129-340146-3 TCAS AND GPWS PROVISIONS PER OPTIONAL PRODUCTIONWORK

NOTENOTENOTENOTE:::: THIS KIT INSTALLATION IS NOT COMPLETE UNTIL THE 1900D FAA APPROVED AIRPLANEFLIGHT MANUAL PART NUMBER 129-590000-3C4 OR LATER AND THE 1900D PILOT’SOPERATING MANUAL PART NUMBER 129-590000-5B2 OR LATER HAVE BEEN INSTALLED INTHE AIRPLANE. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : + 31 LBS.; MOMENT: 4901 IN.-LBS.EST. MAN/HRS: : 48MEN : 1 (MAN)

129-3001-11 SGPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) ATA :1900D UE-(TBD) REFERENCE AIRCRAFT WORK

ORDERTHIS KIT PROVIDES HARDWARE PARTS AND INFORMATION NECESSARY TO INSTALL GROUND PROXIMITYWARNING SYSTEM ( GPWS) IN AIRCRAFT EQUIPPED WITH 129-340123-3 TCAS AND GPWS PROVISIONSPER OPTIONAL PRODUCTION WORK ORDER.



129-3001-3 STCAS (AVIONICS NOT INCLUDED) ATA :1900D UE-(TBD) REFERENCE AIRCRAFT WORK

ORDERTHIS KIT PROVIDES HARDWARE PARTS AND INFORMATION NECESSARY TO INSTALL A TRANSPONDERCOLLISION AVOIDANCE SYSTEM (TCAS) IN AIRCRAFT EQUIPPED WITH 129-340146-3 OR 129-340146-7TCAS PROVISIONS PER OPTIONAL PRODUCTION WORK ORDER.




KIT CATALOG

129-3001-5 SGPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) ATA :1900D UE-(TBD) REFERENCE AIRCRAFT WORK

ORDERTHIS KIT PROVIDES HARDWARE PARTS AND INFORMATION NECESSARY TO INSTALL GROUND PROXIMITYWARNING SYSTEMS (GPWS) ONLY IN AIRCRAFT EQUIPPED WITH 129-340146-3 OR 129-340146-5 GPWSPROVISIONS PER OPTIONAL PRODUCTION WORK ORDER.


WT. CHANGE : + 9; MOMENT: 1476 IN.-LBS.EST. MAN/HRS: : 48MEN : 1 (MAN)

129-3001-7 STCAS AND GPWS HARDWARE ONLY (AVIONICS NOT INCLUDED) ATA :1900D UE-(TBD) REFERENCE AIRCRAFT WORK

ORDERTHIS KIT PROVIDES HARDWARE PARTS AND INFORMATION NECESSARY TO INSTALL TRANSPONDERCOLLISION AVOIDANCE SYSTEM (TCAS) AND GROUND PROXIMITY WARNING SYSTEM (GPWS) IN MODEL1900D AIRCRAFT EQUIPPED WITH 129-340123-3 TCAS AND GPWS PROVISIONS PER OPTIONAL PRODUCT


WT. CHANGE : + 31 IBS.; MOMENT: 15177 IN.-LBS.EST. MAN/HRS: : 48MEN : 1 (MAN)

129-3001-9 STCAS HARDWARE ONLY (AVIONICS NOT INCLUDED) ATA :1900D UE-(TBD) REFERENCE AIRCRAFT WORK

ORDERTHIS KIT PROVIDES HARDWARE PARTS AND INFORMATION NECESSARY TO INSTALL TRANSPONDERCOLLISION AVOIDANCE SYSTEM (TCAS) ONLY IN AIRCRAFT EQUIPPED WITH 129-340123-3 TCAS ANDGPWS PROVISIONS PER OPTIONAL PRODUCTION WORK ORDER.




KIT CATALOG

129-3003-1INSTRUMENT PANEL CLOCK ATA :1900D UE-1 THRU UE-403, UE-405 THRU UE-410

EXCEPT UE-109THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EITHER THE PILOT OR COPILOTMECHANICAL INSTRUMENT PANEL CLOCK WITH AN ELECTRONIC CLOCK FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EC3501A/B" OR "EA9309NA" ADHESIVE NOT SUPPLIED WITH KIT. PROCURE SEPARATELYFROM ANY COMPANY AUTHORIZED OUTLET.


129-3004-1COCKPIT SPEAKER SWITCH ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-1 THRU UE-261PENDING "OPTIONAL" SB NO. 3054, AIRLINER COMMUNIQUE NO. 41, MARCH 1996THIS KIT PROVIDES PARTS AND INFORMATION FOR COCKPIT SPEAKER SWITCH DISCONNECT FOR IN-SERVICE AIRCRAFT. REQUIRED BUT NOT SUPPLIED WITH KIT, AIRCRAFT FLIGHT MANUAL PART NUMBER129-590000-3 AND PILOT’S OPERATING MANUAL PART NUMBER 129-590000-5 AND PILOT’S CH

NOTENOTENOTENOTE:::: EST. MAN HRS: 16 FOR 1900C, AND 8 FOR 1900DWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : SEE NOTEMEN : 1 (MAN)

129-3006-1PROP DEICE BOOT PROTECTION ATA : 301900D UE-1 THRU UE-261"REQUIRED" SB NO. 30-3089THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PROP DEICE BOOT PROTECTION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PILOT OPERATING HANDBOOK SUPPLEMENT PART NUMBER: 129-590000-3D11 AND -5C7WILL NEED TO BE ORDERED SEPARATELY. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


129-3008-1YAW DAMP SWITCH ATA :1900D UE-2 THRU UE-277THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LIGHTED PUSHBUTTON YAW DAMPSWITCH (PART NUMBER 99-21P6H1-16086) WITH A MOMENTARY ACTION TOGGLE SWITCH FOR IN-SERVICE AIRCRAFT WHICH ARE NOT EQUIPPED WITH AUTOPILOT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-3009-1ARTEX ELT, TSOC91A ATA :1900C-1 UC-165 THRU UC-1741900D UE-1 THRU UE-157 UE-159THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF THE ARTEX 452-0150 MOUNT AND452-0020 OR 453-0020 REMOTE ELT SWITCH FOR IN-SERVICE AIRCRAFT.WT. CHANGE : DELTA + 2.7 LBS, MOMENT: = 1239 IN-LBS.EST. MAN/HRS: : 40MEN : 1 (MAN)

129-3009-3ARTEX ELT, TSOC91A ATA :1900C-1 UC-165 THRU UC-1741900D UE-20 THRU UE-23, UE-31 THRU UE-289THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF THE ARTEX 452-0150 METALMOUNT FOR IN-SERVICE AIRCRAFT.WT. CHANGE : DELTA + 1.4 LBS, MOMENT: + 818 IN-LBS.EST. MAN/HRS: : 2MEN : 1 (MAN)

129-3009-5ARTEX ELT, TSOC91A ATA :1900 UA-1 AND AFTER1900C UB-1 AND AFTER1900C-1 UC-1 THRU UC-1641900D UE-1 THRU UE-19, UE-24 THRU UE-30THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF THE ARTEX ELT 110-4-002, 452-0020OR 453-0020 REMOTE ELT SWITCH AND 452-0150 MOUNT FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: WT. CHANGE: DELTA + 4.7 LBS, MOMENT: DELTA + 2407 IN-LBS. (REPLACING THE DM 8.1)EST. MAN/HRS: 48WT. CHANGE: DELTA + 3.4 LBS, MOMENT: DELTA + 1647 IN-LBS. (REPLACING THE NARCOELT-10) EST. MAN/HRS: 48

WT. CHANGE : SEE NOTEEST. MAN/HRS: : SEE NOTEMEN : 1 (MAN)

129-3010-1OVERHEAD PANEL MIC SWITCH ATA :1900D UE-2 THRU UE-302THIS KIT PROVIDES "INFORMATION ONLY" TO REPLACE THE PILOT AND COPILOT MIC SELECT SWITCHESIN THE OVERHEAD PANEL WITH LEVERLOCK TYPE TOGGLE SWITCHES FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-3011-1COVER ASSEMBLY DC GENERATOR CONTROL UNITS ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-287THIS KIT PROVIDES "INFORMATION ONLY" FOR THE INSTALLATION OF THE 129-364004-1 COVERASSEMBLY FOR THE DC GENERATOR CONTROL UNITS ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 2 EACH 129-364004-1 COVERS ARE NOT SUPPLIED WITH THIS KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


129-3012-1EFIS POWER PANEL ATA :1900D UE-2 THRU UE-277THIS KIT PROVIDES "INFORMATION ONLY" TO REPLACE THE LIGHTED PUSHBUTTON EFIS POWERSWITCHES WITH LEVERLOCK TOGGLE SWITCHES FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-3013-1BRIEFER RELAY BOX WIRING, INFO ONLY ATA :1900D UE-1 THRU UE-434THIS KIT PROVIDES INFORMATION ONLY TO REWIRE CABIN BRIEFER RELAY BOX TO ALLOW A GREATERVOLUME ADJUSTMENT RANGE OF THE CABIN BRIEFER LEVELS. THIS IS TO EASE THE PROCESS OFBALANCING CABIN PA LEVELS AND CABIN BRIEFER LEVELS. FOR ALL INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-3014-1ALTIMETER INSTALLATION - INFORMATION ONLY ATA :1900D UE-306, UE-309 AND AFTER AND THOSE

WITH KIT 129-9018-1 INSTALLEDTHIS KIT PROVIDES INFORMATION TO REPLACE THE COPILOT MEGGITT LCD ALTIMETER WITH AKOLLSMAN 570-24929-412 OR 44929-412 ALTIMETER ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-3014-3ALTIMETER INSTALLATION - INFORMATION ONLY ATA :THIS KIT PROVIDES INFORMATION TO RE-INSTALL THE COPILOT MEGGITT 28004-01-02 LCD ALTIMETERAFTER IT HAS BEEN REMOVED BY KIT 129-3014-1 ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-3015-1REPLACEMENT, ENHANCED GROUND PROXIMITY WARNING SYSTEM(EGPWS) COMPUTER-INFORMATION ONLY

ATA :

1900D UE-1 AND AFTER WITH STC SA00855WI-DINSTALLED.

THIS KIT PROVIDES INFORMATION TO REPLACE EGPWS COMPUTER INSTALLED BY STC SA00855WI-DWITH PRODUCTION APPROVED PART NUMBER 965-1186-006 EGPWS COMPUTER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-3401-1ELT INSTL, DUAL MODE ATA :1900D UE-313 AND AFTERTHIS KIT PROVIDES INFORMATION FOR INSTALLATION OF THE ARTEX ELT 110-406 AND DUAL MODE RODANTENNA (110-323) FOR IN-SERVICE AIRCRAFT MODEL 1900D.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-3402-1FDR MODIFICATION, JAA CERTIFICATION ATA :1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR ADDING ACCELEROMETER AND OAT PARAMETERSFOR THE FLIGHT DATA RECORDER ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-3403-1CVR INSTL FOR JAR-OPS, INFO ONLY ATA :1900D UE-1 AND AFTERTHIS KIT PROVIDES INFORMATION FOR INSTALLATION OF THE FAIRCHILD MODEL FA2100 CVR FORINSERVICE AIRCRAFT.WT. CHANGE : WT: -5.8 LBS; ARM: 418.0 IN. MOMENT: -2424.4 IN-LB. (IF REPLACING P/N S100-0080-00 (A100S)).

WT: -12.1 LBS ARM: 418.0 IN. MOMENT: -5057.8 IN'LB. (IF REPLACING P/N 93-A100-83 (A100A)).EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-3404-1ELT, DUAL MODE ATA :1900D UE-313 TO UE-429THIS KIT PROVIDES INFORMATION FOR INSTALLATION OF THE ARTEX ELT C406-2 AND DUAL MODE RODANTENNA (110-323) FOR IN-SERVICE AIRCRAFT MODEL 1900D.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-3621-1WIRE CHAFING INFORMATION ONLY ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-2 THRU UE-262THIS KIT PROVIDES INFORMATION ONLY TO REWORK PARTS TO PREVENT WIRE CHAFING UNDERFLOORBOARDS, STARTING AT F.S. 143.00 TO APPROX. F.S. 290.50 FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4001-1 SWINDOW CABIN GRAVEL RUNWAY OPTION ATA :1900D UE-1 AND AFTER, BUT IS ONLY REQUIRED

ON AIRCRAFT THAT ARE BEING USED INOPERATIONS THAT REQUIRE LANDINGSON GRAVEL RUNWAYS

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL MULTI-PLY CABIN WINDOWSWHEN OPERATING FROM GRAVEL RUNWAYS.

NOTENOTENOTENOTE:::: KIT REPLACES 5 CABIN WINDOWS ON RIGHT SIDE OF AIRCRAFT AND 3 WINDOWS ONLEFT SIDE OF AIRCRAFT. THERE IS A TOTAL OF 8 CABIN WINDOWS PER KIT.


129-4002-1 SP-STATIC PREVENTION ATA :1900D UE-1 THRU UE-17, EXCEPT UE-16"MANDATORY" SB NO. 2494, JULY, 1993THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION TO IMPROVE P-STATIC BONDING.

NOTENOTENOTENOTE:::: FOLLOWING ITEMS NOT FURNISHED BUT REQUIRED TO MAKE KIT INSTALLATION. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. PART NUMBER "890B1/2QT" OR PART NUMBER "890B2" PRO-SEAL 890 SEALANT AND PART NUMBER "ALODINE1200" PROTECTIVE COATING.



KIT CATALOG

129-4003-1 SP-STATIC PREVENTION ATA :1900D UE-16, UE-18 THRU UE-53THIS KIT PROVIDES THE NECESSARY PARTS AND INFORMATION TO IMPROVE P-STATIC BONDING.

NOTENOTENOTENOTE:::: PROTECTIVE COATING PART NUMBER "ALODINE 1200" WILL BE REQUIRED TO INSTALLTHIS KIT ON AIRCRAFT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


129-4004-1 SICE SHIELD INSTALLATION, ALUMINUM ATA :1900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" ON HOW TO INSTALL ALUMINUM ICE SHIELDS ON IN-SERVICEAIRCRAFT.WT. CHANGE : WT: + 24 LBS.; MOMENT: + 4920 IN.-LBS.EST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

129-4005-1 SBULKHEAD REINFORCEMENT, CANTED FS 588.10 INSTALLATION ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-113THIS KIT PROVIDES PARTS AND INFORMATION TO REINFORCE PORTIONS OF BULKHEAD AT CANTEDFUSELAGE STATION 588.10 FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ADHESIVE PART NUMBER: "EC2084", "ALODINE 1200" OR EQUIVALENT AND "MIK-P23377CQT" EPOXY PRIMER ARE NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY. THESE MS RIVETS: MS20470AD4,MS20426AD4 ANDMS20426AD3 ALSO REQUIRED BUT LENGTH TO BE DETERMINED DURING INSTALLATION.

WT. CHANGE : WT: 2 LBS; MOMENT: + 1176 IN.-LBSEST. MAN/HRS: : 48 TO 60MEN : 2 (MEN)

129-4006-1AIRSTAIR DOOR HANDRAIL IMPROVEMENT ATA :1900D UE-1 THRU UE-123THIS KIT PROVIDES THE EQUIPMENT AND INFORMATION TO INSTALL THE AIRSTAIR DOORIMPROVEMENTS TO THE HANDRAIL INSTALLATION AND THE NECESSARY ATTACHING HARDWARE.

NOTENOTENOTENOTE:::: IF 129-400033-59 AIRSTAIR DOOR BOND ASSEMBLY ON YOUR AIRCRAFT, SEE KIT129-4007-1.

NOTENOTENOTENOTE:::: SAFETY WIRE PART NUMBER: "MS20995C32" REQUIRED FOR USAGE WITH THIS KIT BUTNOT FURNISHED. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



KIT CATALOG

129-4007-1AIRSTAIR DOOR HANDRAIL IMPROVEMENT (129-400033-59) ATA :1900D UE-1 THRU UE-123THIS KIT PROVIDES THE EQUIPMENT AND INFORMATION TO INSTALL HANDRAIL IMPROVEMENT TO THEAIRSTAIR DOOR AND THE NECESSARY ATTACHING HARDWARE FOR AIRCRAFT WITH 129-400033-59AIRSTAIR DOOR BOND ASSEMBLY AS A REPLACEMENT FOR THE -3 BOND ASSEMBLY.

NOTENOTENOTENOTE:::: SAFETY WIRE PART NUMBER: "MS2099TC32" REQUIRED FOR USAGE WITH THIS KIT, BUTNOT FURNISHED, IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.

NOTENOTENOTENOTE:::: FOR AIRCRAFT WITH 129-400033-3 BOND ASSEMBLY SEE KIT 129-4006-1.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16 TO 20MEN : 1 (MAN)

129-4008-1ICE SHIELD LH, REPLACEMENT (KEVLAR ) ATA :1900D UE-1 AND AFTERPENDING "OPTIONAL" SB NO. 2529THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE AND REINSTALL A LH KEVLARICE SHIELD ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: WT_CHG: UE-1 TO UE-88; WT: 2 LBS.; MOMENT: 442 IN.-LBS.; UE-89 AND AFTER,NEGLIGIBLE

NOTENOTENOTENOTE:::: THE -3 KIT IS REQUIRED ON THE RH SIDE.NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED ITEMS NOT FURNISHED WITH KIT: FILLER MATERIAL

EITHER "DEVCON F" OR "METALSET A4 6 OZ" OR "METALSET A4 11 OZ" OR "METALSET A4GL". ALSO SEALER "PR1440B1/2 6 OZ K" AND "PR1440B2 6 OZ KT" OR "PR1440B4 6 OZ TU".THIS ALSO GOES FOR "GS NO. 213" STRIP CAULK WHICH COMES IN A ROLL. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : SEE NOTEEST. MAN/HRS: : 16 TO 24MEN : 2 (MEN)

129-4008-3ICE SHIELD LH, REPLACEMENT (KEVLAR ) ATA :1900D UE-1 AND AFTERPENDING "OPTIONAL" SB NO. 2529THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE AND REINSTALL A RH KEVLARICE SHIELD ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED ITEMS NOT FURNISHED WITH KIT: FILLER MATERIALEITHER "DEVCON F" OR "METALSET A4 6 OZ" OR "METALSET A4 11 OZ" OR "METALSET A4GL". ALSO SEALER "PR1440B1/2 6 OZ K" AND "PR1440B2 6 OZ KT "OR" PR1440B4 6 OZ TU".THIS ALSO GOES FOR "GS NO. 213" STRIP CAULK WHICH COMES IN A ROLL. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THE -1 KIT IS REQUIRED ON THE LH SIDEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16 TO 24MEN : 2 (MEN)


KIT CATALOG

129-4009-1ICE SHIELD EXTENSION INSTALLATION, KEVLAR (LH) ATA :1900D UE-1 THRU UE-88PENDING "OPTIONAL" SB NO. 2529THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH KEVLAR ICE SHIELD ON IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED ITEMS NOT FURNISHED WITH KIT: FILLER MATERIALEITHER "DEVCON F" OR "METALSET A4 6 OZ" OR "METALSET A4 11 OZ" OR "METALSET A4GL". ALSO SEALER "PR1440B1/2 6 OZ K" AND "PR1440B2 6 OZ KT "OR" PR1440B4 6 OZ TU".THIS ALSO GOES FOR "GS NO. 213" STRIP CAULK WHICH COMES IN A ROLL. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 2 LBS; MOMENT: 442 IN.-LBSEST. MAN/HRS: : 12 TO 14MEN : 2 (MEN)

129-4012-1FUEL BAY REPAIR INSTALLATION ATA :1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INSTRUCTIONS FOR INSTALLING WING REINFORCEMENTS AND SEALINGOF FUEL TANK ON RH SIDE OF WING.

NOTENOTENOTENOTE:::: ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT, PR-1750 OR PR-1750B2. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 1.0 LBS.; MOMENT: 293 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4013-1FUEL BAY REPAIR INSTALLATION (RH) ATA :1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INSTRUCTIONS NECESSARY FOR INSTALLING HI-LOK FASTENERS ANDSEALING OF FUEL TANK ON RH SIDE OF WING FOR THE IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR1750B2" SEALANT (MIL-S-83430) WILL BE REQUIRED FOR INSTALLATION OF THIS KIT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 0.6 LBS.; MOMENT: 176 IN.-LBS.EST. MAN/HRS: : 24 TO 32MEN : 2 (MEN)


KIT CATALOG

129-4014-1VENT INSTALLATION STABILON ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-181THIS KIT PROVIDES "INFORMATION ONLY" TO ELIMINATE THE POSSIBILITY OF VACUUM DEVELOPINGINSIDE THE STABILON LEADING EDGE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309NA" OR "EA9309 QT" SEALER OR EQUIVALENT REQUIRED FOR USE WITH THIS KIT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


129-4015-1FUEL BAY REPAIR INSTALLATION ATA :1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INSTRUCTIONS FOR INSTALLING HI-LOK FASTENERS AND SEALING OFFUEL TANK ON RH SIDE OF WING FOR INSERVICE AIRCRAFT.





WT. CHANGE : WT: 0.2 LBS.; MOMENT : 58 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG




129-4016-1ACCESS DOORS, FUEL BAY ATA :1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT DEFINES PARTS AND PROVIDES INSTRUCTIONS FOR INSTALLING ACCESS DOORS ON LOWERSURFACE OF RH WING LEADING EDGE FOR INSERVICE AIRCRAFT. NO PARTS ARE PROVIDED WITH KIT.WT. CHANGE : WT: 75 LBS.; MOMENT: 214 IN.-LBS., FOR EACH DOOR INSTALLATIONEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4016-19ACCESS DOORS, FUEL BAY ATA :1900C-1 UC-1 AND AFTER1900C-1(C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" FOR INSTALLING ACCESS DOORS ON LOWER SURFACE OF RHWING LEADING EDGE FOR INSERVICE AIRCRAFT. NO PARTS ARE PROVIDED WITH KIT.WT. CHANGE : WT: 75 LBS.; MOMENT: 214 IN.-LBS., FOR EACH DOOR INSTALLATIONEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4017-1FUEL LEAK REPAIR ATA :1900C-1 UC-1 AND AFTER1900C-1(C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" FOR EXTERNAL SEALING OF FUEL TANK ON RH SIDE OF WINGFOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEALANT REQUIRED BUT NOT SUPPLIED WITH KIT: PR-1750B2 MAY BE PURCHASEDLOCALLY.



KIT CATALOG

129-4018-1FLAP SKIN IMPROVEMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE LH INBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : WT: 3.0 LBS.; MOMENT: + 1017 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4018-2FLAP SKIN IMPROVEMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE RH INBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : WT: 3.0 LBS.; MOMENT: + 1017 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4018-3FLAP SKIN IMPROVEMENT ATA :1900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE LH OUTBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : WT: 2.0 LBS.; MOMENT: + 656 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4018-4FLAP SKIN IMPROVEMENT ATA :1900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE RH OUTBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : WT: 2.0 LBS; MOMENT: + 652 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-4018-5FLAP SKIN IMPROVEMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE LH OUTBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : WT: 2.0 LBS; MOMENT: + 652 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4018-6FLAP SKIN IMPROVEMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE RH OUTBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : WT: 2.0 LBS.; MOMENT: + 656 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4018-7FLAP SKIN IMPROVEMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE LH INBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : + 4.0 LBS.; MOMENT: + 1356 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4018-8FLAP SKIN IMPROVEMENT ATA :1900 UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE RH INBOARD FLAP FOR INSERVICEAIRCRAFT.WT. CHANGE : + 4.0 LBS.; MOMENT: + 1356 IN.LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-4019-1FLAP COVE, INBOARD, FLAP GAP INCREASE (LH) ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE FLAP COVE GAP IMPROVEMENT KIT ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CR3212-4, CR3245-4, MS20426AD4, MS20470AD4, MS20426AD3, AND MS20470AD3 RIVETSREQUIRED ARE NOT SUPPLIED WITH THIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.

WT. CHANGE : + 1.0 LBS.; MOMENT: + 332.0 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4019-2FLAP COVE, INBOARD, FLAP GAP INCREASE (RH) ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 TO UE-375THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE FLAP COVE GAP IMPROVEMENT KIT ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CR3212-4, CR3245-4, MS20426AD4, MS20470AD4, MS20426AD3, AND MS20470AD3 RIVETSREQUIRED ARE NOT SUPPLIED WITH THIS KIT. YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 1.0 LBS; MOMENT: + 332.0 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4020-1HANDLE SUPPORT ASSEMBLY AIRSTAIR DOOR ATA : 521900D UE-1 THRU UE-403"MANDATORY" SB NO. 52-3099THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE BELLCRANK SUPPORTASSY. WITH THROUGH BOLTS ON THE AIRSTAIR DOOR OF INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EST. MAN/HRS: 6 WITH NO LOOSE INSERTS. 6 + 1 HR PER LOOSE INSERT, WITH LOOSEINSERTS.

NOTENOTENOTENOTE:::: EA9309NA "ADHESIVE" REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 +1 PER LOOSE INSERTMEN : 1 (MAN)


KIT CATALOG

129-4022-1EMERGENCY EXIT DOOR SEAL IMPROVEMENTS - INFORMATION ONLY ATA :1900D UE-1 THRU UE-334THIS KIT PROVIDES INFORMATION FOR THE REPLACEMENT OF THE SEAL FOR THE EMERGENCY EXITDOORS.

NOTENOTENOTENOTE:::: "EC1300L" ADHESIVE, "EA960F" FILLER AND "131836-10436" EXTRUSION REQUIRED BUTNOT SUPPLIED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


129-4023-1STATIC WICK REMOVAL - INFORMATION ONLY ATA :1900D UE-1 THRU UE-379THIS KIT PROVIDES INFORMATION REGARDING THE REMOVAL OF THE STATIC DISCHARGERS AND BASEPLATES LOCATED ON THE RUDDER AND ON THE HORIZONTAL STABILIZER.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPLICABLE AIRCRAFT FLIGHTMANUAL REVISION HAS BEEN INCORPORATED. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


129-4024-1SEAT TRACK COVER INSTL - INFORMATION ONLY ATA :1900, 1900C, 1900C-1, 1900C-1 (C-12J),1900D

ALL

THIS KIT PROVIDES INFORMATION TO INSTALL COVERS TO THE FLOOR SEAT TRACK ON ALL 1900 SERIESAIRCARFT.WT. CHANGE : 6 LB; MOMENT:1920 IN-LBEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4024-3SEAT TRACK COVER INSTALLATION INFORMATION ATA :1900, 1900C, 1900C-1, 1900C-1 (C-12J),1900D

ALL

THIS KIT PROVIDES INFORMATION TO INSTALL COVERS TO THE SIDE SEAT TRACK ON ALL 1900 SERIESAIRCRAFT.WT. CHANGE : 3 LB; MOMENT; 1068 IN-LB.EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

129-4026-1INSTALLATION OF CONDENSATION DRAINS ATA :1900 UA-1 AND UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-382THIS KIT PROVIDES INFORMATION FOR THE INSTALLATION OF CONDENSATION DRAINS ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: 50-420082-3 SEAL, 50-420082-5 RETAINING RING, EC847 CEMENT, AND MS20470AD3 RIVETREQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


129-4027-1BIRD STRIKE PROVISIONS - INFORMATION ONLY ATA :1900D UE-1 THRU UE-294THIS KIT PROVIDES INFORMATION FOR BIRD STRIKE PROVISIONS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4028-1RADOME DRAIN INSTALLATION - INFORMATION ONLY ATA :1900 UA-2 AND UA-31900C ALL UB1900C-1 ALL UC1900C-1 (C-12J) ALL UD1900D UE-1 AND AFTERTHIS KIT PROVIDES INFORMATION NECESSARY TO INSTALL A S-43 GROMMET-METAL DRAIN FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 528-104 FLAT BLACK PAINT, EA9309 ADHESIVE, METHYL SOLVENT, AND S43 GROMMETREQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY, OR FROM RAPID.



KIT CATALOG

129-4029-1DE-ICE BOOT INSTL, FAST BOOT - INFORMATION ONLY ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74, UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY TO INSTALL THE BF GOODRICH FASTBOOT PNEUMATIC DEICEBOOT OR STALL STRIP FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4030-1FAIRING REPAIR, INFORMATION ONLY ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74, UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY NECESSARY TO REPAIR THE INBOARD FAIRINGS THAT HAVEBECOME DEBONDED FROM THE LEFT WING LEADING EDGE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4031-1RH PROPELLER IMPACT SHIELD INSTALLATION ATA :1900 UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE EXISTING ICE SHIELD WITHA NEW SHIELD FOR ICE AND PROPELLER PROTECTION ON THE RIGHT SIDE OF THE AIRCRAFT TOPROVIDE BETTER IMPACT RESISTANCE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR1440" SEALER, "EA9309NA" ADHESIVE, "M7885/6-4-08" "M7885/6-4-03" AND "MS20470E5"RIVETS, MASKING TAPE, "DEVCON-F" FILLER AND "GS-213" STRIP CAULK REQUIRED, BUTNOT FURNISHED WITH KIT. PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : 8.9 LBS; MOMENT: 1827 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-4033-1STRUCTURAL PROVISIONING FOR GPS AND VHF ANTENNA ATA :1900D UE-243, UE-271, UE-272, UE-276, UE-277,

UE-278, UE-281, UE-283, UE-285, UE-287,UE-289, UE-346, UE-351, UE-359.

THIS KIT PROVIDES INFORMATION TO INSTALL STRUCTURAL PROVISIONING FOR GPS ANTENNA,BETWEEN FS423.25 AND FS438.25 ON MODEL 1900D AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-4033-3STRUCTURAL PROVISIONING FOR GPS AND VHF ANTENNAINSTALLATIONS

ATA :

1900D UE-243, UE-271, UE-272, UE-276, UE-277,UE-278, UE-281, UE-283, UE-285, UE-287,UE-289, UE-346, UE-351, UE-359

THIS KIT PROVIDES INFORMATION TO INSTALL STRUCTURAL PROVISIONING FOR VHF ANTENNA,BETWEEN F.S.378.25 AND F.S.393.25 ON MODEL 1900D AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-4034-1LIGHTER TINTED CABIN WINDOW ATA :1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LIGHT TINTED CABIN WINDOWS ON IN-SERVICE 1900D AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5000-1 SCABIN HEATING IMPROVEMENT ATA :1900D UE-1 THRU UE-20THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ADDITIONAL BLEED AIR DUCTINSULATION, MODIFY THE VENTILATION DUCTING, AND REVISE THE BLOWER SWITCHING TO PROVIDEIMPROVED HEATING AND AIR DISTRIBUTION.WT. CHANGE : + 3 LBS. @ 256"EST. MAN/HRS: : 24 TO 36MEN : 2 (MEN)

129-5001-1 SBLEED AIR HEATING IMPROVEMENT ATA :1900D UE-2 THRU UE-27THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO PROVIDE IMPROVED CABIN HEATING BYREROUTING OF BLEED AIR PLUMBING AROUND THE AIR CYCLE REFRIGERATION PACK.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 32 TO 47MEN : 1 (MAN)

129-5004-1 MPARTITION PAD, LH FORWARD PARTITION ATA :1900D UE-2 THRU UE-23THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT BY ADDING APARTITION PAD TO THE LH FORWARD PARTITION.WT. CHANGE : WT: + 3 LBS.; MOMENT: + 528 IN.-LBS.EST. MAN/HRS: : 5MEN : 1 (MAN)


KIT CATALOG

129-5005-1 SCABIN EJECTOR NOISE IMPROVEMENT ATA :1900D UE-1 THRU UE-93"RECOMMENDED" SB NO. 2545THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ADDITIONAL THERMAL ANDACOUSTIC INSULATION AROUND THE BLEED AIR EJECTOR INLET FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING SEALER "EA9309 QT" IS REQUIRED FOR INSTALLATION OF KIT, IF NOT INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


129-5006-1REWORK-BEECHCRAFT MODEL 1900D ATA :1900D UE-69THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY IN-SERVICE 1900D PER BEECHCRAFTCOMPAGNIE TRANSAIR REQUIREMENTS.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-5007-1 SPARTITION BRACKETRY INSTALLATION ATA :1900D UE-1 THRU UE-104 (WITH OPTIONAL

SLIDING DOOR PARTITION)"MANDATORY" SB NO. 2556THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE TWO RIGHT SIDE FORWARDPARTITION BRACKETS AND ADD A NEW BRACKET TO THE INBOARD LOWER EDGE OF THE PARTITIONALONG WITH MODIFYING THE AVIONICS COVER TO CLEAR THE NEW BRACKET FOR AIRCRAFT EQUIPPEDWT. CHANGE : WT: 7 LBS; MOMENT: 105 IN.-LBSEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)

129-5008-1 SPARTITION BRACKET COVER INSTALLATION ATA :1900D UE-1 THRU UE-54THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE TWO RIGHT SIDE AFTPARTITION BRACKETS AND ADD PLASTIC COVERS TO THE BRACKET LOCATIONS SO THAT THEBRACKETS MAY BE MOUNTED DIRECTLY TO STRUCTURE AND THE CUTOUTS IN THE UPHOLSTERYCOVERED ON INSERWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)


KIT CATALOG

129-5009-1REPLACEABLE DETENT PIN, ONE THRUST LEVER INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J ) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK BOTH THRUST LEVERS ON ALL AIRCRAFTPEDESTAL ASSEMBLIES. THIS KIT PROVIDES REPLACEMENT FOR 114-524096 DETENT PIN.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 5MEN : 1 (MAN)

129-5009-3REPLACEABLE DETENT PIN, BOTH THRUST LEVER INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO REWORK BOTH THRUST LEVERS ON ALL AIRCRAFTPEDESTAL ASSEMBLIES. THIS KIT PROVIDES REPLACEMENT FOR 114-524096 DETENT PIN. IF ONLYDESIRE TO REPLACE ONE PIN SEE 129-5009-1 KITWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 5 TO 6MEN : 1 (MAN)

129-5010-1STORM WINDOW DRIP TRAY AND PLUMBING INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1, 1900C-1 (C-12J) UD-1 THRU UD-61900D UE-2 THRU UE-171PENDING "OPTIONAL" SB NO. 2589THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL DRIP TRAYS FOR THE COCKPITSTORM WINDOWS BOTH LEFT AND RIGHT SIDES, AND TO PROVIDE PLUMBING TO DRAIN THE MOISTUREFROM DRIP TRAYS TO THE AIRCRAFT BELLY ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED, PART NUMBER:"5776" URALANE ADHESIVE(AS REQUIRED QUANTITY). IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY. WILL ALSO NEED SOME "ALODINE 1200" COATING AND "MILP23377QT" PRIMER TO INSTALL KIT.



KIT CATALOG

129-5011-1ENVIRONMENTAL PLUMBING INSTALLATION, FILTER ASSEMBLY FORFOG NOZZLE

ATA :

1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-6"OPTIONAL" SB NO. 2573NO LONGER OFFERED, CONTACT PRODUCT SUPPORT FOR ADDITIONAL INFORMATION. SEE SB 2669 ANDKITS 129-5023-1 OR -3 TO DETERMINE THE REPLACEMENT KIT INSTALLATION YOU WILL REQUIRE FORYOUR AIRCRAFT. THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A REPLACEABLEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

129-5016-1SPEAKER INSTALLATION, HEADLINER AND SIDEWALL ATA :1900D UE-2 THRU UE-184"RECOMMENDED" SB NO. 2627, NOV. 96THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL SPEAKERS IN THE EXISTINGHEADLINER PANELS TO IMPROVE THE QUALITY AND INCREASE THE VOLUME OF THE AUDIO SYSTEM ONINSERVICE AIRCRAFT WITH A COMM-ANTENNA LOCATED FORWARD OF FS 213.5.

NOTENOTENOTENOTE:::: FOR AIRCRAFT WITH COMM ANTENNA LOCATED APPROXIMATELY @ FS 213-5, SEE -3 KIT.NOTENOTENOTENOTE:::: FOLLOWING AS REQUIRED ITEMS NOT FURNISHED WITH KIT BUT ARE REQUIRED FOR

INSTALLATION: "890 PINT" OR "890B2" PROSEAL. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 9 LBS.; MOMENT: + 2367 IN.-LBS.EST. MAN/HRS: : 12MEN : 2 (MEN)

129-5017-1PRESSURIZATION CONTROLLER, GUARD INSTALLATION ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-TBDTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PROTECTIVE GUARD OVER THEPRESSURIZATION CONTROLLER TO REDUCE DAMAGE TO THE CONTROLLER. THIS KIT MAY REPLACE KIT114-5038-1 IN ITS ENTIRETY FOR GREATER PROTECTION FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALTERNATE KIT IS 114-5038-1 S.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.2MEN : 1 (MAN)


KIT CATALOG

129-5018-1CREW OXYGEN MASK REPLACEMENT - SPARES ATA :1900C, 1900, 1900C-1, 1900C-1(C-12J),1900DWT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-5019-1PLACARD INSTALLATION, FIRE EXTINGUISHER LOCATION FORWARDPARTITION

ATA :

1900D UE-2 THRU UE-128THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE 1900D AIRCRAFT BY ADDINGA FIRE EXTINGUISHER LOCATING PLACARD TO THE FWD PARTITION.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5020-1AIR CONDITIONING REFRIGERANT CHANGE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-2 THRU UE-230THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT THE AC REFRIGERANT FROMR12 TO R134A IN THE AIR CONDITIONING SYSTEMS WHICH USE PART NUMBER 36-555003-5COMPRESSOR.

NOTENOTENOTENOTE:::: ################NOTENOTENOTENOTE:::: EQUIPMENT AND SUPPLIES REQUIRED.

1. FLUSH CART: A SUITABLE FLUSH CART IS CLASSIC TOOL FLUSH-R-CART,MANUFACTURED BY CLASSIC TOOL DESIGN, INC., NEW WINDSOR, NY. ANY SUITABLEDEVICE CONSISTING OF A PUMP, RESERVOIR, FILTER, AND CONTROL VALVE TOCONTROL AND CONTAIN THE SHOP AIR FLO COULD BE SATISFACTORY. 2. SHOP AIR SUPPLY: A MINIMUM OF 90 PSI SHOP AIR SUPPLY FILTERED TO REDUCEMOISTURE, MUST BE SUPPLIED TO THE FLUSH CART.3. FLUSH FLUID: RECOMMENDED FLUSH FLUID IS AC FLUSH SUPPLIED BY CASTROLNORTH AMERICA, SPECIALTY PRODUCTS DIVISION, 16715 VON KARMAN AVE., IRVINE,CA., 92714-4918. (714) 660-94144. APPROXIMATELY 2.5 GALLONS WILL BE REQUIRED.5. REFRIGERANT: APPROXIMATELY 5 LBS., R134A REFRIGERANT REQUIRED TO CHARGESYSTEM.6. LEAK DETECTION DEVICE: AN R134A LEAK DETECTION DEVICE CAPABLE OFDETECTING LEAKS DOWN TO 0.5 OZ. PER YEAR IS REQUIRED.7. DC POWER SUPPLY: A REGULATED DC POWER SUPPLY CAPABLE OF SUPPLYING 18-31VDC IS REQUIRED.

NOTENOTENOTENOTE:::: APPROXIMATELY 5 LBS. OF PART NUMBER: R134A REFRIGERANT WILL BE REQUIRED TOCHARGE THE SYSTEM. WILL ALSO REQUIRE RL100S OIL NOT FURNISHED WITH KIT.



KIT CATALOG

129-5020-3AIR CONDITIONING REFRIGERANT CHANGE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-191900C-1 (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT THE AC REFRIGERANT FROMR12 TO R134A IN THE AIR CONDITIONING SYSTEMS

NOTENOTENOTENOTE:::: AIRCRAFT REQUIRING A/C COMPRESSOR REPLACEMENT ALSO , SEE 129-5020-5 KIT.LATER AIRCRAFT NOT NEEDING A COMPRESSOR SEE 129-5020-1 KIT.

NOTENOTENOTENOTE:::: APPROXIMATELY 5 LBS. OF PART NUMBER: R134A REFRIGERANT WILL BE REQUIRED TOCHARGE THE SYSTEM. YOU WILL ALSO REQUIRE RL100S OIL NOT FURNISHED WITH KIT.

NOTENOTENOTENOTE:::: EQUIPMENT AND SUPPLIES REQUIRED.1. FLUSH CART: A SUITABLE FLUSH CART IS CLASSIC TOOL FLUSH-R-CART,MANUFACTURED BY CLASSIC TOOL DESIGN, INC., NEW WINDSOR, NY. ANY SUITABLEDEVICE CONSISTING OF A PUMP, RESERVOIR, FILTER, AND CONTROL VALVE TOCONTROL AND CONTAIN THE SHOP AIR FLO COULD BE SATISFACTORY.2. SHOP AIR SUPPLY: A MINIMUM OF 90 PSI SHOP AIR SUPPLY FILTERED TO REDUCEMOISTURE, MUST BE SUPPLIED TO THE FLUSH CART.3. FLUSH FLUID: RECOMMENDED FLUSH FLUID IS AC FLUSH SUPPLIED BY CASTROLNORTH AMERICA, SPECIALTY PRODUCTS DIVISION, 16715 VON KARMAN AVE., IRVINE,CA., 92714-4918. (714) 660-9414.4. APPROXIMATELY 2.5 GALLONS WILL BE REQUIRED.5. REFRIGERANT: APPROXIMATELY 5 LBS., R134A REFRIGERANT REQUIRED TO CHARGESYSTEM.6. LEAK DETECTION DEVICE: AN R134A LEAK DETECTION DEVICE CAPABLE OFDETECTING LEAKS DOWN TO 0.5 OZ. PER YEAR IS REQUIRED.7. DC POWER SUPPLY: A REGULATED DC POWER SUPPLY CAPABLE OF SUPPLYING 18-31VDC IS REQUIRED.



KIT CATALOG

129-5020-5AIR CONDITIONING REFRIGERANT AND COMPRESSOR CHANGE ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CONVERT THE AC REFRIGERANT FROMR12 TO R134A IN THE AIR CONDITIONING SYSTEMS WHICH REQUIRE A REPLACEMENT COMPRESSOR(PART NUMBER: 36-555003-1 AND PFD-29 AND PFD-30 HOSES WITH THE KIT.

NOTENOTENOTENOTE:::: EQUIPMENT AND SUPPLIES REQUIRED.1. FLUSH CART: A SUITABLE FLUSH CART IS CLASSIC TOOL FLUSH-R-CART,MANUFACTURED BY CLASSIC TOOL DESIGN, INC., NEW WINDSOR, NY. ANY SUITABLEDEVICE CONSISTING OF A PUMP, RESERVOIR, FILTER, AND CONTROL VALVE TOCONTROL AND CONTAIN THE SHOP AIR FLO COULD BE SATISFACTORY.2. SHOP AIR SUPPLY: A MINIMUM OF 90 PSI SHOP AIR SUPPLY FILTERED TO REDUCEMOISTURE, MUST BE SUPPLIED TO THE FLUSH CART.3. FLUSH FLUID: RECOMMENDED FLUSH FLUID IS AC FLUSH SUPPLIED BY CASTROLNORTH AMERICA, SPECIALTY PRODUCTS DIVISION, 16715 VON KARMAN AVE., IRVINE,CA., 92714-4918. (714) 660-9414.4. APPROXIMATELY 2.5 GALLONS WILL BE REQUIRED.5. REFRIGERANT: APPROXIMATELY 5 LBS., R134A REFRIGERANT REQUIRED TO CHARGESYSTEM.6. LEAK DETECTION DEVICE: AN R134A LEAK DETECTION DEVICE CAPABLE OFDETECTING LEAKS DOWN TO 0.5 OZ. PER YEAR IS REQUIRED.7. DC POWER SUPPLY: A REGULATED DC POWER SUPPLY CAPABLE OF SUPPLYING 18-31VDC IS REQUIRED.

NOTENOTENOTENOTE:::: APPROXIMATELY 5 LBS. OF PART NUMBER: R134A REFRIGERANT WILL BE REQUIRED TOCHARGE THE SYSTEM. YOU WILL ALSO REQUIRE RL100S OIL NOT FURNISHED WITH KIT.

NOTENOTENOTENOTE:::: FOR AIRCRAFT NOT REQUIRING A COMPRESSOR REPLACEMENT, SEE 129-5020-1 AND -3.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5021-1PLACARD, EMERGENCY EVACUATION INSTALLATION (FORWARD CABINPARTITION)

ATA :

1900D UE-2 THRU UE-128PENDING SBTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PLACARDS DENOTING INSTRUCTIONS FORTHE CREW FOR EMERGENCY EXIT IN CASE THE SLIDING DOORS CANNOT BE OPENED IN THE NORMALMANNER IN AN EMERGENCY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .6 TO 1.1MEN : 1 (MAN)


KIT CATALOG

129-5023-1SPRAY NOZZLE INSTALLATION, AIR CYCLE MACHINE MOD FORAIRCRAFT WITHOUT 129-5011-1 INSTALLED

ATA : 21

1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-198"RECOMMENDED" SB NO. 2669, 1 KIT PER AIRCRAFT, AIRLINER COMMUNIQUE 41THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPRAY NOZZLE WITH A LARGER ORIFICEAND REMOVE THE SPRAY FILTER FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR AIRCRAFT WITH 129-5011-1 KIT INSTALLED, SEE 129-5023-3 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

129-5023-3SPRAY NOZZLE INSTALLATION, AIR CYCLE MACHINE MOD FORAIRCRAFT WITH 129-5011-1 INSTALLED

ATA :

1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-198PENDING "RECOMMENDED" SB NO. 2669, ONE 1 KIT PER AIRCRAFTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPRAY NOZZLE WITH A LARGER ORIFICEAND REMOVE THE SPRAY FILTER FOR INSERVICE AIRCRAFT WITH KIT 129-5011-1 INSTALLED.

NOTENOTENOTENOTE:::: AIRCRAFT WITHOUT 129-5011-1 KIT INSTALLED SEE 129-5023-1 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

129-5024-1AIR CONDITIONING COMPRESSOR - SPARES ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-2 THRU UE-143THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR SPARES REQUIREMENTS FOR THEREPLACEMENT OF A/C COMPRESSOR ASSEMBLY, PART NUMBER 102-389006-11, FOR AIRCRAFT WHICHHAVE ALREADY BEEN CONVERTED TO R134A THROUGH THE INSTALLATION OF KIT 129-5020-1 OR -3.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, R314A REFRIGERANT AND RL100S OIL. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

129-5025-1WINDSHIELD REPLACEMENT FOR THE 114-384020-1 WINDSHIELD ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-290THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE NEW HERCULITEWINDSHIELD LH (PILOT) INSTALLATION ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT 101-5041-3 S WILL BE REQUIRED FOR INSTALLATION BUT NOT PART OF KIT. IFCHANGING -1 AND -2 KITS, YOU CAN ORDER 1 EACH 101-5041-1 S KIT (EQUALS 2 EACH101-5041-3 S KIT) TO ACCOMPLISH BOTH WINDSHIELD INSTALLATIONS.

WT. CHANGE : WT: + 3 LBS; ARM: NEGLIGIBLE, MOMENT: + 324 IN.-LBS.EST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

129-5025-2WINDSHIELD REPLACEMENT FOR THE 114-384020-2 WINDSHIELD ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-227THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE NEW HERCULITEWINDSHIELD RH (CO-PILOT) INSTALLATION ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT 101-5041-3 S WILL BE REQUIRED FOR INSTALLATION BUT NOT PART OF KIT. IFCHANGING -1 AND -2 KITS, YOU CAN ORDER 1 EACH 101-5041-1 S KIT (EQUALS 2 EACH101-5041-3 S KIT) TO ACCOMPLISH BOTH WINDSHIELD INSTALLATIONS.

WT. CHANGE : WT: + 3 LBS: ARM: NEGLIGIBLE, MOMENT: + 324 IN.-LBSEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

129-5026-1STRUT ASSEMBLY AIRSTAIR DOOR - SPARES ATA :1900DTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 129-514106-19, -25, -31, -35, -41, -45, OR-49 AIRSTAIR DOOR STRUT ASSEMBLY WITH A XOXOB75-233-717/1400N GAS SPRING, SWITCH RIGGINGAND PROP PITCH CONTROL FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AN960-616 OR 616L WASHER IS NOT FURNISHED WITH THIS KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 1 LBS; MOMENT: 152 IN.-LBS FOR EACH DOOR INSTALLATIONEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-5027-1SWITCH INSTALLATION, ASYMMETRICAL FLAP ATA :1900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-294THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ASYMMETRICAL SWITCH COMPONENTS TOIMPROVE THE SERVICE LIFE OF THE SWITCH MECHANISM ON THE LEFT AND RIGHT WINGS ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MIL-L-7870 LUBRICANT IS NOT FURNISHED WITH THIS KIT, IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 1 LBS; MOMENT: 329 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5027-3SWITCH INSTALLATION, ASYMMETRICAL FLAP ATA :1900 UA-2, UA-31900C UB-1 THRU UB-74THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ASYMMETRICAL SWITCH COMPONENTS TOIMPROVE THE SERVICE LIFE OF THE SWITCH MECHANISM ON THE LEFT AND RIGHT WINGS ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MIL-L-7870 LUBRICANT IS NOT FURNISHED WITH THIS KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : 1 LBS; MOMENT: 329 IN.-LBS.EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-5029-1BLEED AIR TUBE BREAKAGE WARNING SYSTEM ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1 (C-12J) UC-1 THRU UD-61900D UE-1 THRU UE-322THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE CLAMPING OF EVA WARNING TUBES ANDSHORTEN AIRCYCLE WATER DRAIN HOSE IN THE LH WING TO REDUCE SAG, SLOP, AND CHAFING ON IN-SERVICE AIRCRAFT.)

NOTENOTENOTENOTE:::: "URALANE 5776" ADHESIVE, "MIL-S-8802" SEALER, "MS20604AD4W2" OR "CR3213-4-2"RIVET, AND "MS20604AD3W2" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

129-5030-1EXTERIOR MARKING PLACARD ATA :1900D UE-1 THRU UE-268PENDING "MANDATORY" SB NO. 2741THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE EXTERIOR MARKINGSREGARDING DOOR OPENING PROCEDURES ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA3960 EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


129-5031-1LAVATORY SMOKE DETECTOR INSTALLATION ATA :1900D UE-207 THRU UE-299 WITH OPTIONAL

LAVATORY INSTALLED."OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF A LAVATORY COMPARTMENTSMOKE DETECTION SYSTEM FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 608 ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPLICABLE AIRCRAFT FLIGHTMANUAL REVISIONS OR SUPPLEMENTS HAVE BEEN INCORPORATED. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


129-5032-1CREW PROTECTIVE BREATHING PROVISIONS ATA :1900D UE-1 THRU UE-299"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR THOSE AIRCRAFT EQUIPPED WITH FACTORYINSTALLED 101-384220-3 (SCOTT EROS) CREW OXYGEN MASKS. THIS KIT REPLACES EXISTING MASKFACE PIECES TO BE COMPATIBLE WITH SMOKE GOGGLES AND ADDS MATING GOGGLES WITH STORAGEPO

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPLICABLE AIRCRAFT FLIGHTMANUAL REVISION HAS BEEN INCORPORATED. MANUAL REVISION LEVELS SUBSEQUENTTO THOSE NOTED ARE ACCEPTABLE. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.



KIT CATALOG

129-5032-3CREW PROTECTIVE BREATHING PROVISIONS ATA :1900D UE-137 THRU UE-299"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR THOSE AIRCRAFT EQUIPPED WITH FACTORYINSTALLED 128-380067-1 OR -11 (PURITAN-BENNETT, SWEEP ON 2000) CREW OXYGEN MASKS. THOSEMASKS HAVE PROTECTIVE BREATHING PROVISIONS THUS THIS KIT ADDS MATING SMOKE GOGGLES AND



129-5032-5CREW PROTECTIVE BREATHING PROVISIONS ATA :1900D UE-173 THRU UE-299"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR THOSE AIRCRAFT EQUIPPED WITH FACTORYINSTALLED 129-380093-1 (SCOTT 893) CREW OXYGEN MASKS. THIS KIT SUBSTITUTES 129-380020-1(SCOTT 359) CREW OXYGEN MASKS, CHANGES MASK BINS AND ADDS MATING SMOKE GOGGLES ANDSTO



129-5032-7CREW PROTECTIVE BREATHING PROVISIONS ATA :1900D UE-173 THRU UE-299"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION FOR THOSE AIRCRAFT EQUIPPED WITH FACTORYINSTALLED 129-380093-1 (SCOTT 893) CREW OXYGEN MASK. THIS KIT SUBSTITUTES 129-380067-11(PURITAN-BENNETT, SWEEP ON 2000) CREW OXYGEN MASKS, CHANGES MASK BINS AND ADDS MATING




KIT CATALOG

129-5033-1LAVATORY TRASH BIN FIRE EXTINGUISHER, INSTALLATION ATA :1900D UE-207 THRU UE-299 WHICH ARE

EQUIPPED WITH OPTIONAL 129-530010LAVATORY INSTALLED.

"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DISPOSABLE FIRE EXTINGUISHER SYSTEMIN LAVATORY TRASH BIN CONTAINER FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA9309NA ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPLICABLE AIRCRAFT FLIGHTMANUAL REVISIONS OR SUPPLEMENTS HAVE BEEN INCORPORATED. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


129-5035-1COVER, ELECTRIC ELEVATOR TRIM ACTUATOR ATA : 271900D UE-1 THRU UE-246 THAT ARE EQUIPPED

WITH THE ELEVATOR ELECTRIC TRIMOPTION.

"MANDATORY" SB NO. 27-3080THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ELECTRIC ELEVATOR TRIM ACTUATORCOVERS FOR INSERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-5036-1PRESSURIZATION CONTROLLER - SPARES ATA :1900DTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE CABIN PRESSURE CONTROLLER PARTNUMBER 130374-32 WITH AN UPGRADED 130374037. -37 HAS IMPROVEMENTS TO INCREASE DAMAGERESISTANCE OF THE FACE OF THE CONTROLLER ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT REPLACES GUARDS PREVIOUSLY ADDED BY 114-5038-1 OR 129-5017 GUARDINSTALLATION KITS.


129-5037-1SPARES, FLAP ACTUATOR - INFORMATION ONLY ATA :1900D UE-129 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY TO INSTALL A 101-521016-1 IN PLACE OF 129-521050-1. A101-521016-2 IN PLACE OF 129-521050-2. A 50-521222-3 IN PLACE OF 129-521051-1. A 50-521222-4 IN PLACEOF 129-521051-2 FOR FLAP ACTUATOR SPARES FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-5039-11GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74THIS KIT PROVIDES INFORMATION ONLY TO ALLOW THE USE OF DOW CORNING 33 LIGHT GREASE IN THEAILERON TRIM TAB ACTUATOR ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5039-13GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74, UC-1 THRU UC-1741900C (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES INFORMATION ONLY TO ALLOW THE USE OF DOW CORNING 33 LIGHT GREASE ONONE ELEVATOR TRIM TAB ACTUATOR. THIS GEASE CHANGE MAY BE INSTALLED ON EITHER THE LEFT ORRIGHT SIDE. TWO OF THESE KITS ARE REQUIRED IF BOTH SIDES OF THE AIRCRAFT NEED THWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5039-3GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY ATA :1900D UE-1 THRU UE-257THIS KIT PROVIDES INFORMATION ONLY TO ALLOW THE USE OF DOW CORNING 33 LIGHT GREASE INONE ELEVATOR TRIM TAB ACTUATOR. THIS GREASE CHANGE MAY BE INSTALLED ON EITHER THE LEFTOR THE RIGHT SIDE. TWO OF THESE KITS ARE REQUIRED IF BOTH SIDES OF THE AIRCRAFT NEWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5039-5GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY ATA :1900D UE-1 THRU UE-257THIS KIT PROVIDES INFORMATION ONLY TO ALLOW THE USE OF DOW CORNING 33 LIGHT GREASE IN THERUDDER TRIM TAB ACTUATOR ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-5039-7GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY ATA :1900 UA-2 AND UA-31900C UB-1 THRU UB-74 , UC-1 THRU UC-1741900C (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES INFORMATION ONLY TO ALLOW THE USE OF DOW CORNING 33 LIGHT GREASE IN THERUDDER TRIM TAB ACTUATOR ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5039-9GREASE, TRIM TAB ACTUATOR - INFORMATION ONLY ATA :1900C UC-1 THRU UC-1741900C (C-12J) UD-1 THRU UD-6THIS KIT PROVIDES INFORMATION ONLY TO ALLOW THE USE OF DOW CORNING 33 LIGHT GREASE IN THEAILERON TRIM TAB ACTUATOR ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5041-1FIRE EXTINGUISHER RELOCATION AND INSTALLATION - INFORMATIONONLY

ATA :

1900D UC-2 THRU UE-407THIS KIT PROVIDES INFORMATION NECESSARY TO RELOCATE AND INSTALL THE FIRE EXTINGUISHEROUTBOARD TO PROVIDE AISLE CLEARANCE FOR THE HANDLE ON THE NEW REPLACEMENT FIREEXTINGUISHER FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5042-1SEAT INSTALLATION, LH FWD - INFORMATION ONLY ATA :1900D UE-1 THRU UE-117THIS KIT PROVIDES INFORMATION ONLY NECESSARY TO REPLACE 1 LH MODEL 912 PASSENGER SEATWITH 1 LH MODEL 936 SEAT AT STA 189.50 FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: ARM: MOMENT: SEE KIT DRAWINGEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5042-3SEAT INSTALLATION, RH FWD - INFORMATION ONLY ATA :1900D UE-1 THRU UE-117THIS KIT PROVIDES INFORMATION ONLY NECESSARY TO REPLACE 1 RH MODEL 912 PASSENGER SEATWITH 1 RH MODEL 936 SEAT AT STA 189.50 FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: ARM: MOMENT: SEE KIT DRAWINGEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-5042-5SEAT INSTALLATION, LH AFT - INFORMATION ONLY ATA :1900D UE-1 THRU UE-117THIS KIT PROVIDES INFORMATION ONLY NECESSARY TO REPLACE 1 LH MODEL 912 PASSENGER SEATWITH 1 LH MODEL 936 SEAT AT STA 219.50 FOR INSERVICE AIRCRAFT. AIRCRAFT MUST BE EQUIPPEDWITH -1 KIT BEFORE INSTALLING THIS KIT.WT. CHANGE : WT: ARM: MOMENT: SEE KIT DRAWINGEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5042-7SEAT INSTALLATION, RH AFT - INFORMATION ONLY ATA :1900D UE-1 THRU UE-117THIS KIT PROVIDES INFORMATION ONLY NECESSARY TO REPLACE 1 RH MODEL 912 PASSENGER SEATWITH 1 RH MODEL 936 SEAT AT STA 219.50 FOR INSERVICE AIRCRAFT. AIRCRAFT MUST BE EQUIPPEDWITH -3 KIT BEFORE INSTALLING THIS KIT.WT. CHANGE : WT: ARM: MOMENT: SEE KIT DRAWINGEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5043-1ACTUATOR ASSY & INSTL, ELEVATOR TRIM TAB ATA : 271900D UE-2 THRU UE-211SB NO. 27-3032THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE ELEVATOR TRIM TAB ACTUATORS TOINSTALL HELICAL GEARS, PLUG SOME DRAIN HOLES, USE DOW CORNING 33 LIGHT GREASE AND ADDROD SEALS.

NOTENOTENOTENOTE:::: "MS21258-1" SAFETY CLIP-TURNBUCKLE, "MS20995C32" SAFETY WIRE, "LOCTITE 609"RETAINING COMPOUND, "7471" PRIMER, "EC2216" ADHESIVE, "MPK" SOLVENT, 100 GRITSANDPAPER, "33" GREASE & "PD680" CLEANING SOLVENT REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

NOTENOTENOTENOTE:::: THIS IS USED WITH SERIALS THAT HAVE ACTUATOR PART NUMBERS 129-526033-1 OR129-526033-3.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24 HRSMEN : 2 (MEN)


KIT CATALOG

129-5043-11ACTUATOR ASSY & INSTL, ELEVATOR TRIM TAB ATA : 271900D UE-212 THRU UE-257SB NO. 27-3032THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE ELEVATOR TRIM TAB ACTUATORS TOINSTALL HELICAL GEARS, PLUG SOME DRAIN HOLES, USE DOW CORNING 33 LIGHT GREASE, AND ADDROD SEALS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALSO USED ON UE-2 THRU UE-211 THAT HAVE INSTALLED THE 129-526033-5 OR129-526033-6 ACTUATORS AS SPARES.

NOTENOTENOTENOTE:::: "MS21258-1" SAFETY CLIP-TURNBUCKLE, "MS20995C32" SAFETY WIRE, "LOCKTITE 609"RETAINING COMPOUND, "7471" PRIMER, "EC2216" ADHESIVE, "MPK" SOLVENT, 100 GRITSANDPAPER, "33" GREASE & "PD680" CLEANING SOLVENT REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


129-5043-17ACTUATOR ASSY & INSTL, ELEVATOR TRIM TAB ATA : 271900D UE-258 THRU UE-423SB NO. 27-3032THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE ELEVATOR TRIM TAB ACTUATORS TOINSTALL HELICAL GEARS, PLUG SOME DRAIN HOLES, USE DOW CORNING 33 LIGHT GREASE, AND ADDROD SEALS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALSO USED ON UE-2 AND AFTER THAT HAVE ACTUATOR PART NUMBERS 129-526033-7OR 129-526033-9 ACTUATORS AS SPARES.

NOTENOTENOTENOTE:::: "MS21258-1" SAFETY CLIP-TURNBUCKLE, "MS20995C32" SAFETY WIRE, "LOCTITE 609"RETAINING COMPOUND, "7471" PRIMER, "EC2216" ADHESIVE, "MPK" SOLVENT, 100 GRITSANDPAPER, "33" GREASE AND "PD680" CLEANING SOLVENT REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


129-5045-1KIT - MODEL 1900D ZERO FUEL WEIGHT INCREASE (15,700 LBS) ATA :1900D UE-1 THRU UE-423ORDER THROUGH TMDC AT WWW.RACPUBS.COM.WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

129-5046-0001FLAP SAFETY SWITCH, GREASE FITTING INSTL ATA :1900 SERIES UC-1 THRU UC-174, UD-1 THRU UD-6 AND

UE-1 THRU UE-439.THIS KIT PROVIDES INFORMATION TO INSTALL A GREASE FITTING ON THE LEFT AND RIGHT FLAPASYMMETRIC SWITCH ASSEMBLY

NOTENOTENOTENOTE:::: IN ADDITION, COMPLIANCE WITH 14 CFR PART 23.25 AND PART 3.74 MUST BEMAINTAINED. (WEIGHT LIMIT VERSUS AIRCRAFT LOADING).

NOTENOTENOTENOTE:::: THE ABOVE IS AN ESTIMATE BASED ON EXPERIENCED, PROPERLY EQUIPPEDPERSONNEL COMPLYING WITH THIS SERVICE BULLETIN. OCCASIONALLY, AFTER WORKHAS STARTED, CONDITIONS MAY BE FOUND WHICH COULD RESULT IN ADDITIONAL MAN-HOURS


129-5200-1INSTALLATION GROUND FINE SWITCH ATA :1900D UE-1 THRU UE-253PENDING "MANDATORY" SB NO. 2714THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE GROUND FINE SWITCH MOUNTING ANDELECTRICAL CIRCUIT. IT WILL PROVIDE IMPROVED SWITCH RIGGING AND PROP PITCH CONTROL FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUALAND PILOT’S OPERATING REVISIONS (OR SUPPLEMENTS) HAVE BEEN INCORPORATEDAND MAY BE OBTAINED LOCALLY, 129-590000-3D, 129-590000-5C, AND 129-590000-7H.SUGGESTED TOOL LIST: 47907-1, 47386, 90083, 90067, 91002-1, 465199-1 AND 305183.


129-5300-1FIRST AID KIT INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM ATA :1900D UE-1 THRU UE-261"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE FIRST AID KIT.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, FOLLOWING AS REQUIRED ITEM: EA9309 QTADHESIVE, AND 17X005 PT, 1900 GRAY ACRYLIC LACQUER PAINT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: INFORMATION KIT 129-0012-1 WILL FURNISH LIST: FAR PART 121 KITS AND ETC.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)


KIT CATALOG

129-5301-1PLACARD INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM ATA :1900D UE-162, UE-163, UE-165, UE-167, UE-171,

UE-173, UE-174, UE-176, UE-178, UE-179,UE-182, UE-184, UE-190, UE-192, UE-195,UE-218, UE-219, UE-220, UE-224, UE-226,UE-228

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO LOCATE AND INSTALL THE "KEEP SEATFASTENED WHILE SEATED" PLACARD TO THE LEFT AND RIGHT HAND SIDES OF THE CABIN.

NOTENOTENOTENOTE:::: INFORMATION KIT 129-0012-1 WILL FURNISH LIST: FAR PART 121 KITS AND ETC.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5303-1FORWARD PARTITIONS - INFORMATION ONLY ATA :1900D UE-1 AND AFTERTHIS KIT IS FOR THE REMOVAL OF 128-384027-17 POP-UP ON LEFT HAND PARTITION DOOR ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5303-3FORWARD PARTITIONS - INFORMATION ONLY ATA :1900D UE-1 AND AFTERTHIS KIT IS FOR THE REMOVAL OF 128-384027-18 POP-UP ON RIGHT HAND PARTITION DOOR ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5304-1CRASH AXE INSTL, JAR-OPS ATA :1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR THE ADDITION OF A CRASH AXE WITH COVER TO THEFWD RIGHT HAND PARTITION INSIDE THE 1900D COCKPIT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED FLIGHT MANUAL"129-590000-103" REVISION (OR SUPPLEMENT) HAS BEEN INCORPORATED. PROCURESEPARATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: "EA9394NA" ADHESIVE & "242-31" LOCTITE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : WT: 2.86 LBS; MOMENT: 427.86 IN-LB WITH COCKPIT CURTAIN.WT: 2.86 LBS; MOMENT: 425.00 IN-LB WIRH COCKPIT DOOR.



KIT CATALOG

129-5306-1FRAME CHAFING - INFORMATION ONLY ATA :1900D UE-1 THRU UE-380THIS KIT IS FOR INSPECTION FOR POSSIBLE CHAFING AND REWORK OF SCREWS OR REPLACEMENT OFSCREWS IN ALL WINDOW MOLDINGS ON MODEL 1900D AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-5312-1FLASHLIGHT INSTALLATION, CABIN FAR PART 121 COMPLIANCE ITEM ATA :1900D UE-1 THRU UE-261"OPTIONAL" SB NO. 2727THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE FLASHLIGHT HOLDER.

NOTENOTENOTENOTE:::: INFORMATION KIT 129-0012-1 WILL FURNISH LIST: FAR PART 121 KITS AND ETC.WT. CHANGE : WT: 1 LBS; MOMENT: 122 IN.-LBSEST. MAN/HRS: : 1.5MEN : 1 (MAN)

129-5313-1EMERGENCY EXIT LIGHT, HEADLINER ATA :1900D UE-1 THRU UE-367THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL EMERGENCY EXIT LIGHTS INEXISTING HEADLINER PANELS FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA-9309" REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 1.3; MOMENT: 393 IN,-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-5314-1EMERGENCY EXIT LIGHT, JAR-OPS ATA :1900D UE-185 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL EMERGENCY EXIT LIGHTS INEXISTING HEADLINER PANELS TO INCREASE AWARENESS OF EMERGENCY EXIT LOCATIONS FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED FLIGHT MANUAL REVISION (ORSUPPLEMENT) HAS BEEN INCORPORATED. PROCURE SEPARATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: "ALODINE 600" COATING, "EA9309" ADHESIVE & CLEANING SOLVENT REQUIRED, BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : WT: 5 LBS; MOMENT: 1341 IN-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-8002-1BRAKE ASSEMBLY ATA :1900D UE-200 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" NECESSARY TO INSTALL A 114-8008-3 BRAKE ASSEMBLY TOREPLACE A 114-388024-1 BRAKE ASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : WT: 7 LB.; MOMENT: 220 IN.-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-8003-1PISTON & SOCKET SPARES, MAIN LANDING GEAR ATA :1900C-1 UC-168 THRU UC-1741900D UE-3 THRU UE-439THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE AN AXLE & PISTON ASSY FOR THE MLG FORIN-SERVICE MODEL 1900 SERIES AIRCRAFT, OR FOR AIRCRAFT THAT HAVE FLANGED BUSHINGSINSTALLED IN THE SOCKET WHERE THE LOWER TORQUE KNEE ATTACHES. (AXLE & PISTON ASSY,WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-8004-0001MAIN LANDING GEAR ID PLATE INSTALLATION ATA :1900, 1900C, 1900C-1, 1900C-1 (C-12J),1900D

ALL

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW MAIN LANDING GEAR ID PLATE FORALL IN-SERVICE MODEL 1900 SERIES AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-8100-1BRAKE ANTI-SKID INSTALLATION, AIRCRAFT WITHOUT POWERSTEERING

ATA :

1900D UE-2 AND AFTER (WITHOUT POWERSTEERING)

THIS KIT PROVIDES "INFORMATION ONLY" FOR THE INSTALLATION OF ANTI-SKID BRAKE SYSTEM FORINSERVICE AIRCRAFT WITHOUT POWER STEERING SYSTEM ON REFERENCED AIRCRAFT.

NOTENOTENOTENOTE:::: IF PURCHASING THIS KIT FOR GRAVEL RUNWAY OPERATION, YOU MUST ALSO ENSUREAIRCRAFT HAS FACTORY INSTALLED OR REFERENCE KITS INSTALLED IN CONJUNCTIONWITH THIS KIT: 114-4035-3 P GRAVEL RUNWAY KIT AND 129-4001-1 S CABIN WINDOWSGRAVEL RUNWAY INSTALLATION KIT TO GET AIRCRAFT CERTIFIED FOR GRAVELRUNWAY OPERATION.

WT. CHANGE : SEE KIT DRAWING.EST. MAN/HRS: : 48 TO 60MEN : 2 (MEN)


KIT CATALOG

129-8100-3BRAKE ANTI-SKID INSTALLATION, WITH POWER STEERING ATA :1900D UE-2 AND AFTER (WITH POWER

STEERING)THIS KIT PROVIDES PARTS AND INFORMATION FOR THE INSTALLATION OF ANTI-SKID BRAKE SYSTEMFOR INSERVICE AIRCRAFT WITH POWER STEERING SYSTEM INSTALLED ON REFERENCED AIRCRAFT.

NOTENOTENOTENOTE:::: IF PURCHASING THIS KIT FOR GRAVEL RUNWAY OPERATION, YOU MUST ALSO ENSUREAIRCRAFT HAS FACTORY INSTALLED OR REFERENCE KITS INSTALLED IN CONJUNCTIONWITH THIS KIT: 114-4035-3 P GRAVEL RUNWAY KIT AND 129-4001-1 S CABIN WINDOWSGRAVEL RUNWAY INSTALLATION KIT TO GET AIRCRAFT CERTIFIED FOR GRAVELRUNWAY OPERATION.

WT. CHANGE : SEE KIT DRAWINGEST. MAN/HRS: : 40 TO 60MEN : 2 (MEN)

129-9001-3QUICK ENGINE CHANGE ATA :1900D UE-421 THRU UE-439THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO PERFORM A QUICK ENGINE CHANGE ANDALSO INCLUDES INFORMATION NEEDED TO CONVERT THE QUICK ENGINE CHANGE FROM A RIGHT HANDTO A LEFT HAND ENGINE.

NOTENOTENOTENOTE:::: "MS20470AD4" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPARATELYFROM ANY COMPANY AUTHORIZED OUTLET.


129-9002-1 SPLACARD, WARNING INSTALLATION ATA :1900D UE-1 THRU UE-27, WITH A TEMPORARY

REVISION PAGE TO INSERT IN THE 1900DFAA APPROVED AIRPLANE FLIGHTMANUAL PART NUMBER: 129-590000-3C

THIS KIT PROVIDES A PLACARD TO INSTALL ON THE AFT EDGE OF THE GLARESHIELD BETWEEN THEPILOT’S MASTER CAUTION AND THE PILOT’S ENGINE FIRE DETECT ANNUNCIATORS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 0.2MEN : 1 (MAN)

129-9004-1FREON COMPRESSOR QUIL SHAFT, SERVICE EVALUATION ATA :1900D UE-2 THRU UE-6, UE-9, UE-11, UE-13,

UE-14, UE-15, UE-17, UE-18, UE-21, UE-23,UE-26 UE-28, UE-29, UE-31, UE-33, UE-35,UE-37, UE-39, UE-46, UE-48 ONLY.

THIS KIT PROVIDES A PART AND INFORMATION TO INSTALL A SERVICE EVALUATION FREONCOMPRESSOR QUILL SHAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

129-9005-1EXHAUST PIPE, SERVICE EVALUATION ATA :1900D UE-16, UE-20 & UE-25 ONLYTHIS KIT PROVIDES A PART AND INFORMATION TO INSTALL A SERVICE EVALUATION EXHAUST PIPEEFFECTIVE MODEL 1900D.WT. CHANGE : 3 LBS. ARM: 224 MOMENT: 672 IN-LBS.EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-9006-1ENGINE TRUSS REPAIR ATA :1900 UA-2, UA-31900C UB-1 AND AFTER1900C-1 UC-1 AND AFTER1900C-1 (C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES "INFORMATION ONLY" REQUIRED TO REPAIR CRACKED AND DAMAGED ENGINETRUSSES INSTALLED BY KIT 114-9036.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9007-1 SBRUSH BLOCK, HEAVY DUTY, PROP DEICE EVALUATION ATA :1900D UE-2, UE-3, UE-6, UE-9

UE-11 THRU UE-26UE-28 THRU UE-40UE-45 THRU UE-56UE-60, UE-61 AND UE-66

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SERVICE EVALUATION BRUSH BLOCKS ANDSLIP RINGS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PRODUCT SUPPORT, NEEDS TO BE CONTACTED ON ANY PROBLEMS ON THESE KITS ASDEPT. 52, FURNISHED ALL KITS AND ASSIGNED ALL KIT SERIAL NUMBERS REQUIREDFOR INSTALLATION OF THESE SERVICE EVALUATION KITS ON ABOVE REFERENCEAIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS TO HAVE B. F. GOODRICH PARTS INSTALLED ON LH ENGINE AND D.J.MOULDINGS PARTS INSTALLED ON RH ENGINE.



KIT CATALOG

129-9007-3 SBRUSH BLOCK, HEAVY DUTY, PROP DEICE EVALUATION ATA :1900D UE-45 THRU UE-561900D UE-2, UE-3, UE-6, UE-91900D UE-28 THRU UE-401900D UE-60, UE-61 AND UE-661900D UE-11 THRU UE-26THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SERVICE EVALUATION BRUSH BLOCKS ANDSLIP RINGS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CONTACT PRODUCT SUPPORT, ON ANY PROBLEMS ON THESE KITS AS DEPT. 52,FURNISHED ALL KITS AND ASSIGNED ALL SERIAL NUMBERS REQUIRED FORINSTALLATION OF THESE SERVICE EVALUATION KITS ON REFERENCE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS TO HAVE D. J. MOULDINGS PARTS INSTALLED ON LH ENGINE AND B. F.GOODRICH PARTS INSTALLED ON RH ENGINE.


129-9008-1 SGENERATOR WIRING RUB STRIP, AFT COWLING MODIFICATION ATA :1900C UB-1 AND AFTER1900C-1 UC-1 AND AFTER1900C-1(C-12J) UD-1 AND AFTER1900D UE-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL 118-910028-47 LIP ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: FOLLOWING ITEMS REQUIRED TO INSTALL BUT NOT FURNISHED WITH KIT: "MEK"CLEANER AND "5776" URALANE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


129-9009-1 SPROP DEICE HEAVY DUTY BRUSH BLOCK ATA :1900D UE-1 THRU UE-99, UE-101, UE-102"RECOMMENDED" SB NO. 2571THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HEAVY DUTY BRUSH BLOCKS AND SLIP RINGSON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE AD BROCHURE FIGURE 2, FOR ADDITIONAL INFORMATION.NOTENOTENOTENOTE:::: FOR ECONOMICAL ALTERNATIVE SEE 129-9009-3 KIT INSTALLATION, LESS SLIP RINGS.



KIT CATALOG

129-9009-3PROP DEICE HEAVY DUTY BRUSH BLOCK INSTALLATION - LESS SLIPRINGS

ATA :

1900D UE-1 THRU UE-99, UE-101, UE-102"RECOMMENDED" SB NO. 2571THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HEAVY DUTY BRUSH BLOCKS ON THEINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE AD BROCHURE, FIGURE 2, FOR ADDITIONAL INFORMATION.NOTENOTENOTENOTE:::: IF YOU NEED TO REPLACE SLIP RINGS OR DESIRE IMPROVED SLIP RING CHANGE MADE

AT SAME TIME SEE 129-9009-1 S KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

129-9010-1PNEUMATIC SYSTEM MODIFICATION INSTALLATION ATA :1900D UE-1 AND AFTERSB NO. 2591, FOR ALTERNATE METHOD SEE -3 KITTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE PNEUMATIC SYSTEM ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CAN USE "MEK" AS ALT FOR SOLVENT: MIL-C3876 FOR CLEANING USAGE REQUIRED FORTHIS KIT. YOU WILL ALSO REQUIRE 24 "SF" OF INSULATION PART NUMBER: "BS272HH1"PER KIT TO COMPLETE KIT INSTALLATION ON YOUR AIRCRAFT. (3 EACH 4’ X 2’ SHEETS OFINSTALLATION). IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: FOLLOWING NOT FURNISHED WITH KIT BUT REQUIRED. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY: "ALODINE 1000", CHEM-FILM COATING,"002X3W 300 FT RL" OR "002X3W 150 FT RL" PRESSURE SENSITIVE ALUMINUM TAPE AND"EA934NA QT" OR EA9394NA QT" NON-ASBESTOS ADHESIVE. ITEMS AS REQUIREDUSAGE, INDICATES NORMAL STOCK WILL COVER SEVERAL KIT INSTALLATIONS.


129-9010-3PNEUMATIC SYSTEM MODIFICATION REWORK INSTALLATION ATA :1900D UE-1 AND AFTERSB NO. 2591, 12/1/94 . FOR ALTERNATE METHOD SEE -1 KITTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REWORK THE PNEUMATIC SYSTEM ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: YOU WILL ALSO REQUIRE 24 "SF" OF INSULATION PART NUMBER "BS272HH1" PER KIT TOCOMPLETE KIT INSTALLATION ON YOUR AIRCRAFT (3 EACH 4’ X 2’ SHEETS OFINSTALLATION). IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: FOLLOWING ITEMS NOT FURNISHED WITH KIT BUT REQUIRED. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "ALODINE 1000", CHEM-FILMCOATING, "002X3W 150 FT RL" OR "002X3W 300 FT RL" PRESSURE SENSITIVE ALUMINUMTAPE AND "EA934NA QT" OR "EA9394NA QT" NON-ASBESTOS ADHESIVE. ITEMS ASREQUIRED USAGE, INDICATES NORMAL STOCK WILL COVER SEVERAL KITINSTALLATIONS.



KIT CATALOG

129-9011-1GROUND IDLE SYSTEM ATA :1900D UE-1 THRU UE-334THIS KIT PROVIDES PARTS AND INFORMATION FOR GROUND IDLE SYSTEM ANNUNCIATION FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EC801" SEALANT REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPARATELYFROM RAPID OR YOUR LOCAL SUPPLIER.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED A/C FLIGHT MANUAL & PILOT'SOPERATING MANUAL REVISIONS (OR SUPPLEMENTS) HAVE BEEN INCORPORATED.PROCURE FROM RAPID OR YOU LOCAL SUPPLIER.


129-9013-1EXHAUST STACK, RH, 25 DEGREE TILT INSTALLATION ATA :1900D UE-1 THRU UE-225PENDING "MANDATORY" SB NO. 2686THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE RH EXHAUST STACKS ONBOTH ENGINES ON INSERVICE AIRCRAFT, WITH A 25 DEGREE TILTED STACKS.

NOTENOTENOTENOTE:::: PAINT AND CORRECT SIZE MS20426AD4 RIVET (LENGTH TO BE DETERMINED DURINGINSTALLATION). IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 7 LBS, MOMENT: + 1561 IN.-LBSEST. MAN/HRS: : 10MEN : 2 (MEN)

129-9016-1ICE VANE INSTALLATION, INLET ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-292THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN ICE VANE ASSEMBLY IN THEINERTIAL SEPARATOR OF THE AIR INLET ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-9017-1ENGINE TRUSS REPAIR ATA :1900 UA-2 AND UA-3 WITH KIT 114-9045-1, -3 OR

-5 INSTALLED1900C UB-1 THRU UB-74 WITH KIT 114-9045-1, -3

OR -5 INSTALLED.1900C-1 UC-1 THRU UC-174 WITH KIT 114-9045-1, -3

OR -5 INSTALLED.1900C-1 (C-12J) UD-1 THRU UD-6 WITH KIT 114-9045-1, -3

OR -5 INSTALLED.1900D UE-1 THRU UE-166 WITH KIT 114-9045-1, -3

OR -5 INSTALLED.1900D UE-166 AND AFTERTHIS KIT PROVIDES INFORMATION TO REPAIR WELDMENT CRACKS ON 129-910047-1 AND -13 ENGINETRUSS ASSEMBLIES ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

129-9018-1MEGGITT LCD ENCODING ALTIMETER ATA :1900D UE-1 THRU UE-307, UE-308THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF MEGGITT LCD ALTIMETER FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT’S OPERATING HANDBOOK REVISION HAS BEEN INCORPORATED. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: "PS-1440" SEALER REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.


129-9019-1FIRE LOOP CLAMP ATA :1900 UE-15 THRU UE-300THIS KIT PROVIDES INFORMATION ONLY FOR A REPLACEMENT CLAMP FOR THE QUICK DISCONNECTCLAMPS (3 EACH) ON THE FIRELOOP ASSEMBLY NEAR THE ENGINE INTAKE AREA FOR ALL INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9021-1PROPROPELLER SHAFT SEAL DRAIN VALVE ATA :1900D UE-1 THRU UE-325THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL PROPELLER SEAL DRAIN LINESON BOTH ENGINES ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-9023-1FIRE DETECTOR REINFORCEMENT ATA :1900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900C-1(C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-324THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD REINFORCEMENTS TO THE FIREDETECTOR LOOP CABLE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9024-1PROPELLER DE-ICER ATA :1900D UE-1 THRU UE-326THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE 4E3017-1 PROPELLER DE-ICERS WITH THE LOWER WATT DENSITY 4E3400-1 PROPELLER DE-ICERS ON BOTH PROPELLERS ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AIRCRAFT MODIFIED WITH THIS KIT MUST USE THE 129-960032-5 PROPELLER ASSEMBLYFOR SPARES. THIS MODIFIED ASSEMBLY IS NOT INTERCHANGEABLE WITH THE129-960032-1 OR -3 PROPELLER ASSEMBLIES.


129-9024-3PROPELLER DE-ICER - INFORMATION ONLY ATA :1900D UE-1 THRU UE-326THIS KIT PROVIDES "INFORMATION ONLY" TO REPLACE THE 4E3017-1 PROPELLER DE-ICERS WITH THELOWER WATT DENSITY 4E3400-1 PROPELLER DE-ICERS WHICH HAVE HAD THE DE-ICERS ON BOTHPROPELLER ASSEMBLIES REPLACED WITH LOWER WATT DENSITY DE-ICERS AT A PROP REPAIR FAC

NOTENOTENOTENOTE:::: AIRCRAFT MODIFIED WITH THIS KIT MUST USE THE 129-960032-5 PROPELLER ASSEMBLYFOR SPARES. THIS MODIFIED ASSEMBLY IS NOT INTERCHANGEABLE WITH THE129-960032-1 OR -3 PROPELLER ASSEMBLIES.


129-9025-1FUEL PUMP DRAIN ATA :1900, 1900C, 1900C-1, 1900C-1(C-12J) ALL1900D UE-1 THRU UE-395THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DRAIN LINE ON BOTH ENGINES,FROM THE ENGINE DRIVEN FUEL BOOST PUMP TO THE DRAIN MANIFOLD.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

129-9026-1FUEL SYSTEM INSTALLATION ATA :1900C UC-1 THRU UC-1741900C (C-12J) UD-1 THRU UD-61900D UE-1 THRU UE-421THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE AIR-MAZE FUEL FILTERDISCS WITH THE NEW AIR-MAZE FUEL FILTER DISCS ON THE LEFT SIDE FUEL SYSTEM ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9030-1GROUND IDLE SYSTEM ANNUNCIATION REMOVAL ATA :1900D UE-335 TO UE-439 & UE-1 THRU UE-334

WITH KIT 129-9011 INSTALLED.THIS KIT PROVIDES PARTS AND INFORMATION FOR GROUND IDLE SYSTEM ANNUNCIATION REMOVALFOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUALAND PILOT'S OPERATING MANUAL REVISIONS (OR SUPPLEMENTS) HAVE BEENINCORPORATED. THEY MAY BE PURCHASED FROM ANY COMPANY AUTHORIZEDOUTLET. MANUAL REVISION LEVELS SUBSEQUENT TO THOSE NOTED ARE ACCEPTABLE.


129-9100-1ENGINE EXCITER RELOCATION ATA :1900C UC-1 THRU UC-1741900D UE-1 THRU UE-420PRATT AND WHITNEY SBS 14312 & 14322.THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO RELOCATE THE ENGINE EXCITER TO THEFORWARD SIDE OF THE ENGINE BAFFLE FOR BETTER ACCESSIBILITY AND REPLACE THE CURRENTEXCITER CABLES WITH SHORTER CABLES ON ONE ENGINE ONLY ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REWORK OF BOTH ENGINES REQUIRES INSTALLATION OF TWO KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9500-1EXHAUST FLANGE ATA :1900D UE-1 THRU UE-331THIS KIT PROVIDES A SPARE REPLACEMENT FOR THE 129-950000-1 EXHAUST STACK FOR ALL INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

129-9500-3EXHAUST FLANGE ATA :1900D UE-226 THRU UE-3311900D UE-1 THRU UE-225 (WITH KIT 129-9013-1

INSTALLED)THIS KIT PROVIDES A SPARE REPLACEMENT FOR THE 129-950020-1 EXHAUST STACK FOR ALL INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9500-5EXHAUST FLANGE ATA :1900 UA-2, UA-31900C UB-1 THRU UB-741900C-1 UC-1 THRU UC-1741900D UE-1 THRU UE-331THIS KIT ALLOWS THE INSTALLATION OF 129-950033-1 DOUBLERS ON AIRCRAFT THAT HAVE NOT BEENMODIFIED WITH IMPROVED EXHAUST STACKS AS DEFINED BY KIT 129-9500-1 AND -3 ON ALL INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

129-9700-1SURFACE DEICE PRESSURE SWITCH ATA :1900 UE-1 UP TO UE-298THIS KIT PROVIDES "INFORMATION ONLY" TO RELOCATE THE TAIL DEICE PRESSURE SWITCH ATTACHEDTO THE STABILON BEHIND THE PRESSURE BULKHEAD FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MS21042L3 NUT, MS15795-810 WASHER, AN960-10L WASHER, MS35207-263 SCREW, AND114-620025-1 BRACKET REQUIRED BUT NOT FURNISHED WITH THIS KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


140-5058-000FIED SERVICE KIT ATA :

UA-2 AND UA-3, UB-1 THRU UB-74, UC-1THRU UC-174, UD-1 THRU UD-6, AND UE-1THRU UE-439

THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 114-524022-23 UNIVERSAL JOINT FORTHE ELECTRIC ELEVATOR TRIM CONTROL INSTALLATION WITH A COVERED UNIVERSAL JOINT FOR INSERVICE E MODEL 1900, MODEL 1900C AND MODEL 1900D.

MEN : N/A


KIT CATALOG

23-2001-1 SEXTERIOR PLACARDS ATA : 1119, 23, 24THIS KIT INCLUDES INSTRUCTIONS AND A REPLACEMENT SET OF PRESSURE SENSITIVE STANDARDEXTERIOR PLACARDS.

NOTENOTENOTENOTE:::: SPRAY CAN OF PROTECTIVE FINISH PAINT HAS BEEN REMOVED FROM KIT TO PREVENTUNNECESSARY SHIPPING DELAYS. PURCHASE SPRAY PAINT LOCALLY.

NOTENOTENOTENOTE:::: BEECHCRAFT EMBLEM PLACARD IS NOT PART OF THIS KIT, IT WAS DELETED PERCHANGE ORDER "CO E69504 REV: A". ORDER P/N 118663-1 SEPARATELY IF THECUSTOMER DESIRES THIS PLACARD ALSO FOR THE AIRCRAFT.


23-2002-1 SINTERIOR PLACARDS ATA : 1119, 23, 24INCLUDES INSTRUCTIONS AND A REPLACEMENT SET OF EASILY INSTALLED, PRESSURE SENSITIVESTANDARD INTERIOR PLACARDS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : N/A

23-2003-1 SFUEL (MINIMUM AND UNUSABLE FUEL) PLACARD ATA : 1119, 19A, M19, B19 MB-1 THRU MB-65423, A23, A23A, B23, C23 M-1 THRU M-151624, A24 MA-1 THRU MA-368A24R MC-2 THRU MC-150SI. NO. 0624-281 OR SUBSEQUENTTHIS KIT PROVIDES PRESSURE SENSITIVE PLACARDS WITH INFORMATION ON MINIMUM FUEL FORTAKEOFF AND UNUSABLE FUEL. COMPLETE INSTRUCTIONS INCLUDED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 4 (MEN)

23-9-11 SLEADING EDGE REPLACEMENT, WING RIGHT HAND, BONDED ATA : 57A24R, B24R, C24R MC-2 THRU MC-795THESE KITS CONTAIN THE NECESSARY PARTS FOR REPLACING THE ENTIRE LEADING EDGE ASSEMBLYOUTBOARD OF THE FUEL TANK AREA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

23-9-5 SLEADING EDGE REPLACEMENT, WING LEFT HAND, BONDED ATA : 57THIS KIT CONTAINS THE NECESSARY PARTS FOR REPLACING THE ENTIRE LEADING EDGE ASSEMBLYOUTBOARD OF THE FUEL TANK AREA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : 1 (MAN)

23-9-7 SLEADING EDGE REPLACEMENT, WING RIGHT HAND, BONDED ATA : 57A23-19, 19A, B1923, A23, A23A, B23, C23,A23-24THIS KIT CONTAINS THE NECESSARY PARTS FOR REPLACING THE ENTIRE LEADING EDGE ASSEMBLYOUTBOARD OF THE FUEL TANK AREA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

23-9-9 SLEADING EDGE REPLACEMENT, WING LEFT HAND, BONDED ATA : 57A24R, B24R, C24R MC-2 THRU M-C795THIS KIT CONTAINS THE NECESSARY PARTS FOR REPLACING THE ENTIRE LEADING EDGE ASSEMBLYOUTBOARD OF THE FUEL TANK AREA.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

36-5017-1 SFIRE EXTINGUISHER REPLACEMENT "RESTRICTED ARTICLE* ATA :B99, C99 U-146 THRU U-164, U-50, U-165 THRU U-230,

(SEE 99-5023-1, -3, -5 AND -7)SPARES SEE KIT CATALOG FOR AIRCRAFT MODELS AND SERIAL NUMBERS, EXCEPT FOR FOLLOWINGAIRCRAFT LISTED BELOW: REPLACEMENT KITS LISTED BELOW ONLY FOR REFERENCE MODELS.

NOTENOTENOTENOTE:::: IF YOUR AIRCRAFT IS NOT LISTED, ORDER 36-5017-1 S KIT AND REFERENCE YOURAIRCRAFT SERIAL NUMBER ON ORDER SO WE CAN CHECK WITH ENGINEERS ON THATMODEL FOR YOUR IMMEDIATE NEED.

WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

36-5027-1COVER ASSEMBLY, RH CONTROL WHEEL ATA :99A, B99THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 36-530171-23 COVER ASSEMBLY ON IN-SERVICE AIRCRAFT THAT PREVIOUSLY HAD 50-534846-11 PLATE INSTALLED ON THE RH CONTROLWHEEL.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

55-3028-3 PCONTROL WHEEL CLOCK INSTALLATION (28-VOLT) ATA :99, B99THIS KIT MAY BE USED AS SPARES REPLACEMENT FOR 58-380015-3, 50-534622-13, 50-534622-17,50-534622-21, 50-384209-1, 50-384210-1, OR 50-384211-1 8-DAY CLOCKS WHEN USED IN A 28-VOLT SYSTEM.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

90-3106-1 SOIL PRESSURE TRANSDUCER INSTALLATION ATA :19001900C"OPTIONAL" SB NO. 2159, REV. 2 FOR AIRCRAFT SERIAL NUMBER AFFECTED. ALSO SEE SB NO. 1072THIS KIT PROVIDES PARTS AND INFORMATION FOR REPLACEMENT OF ENGINE OIL PRESSURETRANSDUCERS WITH REPLACEMENT TRANSDUCERS WITH GOLD PINS WHICH ALLEVIATE THEPOSSIBILITY OF ANY CORROSION AND ACCOMPANYING FLUCTUATIONS DUE TO ELECTRICAL SIGNALINTERRUPTION ON

NOTENOTENOTENOTE:::: SERVICE BULLETIN NO. 1072 NEEDS TO BE COMPLIED WITH BEFORE 90-3106-1 S KITINSTALLED AS THIS KIT DOES NOT CONTAIN INDICATOR, CLIP OR ETC, 90-3106-1 SFURNISHES IMPROVED TRANSDUCERS AND NECESSARY HARDWARE FOR INSTALLATIONOF SAME. CHECK SERVICE BULLETIN NO.1072 TO SEE IF IT AFFECTS YOUR AIRCRAFTSERIAL NUMBER AND ORDER ACCORDINGLY.

WT. CHANGE : NEGLIGIBLE (1 KIT PER AIRCRAFT)EST. MAN/HRS: : 1MEN : 1 (MAN)

90-4102-1 SSTABILIZER AND FIN SEALING ATA :1900SB NO. 2254 OR SUBSEQUENTTHIS KIT CONSISTS OF PARTS AND INFORMATION FOR MOISTURE PROTECTION AND INSTALLATION OFBONDING JUMPER.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)

90-5065-1 SELEVATOR TRIM TAB CABLE GUARD ATA :1900 UA-1 THRU UA-31900C UB-1 THRU UB-4SB NO. 2028, REV. 3 OR SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN IMPROVED CABLE GUARD ON THEELEVATOR TRIM CABLE DRUM IN THE PEDESTAL.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

99-3038-1 PSERVO AMPLIFIER INSTALLATION - SPARES ATA :19001900CTHIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT FOR THE 513-1 SERVO.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberELECTRICAL BONDING EQUIPMENT - (101-3227-1) 1



ELECTRICAL EQUIPMENT INSTALLATION, FUSELAGE - (122-3000-1 S) 1

AUTOPILOT DISCONNECT AURAL WARNING TONE DISABLE - (122-3001-1 S) 1

AUTOPILOT DISCONNECT AURAL WARNING TONE DISABLE - (122-3001-3 S) 2

EXTERNAL POWER RECEPTACLE INSTALLATION - (122-3002-1 S) 2



DOOR ASSEMBLY, EXTERNAL POWER RECEPTACLE INSTALLATION - (122-3002-9 S) 2

GROSS WEIGHT INCREASE 14,500 LBS. - (122-3003-1 S) 3

COCKPIT VOICE RECORDER INSTALLATION - (122-3004-1 P) 3

COCKPIT VOICE RECORDER INSTALLATION - (122-3004-3 P) 3

FLIGHT DATA RECORDER INSTALLATION - (122-3005-1 P) 3

COCKPIT AUXILIARY MICROPHONE AND JACK INSTALLATION - (122-3008-1 S) 4

CABIN SPEAKER UPDATE, OPEN MESH GRILL USING 2 STANDARD SPEAKERS - (122-3009-1 S) 4

CABIN SPEAKER UPDATE, OPEN MESH GRILL REPLACING 4 STEREO SPEAKERS WITH 6 SPEAKER SYSTEMINSTALLED - (122-3009-3 S)

4

CABIN SPEAKER UPDATE, OPEN MESH GRILL USING 2 STANDARD SPEAKERS - (122-3009-5 S) 5

CABIN SPEAKER UPDATE - (122-3009-7 S) 5

ELT ANTENNA, GROUND PLANE PROVISIONS - (122-3010-1 S) 5

ENTRY LIGHT AND SWITCH ASSEMBLY UPDATE REWIRING - (122-3011-1 S) 6

BLEED AIR CONTROL CIRCUIT BREAKER, REWIRE - (122-3012-1 S) 6

FLUORESCENT LIGHT INSTALLATION, COMPLETE CABIN AREA - (122-3013-1 S) 6

ANTENNA BOOT INSTALLATION - (122-3014-1 S) 6

ANTENNA BOOT INSTALLATION - (122-3014-3) 7

SWITCH INSTALLATION, CABIN DOOR - (122-3015-1 S) 7

SWITCH INSTALLATION, CABIN DOOR - (122-3015-3 S) 7

AUDIO NOISE REDUCTION, CABIN, ENGINE START, PILOT AND PAGING AUDIO - (122-3016-1 S) 8

CABIN NOISE REDUCTION, ENGINE START, PILOT AND PAGING AUDIO - (122-3016-5 S) 8

OVERHEAD FLOOD LIGHT CIRCUIT UPDATE - (122-3017-1 S) 8

BATTERY 45 AMP HOUR, INSTALLATION (WITH BATTERY) - (122-3018-1 S) 9

BATTERY 45 AMP HOUR, INSTALLATION (WITHOUT BATTERY) - (122-3018-3) 9

BATTERY ASSISTED AIR START INSTALLATION - (122-3019-1 S) 9

BATTERY ASSISTED AIR START INSTALLATION - (122-3019-5) 9

ANTENNA INSTALLATION, NAV VOR - (122-3020-1 S) 10

ANTENNA INSTALLATION, NAV, VOR LIMITATION REMOVAL - (122-3020-3 S) 10

EMI SUPPRESSION, AVIONICS INSTALLATION - (122-3021-1 S) 10



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberELECTRIC TRIM RETROFIT (YAW, ROLL AND PITCH TRIM PCB UPDATE) - (122-3022-1 S) 11

ELECTRIC TRIM RETROFIT - (122-3022-5) 11

CABIN LIGHTS - (122-3023-1) 11

BAGGAGE LIGHT TIMER INSTALLATION-AFT BAGGAGE AREA - (122-3024-1) 11

BAGGAGE LIGHT TIMER INSTALLATION-AFT BAGGAGE AREA - (122-3024-3) 12

NOSE GEAR CENTERING SQUAT SWITCH - (122-3026-1) 12

POWER PANEL ASSEMBLY - SPARES - (122-3027-1) 12

EMERGENCY EXIT MODIFICATION - (122-4001-1 S) 12

STRUCTURAL REPAIR ADHESIVE, *RESTRICTED ARTICLES* - (122-4002-1 S) 13

STRUCTURAL REPAIR, UPPER WING SKIN - (122-4002-101 S) 13




STRUCTURAL REPAIR, WING ROOT RIB - (122-4002-111 S) 14

STRUCTURAL REPAIR, MAIN LANDING GEAR SPAR - (122-4002-113 S) 14



STRUCTURAL REPAIR, WING FORWARD SPAR - (122-4002-121 S) 14

STRUCTURAL REPAIR, WING AFT SPAR - (122-4002-125 S) 15

STRUCTURAL REPAIR, WING AFT OUTBOARD SPAR - (122-4002-129 S) 15

STRUCTURAL REPAIR, WING AFT INBOARD SPAR - (122-4002-137 S) 15

STRUCTURAL REPAIR, WING FUEL TANK SKINS - (122-4002-139 S) 15

STRUCTURAL REPAIR, FORWARD WING STRUCTURE - (122-4002-141 S) 15

STRUCTURAL REPAIR, TIPSAIL INBOARD SKIN - (122-4002-145 S) 16




STRUCTURAL REPAIR, TIPSAIL OUTBOARD SKIN - (122-4002-157 S) 16



STRUCTURAL REPAIR, ELEVON, ELEVATOR, RUDDER AND FLAP - (122-4002-163 S) 17

STRUCTURAL REPAIR, NACELLE FORWARD LOWER SKIN - (122-4002-165 S) 17

STRUCTURAL REPAIR, NACELLE CENTER LOWER SKIN - (122-4002-167 S) 17

STRUCTURAL REPAIR, NACELLE AFT SKIN - (122-4002-169 S) 18

STRUCTURAL REPAIR, NACELLE ACCESS DOORS - (122-4002-171 S) 18

STRUCTURAL REPAIR, ALL LANDING GEAR DOORS - (122-4002-173 S) 18

STRUCTURAL REPAIR, TIPSAIL LEADING EDGE - (122-4002-207 S) 18



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSTRUCTURAL REPAIR, VENTRAL STABILIZER LEADING EDGE - (122-4002-209 S) 19

STRUCTURAL REPAIR, LOWER FORWARD, UPPER AND LOWER AFT COWLING, EXTERIOR - (122-4002-211 S) 19

STRUCTURAL REPAIR, LOWER FORWARD, UPPER AND LOWER AFT COWLING INTERIOR - (122-4002-217 S) 19

STRUCTURAL REPAIR, LOWER FORWARD, UPPER AND AFT COWLING INTERIOR - (122-4002-219 S) 19

STRUCTURAL REPAIR, LOWER FORWARD, UPPER AND LOWER AFT COWLING, EXTERIOR - (122-4002-221 S) 20

STRUCTURAL REPAIR, LOWER FORWARD, UPPER AND AFT COWLING, INTERIOR - (122-4002-225 S) 20

STRUCTURAL REPAIR, UPPER FORWARD COWLING, EXTERIOR - (122-4002-227 S) 20

STRUCTURAL REPAIR, UPPER FORWARD COWLING, INTERIOR - (122-4002-231 S) 20

STRUCTURAL REPAIR, CABIN ENTRY DOOR - (122-4002-29 S) 21

STRUCTURAL REPAIR, FUSELAGE SHELL - (122-4002-3 S) 21

STRUCTURAL REPAIR, F.S. 46 BULKHEAD - (122-4002-37 S) 21

STRUCTURAL REPAIR, F.S. 18 BULKHEAD - (122-4002-41 S) 21

STRUCTURAL REPAIR, NOSE SECTION B.L.D. 8.5 KEEL - (122-4002-43 S) 21

STRUCTURAL REPAIR, NOSE SECTION B.L.D. KEEL - (122-4002-47 S) 22

STRUCTURAL REPAIR, NOSE SECTION B.L.D MID KEEL - (122-4002-49 S) 22

STRUCTURAL REPAIR, NOSE SECTION AVIONICS DOOR - (122-4002-51 S) 22

STRUCTURAL REPAIR, NOSE SECTION CHECK SKIN DOOR - (122-4002-53 S) 22

STRUCTURAL REPAIR, NOSE SECTION INTER-SHELF CONNECT BEAMS - (122-4002-57 S) 22

STRUCTURAL REPAIR, NOSE SECTION FORWARD SKIN - (122-4002-59 S) 23

STRUCTURAL REPAIR, AFT FUSELAGE - (122-4002-63 S) 23

STRUCTURAL REPAIR, VENTRAL STABILIZER - (122-4002-65 S) 23

STRUCTURAL REPAIR, LOWER WING SKIN - (122-4002-67 S) 23















RIB ATTACHMENT FLAP COVE - (122-4003-1 S) 26



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberRIB ATTACHMENT FLAP COVE - (122-4003-3 S) 27

SOUND REDUCTION MODIFICATION - (122-4005-1 S) 27

SOUND REDUCTION MODIFICATION - (122-4006-1 S) 27

RIB ATTACHMENT, CENTER TRACK FLAP - (122-4007-1 S) 28

LENS LANDING LIGHT, HARD COATED (LH AND RH SIDES) - SPARES - (122-4008-1 P) 28

FUSELAGE DRAINAGE IMPROVEMENT BL 0.00 - (122-4009-1 S) 28

HANDRAIL ASSEMBLY DOOR MOD, TORSION SPRING IMPROVEMENT - (122-4010-1 S) 28

EROSION BOOT, VERTICAL STABILIZER - (122-4011-1 S) 29

RADOME, LIGHTNING DIVERTER STRIP - (122-4015-1) 29

RADOME, LIGHTNING DIVERTER STRIP - (122-4015-3) 29

DOOR REINFORCEMENT CABIN FOR MAJOR DELAMINATIONS/DISBONDS WITH TEC SUPPORT - (122-4016-1) 29

DOOR REINFORCEMENT CABIN FOR MAJOR DELAMINATIONS/DISBONDS WITH TEC SUPPORT - (122-4016-3) 30

REINFORCEMENT, CABIN DOOR - (122-4017-1) 30

MODIFICATION, FWD MAIN GEAR CLOSURE PANEL - (122-4018-1) 30

RIB ATTACHMENT, CENTER FLAP TRACK - (122-4019-1) 30

RIB ATTACHMENT, CENTER FLAP TRACK - (122-4019-3) 31

MODIFICATION, FORWARD MAIN GEAR CLOSURE PANEL - (122-4020-1 S) 31

BLEED AIR VALVE AND CONTROLLER CHANGE - (122-5003-1 S) 31

UPHOLSTERED PANEL CHANGE ESCAPE HATCH - (122-5004-1 S) 31

UPHOLSTERED PANEL CHANGE ESCAPE HATCH - (122-5004-3 S) 32

TRACK ROLLER MODIFICATION, CREW SEAT - (122-5005-1 S) 32

PEDESTAL SHROUD, CABIN CHAIR - (122-5006-1 S) 32

AIR OUTLET UPDATE, CABIN OVERHEAD - (122-5007-1 S) 32

AIR OUTLET UPDATE, CABIN OVERHEAD - (122-5007-3 S) 32

FLAP BUSHING REPLACEMENT - (122-5008-1 S) 33

CABIN WINDOW DEFOG SYSTEM UPDATE WITH WINDOWS - (122-5009-1 S) 33

CABIN WINDOW DEFOG SYSTEM UPDATE (LESS WINDOW) - (122-5009-3 S) 33

CLOSURE INSTALLATION ENVIRONMENTAL DOME - (122-5011-1 S) 33

CABIN DOOR FRAME INSTALLATION - (122-5012-1 S) 33

5 OHM ADJUSTABLE RESISTER AND 12V CLUTCH COIL, COMPRESSOR MOD - (122-5013-1 S) 34

EVAPORATOR COIL INSTALLATION - (122-5015-1 S) 34

CABIN PAGING AND STEREO SPEAKER INSTALLATION - (122-5016-1 S) 34

CABIN WINDOW, DUAL PANE, ANTI-FOG - (122-5017-1 S) 34



COMPRESSOR ASSEMBLY, AIR CONDITIONER CHANGE - (122-5018-1 S) 35

WINDOW INSTALLATION, MANUAL POLARIZED WINDOW MOD - (122-5019-1 S) 35



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberCABIN TEMPERATURE TRANSDUCER RELOCATION, FORWARD CABIN - (122-5022-1 S) 35

THIRD ICE DETECTOR INSTALLATION - (122-5024-1 S) 36

PASSENGER OXYGEN SYSTEM, MASK DROPOUT FUNCTION UPDATE - (122-5025-1 S) 36

PASSENGER OXYGEN SYSTEM, MASK DROPOUT FUNCTION UPDATE - (122-5025-3 S) 36

FAIRLEAD RUDDER CABLE INSTALLATION, F.S. 196.63 - (122-5026-1 S) 36

ICE CHEST (REMOVABLE) INSTALLATION - (122-5027-1 P) 37

AIRSTAIR DOOR FRAME, OVERHEAD BUMPER PAD INSTALLATION - (122-5028-1) 37

SOUND DAMPENER BAGGAGE AREA - (122-5029-1) 37



REFRIGERANT CHANGE AIR CONDITIONING - (122-5030-1) 38

WINDOW DESSICANT SYSTEM - (122-5031-1) 38



DRAIN IMPROVEMENT, AFT EVAPORATOR CONDENSATION - (122-5034-1) 39

OVERPRESSURE PROTECTION, HYDRAULIC POWER PACK - (122-5036-1) 39

WHEEL BEARING, MAIN LANDING GEAR ANTISKID IMPROVEMENT - (122-8001-1 S) 39

CHARGE VALVE RELOCATION POWER BRAKE ACCUMULATOR - (122-8002-1) 40

DRAIN MAST, LONGER - (122-9001-1 S) 40

GROSS WEIGHT INCREASE MOD 2000 TO 2000A LIMITS - (122-9002-1 S) 40

GROSS WEIGHT INCREASE MOD 2000 TO 2000A LIMITS - (122-9002-3 S) 41

PLACARD INSTALLATION - GLARESHIELD AFT EDGE PILOT SIDE - (122-9004-1 S) 41

BRACKET ASSEMBLY REWORK, THROTTLE CONTROL CABLE - (122-9005-1) 41


KIT CATALOG



101-4310-1PLACARD INSTALLATION, EMERGENCY EXIT ATA : 522000 NC-4 THRU NC-53"MANDATORY" SB NO. 52-3096THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL AN AIRSTAIR DOOR OPERATINGINSTRUCTIONS PLACARD ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

122-3000-1 SELECTRICAL EQUIPMENT INSTALLATION, FUSELAGE ATA :2000 NC-4, NC-6 THRU NC-9THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD CABIN READING AND TABLE LIGHTCIRCUIT BREAKERS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

122-3001-1 SAUTOPILOT DISCONNECT AURAL WARNING TONE DISABLE ATA :2000 NC-4 THRU NC-15THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT FOR AUTOPILOTDISCONNECT AURAL WARNING TONE DISABLE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 18MEN : 1 (MAN)


KIT CATALOG

122-3001-3 SAUTOPILOT DISCONNECT AURAL WARNING TONE DISABLE ATA :2000 NC-16 THRU NC-22THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT FOR AUTOPILOTDISCONNECT AURAL WARNING TONE DISABLE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 18MEN : 1 (MAN)

122-3002-1 SEXTERNAL POWER RECEPTACLE INSTALLATION ATA :2000 NC-4 THRU NC-13THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE EXTERNAL POWER RECEPTACLE IN THELH WING LEADING EDGE FROM THE WING CENTER SECTION AT FS 400.50.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 18MEN : 1 (MAN)

122-3002-3 SEXTERNAL POWER RECEPTACLE INSTALLATION ATA :2000 NC-14 THRU NC-29THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE EXTERNAL POWER RECEPTACLE IN THELH WING LEADING EDGE FROM THE WING CENTER SECTION AT FS 400.50.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 18MEN : 1 (MAN)

122-3002-7 SEXTERNAL POWER RECEPTACLE INSTALLATION ATA :2000 NC-5, NC-26 THRU NC-29THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE EXTERNAL POWER RECEPTACLE IN THELH LEADING EDGE AT FS 400.50 ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)

122-3002-9 SDOOR ASSEMBLY, EXTERNAL POWER RECEPTACLE INSTALLATION ATA :2000 NC-4, NC-6 THRU NC-25 WITH 122-3002-1 S

KIT INSTALLEDTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE NEW DOOR ASSEMBLY ANDSUPPORT ASSEMBLY TO THE EXTERNAL POWER RECEPTACLE IN THE LH WING LEADING EDGE FROMTHE WING CENTER SECTION AT FA 400, 50 ON AIRCRAFT THAT HAVE ALREADY INSTALLED KIT 122WT. CHANGE : WT: 20 LBS; ARM: 393; MOMENT: 7860 IN.-LBSEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)


KIT CATALOG

122-3003-1 SGROSS WEIGHT INCREASE 14,500 LBS. ATA :2000 NC-4 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE ECD-870 EICAS AND MFD-870 MULTI-FUNCTION DISPLAY IN THE INSTRUMENT PANEL AND REQUIRED FLIGHT MANUALS FOR INCREASEDGROSS WEIGHT TO 14,500 LBS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)

122-3004-1 PCOCKPIT VOICE RECORDER INSTALLATION ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A VOICE RECORDER BETWEENFS 430.00 AND FS 450.00 ON INSERVICE AIRCRAFT WITHOUT DOUBLE WIDE PEDESTAL WITH PROVISIONSFOR FDR AND HF CONTROLLERS.

NOTENOTENOTENOTE:::: REVISED KIT HAS LATEST SOLID STATE VOICE RECORDER SYSTEM FOR OVERALLIMPROVEMENT IN LIFE AND RELIABILITY OF THE SYSTEM.

NOTENOTENOTENOTE:::: AUDIO AMPLIFIER 418 (2 EACH) TO BE REMOVED FROM AIRCRAFT AND RETURNED TORAYTHEON AS CORES AGAINST 2 EACH AUDIO AMPLIFIER P/N: "DB438 OVH" YOU NEEDTO ORDER AT THE SAME TIME YOU ORDER THIS KIT TO COMPLETE INSTALLATION ASSOON AS POSSIBLE.

WT. CHANGE : WT: 37.5 LBS; MOMENT: 14871.4 IN.-LBSEST. MAN/HRS: : 90 TO 120MEN : 1 (MAN)

122-3004-3 PCOCKPIT VOICE RECORDER INSTALLATION ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES INFORMATION AND PARTS TO INSTALL A VOICE RECORDER BETWEEN FS 430.00 ANDFS 450.00 WITH PROVISIONS IN DOUBLE WIDE PEDESTAL EXTENSION FOR FDR AND HF CONTROLLERSON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AUDIO AMPLIFIER 418 (2 EACH) TO BE REMOVED FROM AIRCRAFT AND RETURNED TORAYTHEON AS CORES AGAINST 2 EACH AUDIO AMPLIFIER P/N: "DB438 OVH" YOU NEEDTO ORDER AT THE SAME TIME YOU ORDER THIS KIT TO COMPLETE INSTALLATION ASSOON AS POSSIBLE.

NOTENOTENOTENOTE:::: REVISED KIT HAS LATEST SOLID STATE VOICE RECORDER FOR OVERALL IMPROVEMENTIN LIFE AND RELIABILITY OF THE SYSTEM.

WT. CHANGE : WT: 38.5 LBS; MOMENT: 15009.6EST. MAN/HRS: : 90 TO 120MEN : 1 (MAN)

122-3005-1 PFLIGHT DATA RECORDER INSTALLATION ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLIGHT DATA RECORDER SYSTEM ONINSERVICE AIRCRAFT.WT. CHANGE : WT: 58 LBS; MOMENT: 19.782 IN.-LBSEST. MAN/HRS: : 120 TO 130MEN : 1 (MAN)


KIT CATALOG

122-3008-1 SCOCKPIT AUXILIARY MICROPHONE AND JACK INSTALLATION ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SUBPANEL MOUNTED HEADSET ANDMICROPHONE JACK. WHEN FORWARD HEADSET AND BOOM MIC ARE PLUGGED IN, THE AFT CONSOLEHEADSET AND MIC ARE DISABLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

122-3009-1 SCABIN SPEAKER UPDATE, OPEN MESH GRILL USING 2 STANDARDSPEAKERS

ATA :

2000 NC-4 THRU NC-20STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OPEN MESH GRILLS, SUPPORTS, ANDENCLOSURES TO ALLOW UNDISTORTED SOUND TO BE DELIVERED TO THE CABIN AREA USING THE 2STANDARD SPEAKERS DELIVERED WITH THE AIRCRAFT OR FOR YOU TO PURCHASE ALTERNATESPEAKERS

NOTENOTENOTENOTE:::: THIS KIT DOES NOT CONTAIN ANY SPEAKERS. TAKES ONE KIT PER AIRCRAFT. IF YOUHAVE AIRCRAFT WITH OPTIONAL 6 SPEAKER STEREO SYSTEM SEE -3 S KIT. IF NC-21 ANDAFTER, SEE -5 S OR -7 S KITS.


122-3009-3 SCABIN SPEAKER UPDATE, OPEN MESH GRILL REPLACING 4 STEREOSPEAKERS WITH 6 SPEAKER SYSTEM INSTALLED

ATA :

2000 NC-4 THRU NC-20STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SPEAKERS, OPEN MESH GRILLS, SUPPORTS,AND ENCLOSURES TO ALLOW UNDISTORTED SOUND TO BE DELIVERED TO THE CABIN AREA ONINSERVICE AIRCRAFT WITH 6 SPEAKER STEREO SYSTEM INSTALLED. THIS KIT CONTAINS 4 REPLACEM

NOTENOTENOTENOTE:::: ACCEPTABLE TO USE SPEAKERS KFC-HQ100 OR KFC-HQ102 OR KFC-1074 FOR FIRSTISSUE KIT OR SPARES. (P/N OF KENWOOD CORPORATION, LONG BEACH, CALIFORNIA).

WT. CHANGE : WT: 8 LBS @ 2274 MOMENTEST. MAN/HRS: : 6 TO 10MEN : 1 (MAN)


KIT CATALOG

122-3009-5 SCABIN SPEAKER UPDATE, OPEN MESH GRILL USING 2 STANDARDSPEAKERS

ATA :

2000 NC-21 THRU NC-35STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OPEN MESH GRILLS, SUPPORTS, ANDENCLOSURES TO ALLOW UNDISTORTED SOUND TO BE DELIVERED TO THE CABIN AREA USING THE 2STANDARD SPEAKERS DELIVERED WITH THE AIRCRAFT OR FOR YOU TO PURCHASE ALTERNATESPEAKERS

NOTENOTENOTENOTE:::: THIS KIT DOES NOT CONTAIN ANY SPEAKERS. TAKES ONE KIT PER AIRCRAFT. IF YOUHAVE AIRCRAFT WITH OPTIONAL 6 STEREO SPEAKERS SYSTEM SEE -7 S KIT.


122-3009-7 SCABIN SPEAKER UPDATE ATA :2000 NC-21 AND AFTERSTARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OPEN MESH GRILLS, SUPPORTS, ANDENCLOSURES TO ALLOW UNDISTORTED SOUND TO BE DELIVERED TO THE CABIN AREA USING THE 6STEREO SPEAKERS DELIVERED WITH THE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT CONTAIN ANY SPEAKERS. ONE KIT PER AIRCRAFT. FOR AIRCRAFTWITH STANDARD 2 SPEAKER SYSTEM SEE 122-3009-5 S KIT. FOR SERIAL NUMBERSBELOW NC-21, SEE 122-3009-1 S OR 122-3009-3 S KITS.

NOTENOTENOTENOTE:::: ACCEPTABLE TO USE SPEAKERS KFC-HQ100 OR KFC-HQ102 OR KFC-1074 FOR FIRSTISSUE KIT OR SPARES. (P/N OF KENWOOD CORPORATION, LONG BEACH, CALIFORNIA).

WT. CHANGE : WT: 8 LBS @ 277.25EST. MAN/HRS: : 6 TO 10MEN : 1 (MAN)

122-3010-1 SELT ANTENNA, GROUND PLANE PROVISIONS ATA :2000 NC-4 THRU NC-25THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A GROUND PLANE FOR NAVAND ELT ANTENNAS.

NOTENOTENOTENOTE:::: YOU WILL ALSO REQUIRE SOME TRICLOROETHANE SOLVENT TO CLEAN SURFACE AREAYOU WILL BE WORKING ON. RAYTHEON RECOMMENDS P/N: 'MEK IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY, A LESS TOXIC MATERIAL PER TT-M-261 EQUIVALENT.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR INSTALLATION BUT ARE NOTFURNISHED WITH THE KIT: P/N: EC2084, SEALER 5 OZ "RA", P/N: ALODINE 1200 COATING 1OZ "RA, P/N: "890B1/2 6 OZ TU" OR "890B1/2 QT" OR "890B2 PRO-SEAL" WHICH IS WHAT "P/N 890BA" SHOWN ON BASIC KIT DRAWING INDICATES. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-3011-1 SENTRY LIGHT AND SWITCH ASSEMBLY UPDATE REWIRING ATA :2000 NC-4 THRU NC-25THIS KIT PROVIDES "INFORMATION ONLY" TO REWIRE THE ENTRY LIGHT AND SWITCH ASSEMBLY TOCHANGE THE LED LAMP ASSEMBLY TO ILLUMINATE WHEN THE SWITCH IS PRESSED TO THE "ON"POSITION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 2MEN : 1 (MAN)

122-3012-1 SBLEED AIR CONTROL CIRCUIT BREAKER, REWIRE ATA :2000A NC-26 THRU NC-44THIS KIT PROVIDES "INFORMATION ONLY" TO REWIRE THE LEFT AND RIGHT BLEED AIR CIRCUITBREAKERS TO PREVENT A LOSS OF CABIN PRESSURIZATION IN THE EVENT OF AN INTERNAL SHORT INTHE ENVIRONMENTAL SYSTEM CONTROLLER.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)

122-3013-1 SFLUORESCENT LIGHT INSTALLATION, COMPLETE CABIN AREA ATA :2000 NC-4 THRU NC-202000/2000A NC-4 THRU NC-42THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE CABIN AREA LIGHTINGINSTALLATION TO FLUORESCENT LIGHTING ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOLLOWING ITEMS REQUIRED FOR INSTALLATION BUT ARE NOT PART OF THIS KIT.SEALER P/N: "EA9309 QT", METHYL-ETHYL P/N: "MEK" AND PRO-SEAL 890 P/N: "890B1/2QT" OR "890B2" WHICH ALSO COMES IN "QT" QUANTITY.


122-3014-1 SANTENNA BOOT INSTALLATION ATA :2000 NC-14 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO THE ANTENNA INSTALLATION AREAS ONINSERVICE AIRCRAFT WITH THE ADDITION OF BOOTS.

NOTENOTENOTENOTE:::: FOR MODEL 2000 NC-4 THRU NC-13 SEE 122-3014-3 KIT.NOTENOTENOTENOTE:::: IT IS RECOMMENDED THAT KIT 122-4009 BE INSTALLED ON AIRCRAFT WHEN THIS KIT IS

INSTALLED.NOTENOTENOTENOTE:::: MEK SOLVENT AND RTV738 SEALER WILL BE NEEDED TO INSTALL THIS KIT. IF NOT

AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.WT. CHANGE : N/AEST. MAN/HRS: : 48 TO 50MEN : 1 (MAN)


KIT CATALOG

122-3014-3ANTENNA BOOT INSTALLATION ATA :2000 NC-4 THRU NC-13THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE ANTENNA INSTALLATIONAREAS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR NC-14 AND AFTER SEE KIT 122-3014-1 S.NOTENOTENOTENOTE:::: MEK SOLVENT AND RTV738 SEALANT WILL BE REQUIRED TO INSTALL THIS KIT. IF NOT

AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.NOTENOTENOTENOTE:::: IT IS RECOMMENDED THAT KIT 122-4009 BE INSTALLED ON AIRCRAFT WHEN THIS KIT IS

BEING INSTALLED.WT. CHANGE : N/AEST. MAN/HRS: : 48 TO 50MEN : 1 (MAN)

122-3015-1 SSWITCH INSTALLATION, CABIN DOOR ATA :2000 NC-4 THRU NC-24THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL LOW FORCE SWITCHES IN THECABIN DOOR FRAME AS WELL AS PROVIDE ADDITIONAL ADJUSTMENT FOR THESE SWITCHES. IT ALSOPROVIDES FOR AN IMPROVED LOCATION FOR THE UPPER CENTER PIN SWITCH ON INSERVICE AIR

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR USE WITH THIS KIT, IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY . "890 PINT"PRO-SEAL890, "LOCTITE242 BONDING CEMENT AND "LOCQUIC PRIMER N" PRIMER.


122-3015-3 SSWITCH INSTALLATION, CABIN DOOR ATA :2000 NC-252000A NC-26 THRU NC-52THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL LOW FORCE SWITCHES INTHE CABIN DOOR FRAME (ADDITIONAL ADJUSTMENT ALREADY INSTALLED ON NC-25 THRU NC-52) ANDALSO AN IMPROVED LOCATION FOR THE UPPER CENTER PIN SWITCH.

NOTENOTENOTENOTE:::: 890 PINT PRO-SEAL 890 SEALANT WILL BE REQUIRED FOR USE WITH THIS KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-3016-1 SAUDIO NOISE REDUCTION, CABIN, ENGINE START, PILOT AND PAGINGAUDIO

ATA :

2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REWIRE THE PILOTS AUDIO AMPLIFIERAND THE CABIN PAGING AMPLIFIER TO REDUCE OBJECTIONABLE CABIN NOISE DURING ENGINE STARTFOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING TOOLS WILL BE REQUIRED FOR INSTALLATION OF THIS KIT:M81969/14-03 INSERT-EXTRACT TOOL, M22520/5-100 AND M 22520/5-103 CRIMP DIE,M22520/1-01 AND M22520/5-01 CRIMP TOOL, M22520/1-02 TURRET HEAD (1 OF EACH) ANDSN60WRMAP3.031 SOLDER (FED QQ-S-571, CMPSN: SN60WRMAP3). IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-3016-5 SCABIN NOISE REDUCTION, ENGINE START, PILOT AND PAGING AUDIO ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REWIRE THE PILOTS AUDIO AMPLIFIER AND THE CABINPAGING AMPLIFIER TO REDUCE OBJECTIONABLE CABIN NOISE DURING ENGINE START FOR INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: SEE INFORMATION ON -1BS KIT FOR ADDITIONAL ITEMS REQUIRED TO INSTALL -1 OR -5 SKIT ON AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS THE SAME AS KIT 122-3016-1 S EXCEPT THE -7 LOOSE WIRE SET FOR -5 S KITINSTALLATION REPLACES THE -3 LOOSE WIRE SET FURNISHED WITH 1 S KIT.


122-3017-1 SOVERHEAD FLOOD LIGHT CIRCUIT UPDATE ATA :2000 NC-4 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION TO PREVENT HOT BATTERY BUS FROM FEEDINGTHROUGH TRIPLE FED BUS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: INSTALLATION AGENCY IS TO SUPPLY SOLDER (FED QQ-S-571, COMPSN:SN60WRMAP3)P/N: SN60WRMAP3.031 OR EQUIVALENT AND TO REPLACE OR ADD HEAT SHRINK TUBINGAS REQUIRED. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-3018-1 SBATTERY 45 AMP HOUR, INSTALLATION (WITH BATTERY) ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY INSERVICE AIRCRAFT, BY INSTALLING LARGER45 AMP HOUR BATTERY AND REMOVING SMALLER BATTERY AND BATTERY COOLING SYSTEM.

NOTENOTENOTENOTE:::: O22854 BATTERY REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 7.0 LBS: ARM: NEG.; MOMENT: 29.12 IN.-LBSEST. MAN/HRS: : 8MEN : 1 (MAN)

122-3018-3BATTERY 45 AMP HOUR, INSTALLATION (WITHOUT BATTERY) ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY INSERVICE AIRCRAFT, BY INSTALLINGHARDWARE REQUIRED FOR INSTALLING A LARGER 45 AMP BATTERY AND REMOVING SMALLER BATTERYAND BATTERY COOLING SYSTEM. THIS KIT DOES NOT INCLUDE THE 022854 BATTERY.

NOTENOTENOTENOTE:::: IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.WT. CHANGE : WT: 7.0 LBS; ARM: NEG.; MOMENT: 29.12 IN.-LBSEST. MAN/HRS: : 8MEN : 1 (MAN)

122-3019-1 SBATTERY ASSISTED AIR START INSTALLATION ATA :2000 NC-5 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE AND INSTALL NEW POWER PANELS ANDREWIRE START RELAY TO PROVIDE BATTERY ASSISTED AIR START FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS NO LONGER OFFERED, IT HAS BEEN DELETED FROM DRAWING. SEE122-3019-5 FOR REPLACEMENT KIT WHICH DOES NOT INCORPORATE ALL THEMODIFICATIONS THE -1 S KIT WOULD HAVE REQUIRED.


122-3019-5BATTERY ASSISTED AIR START INSTALLATION ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE OLD 122-389020-3 POWER PANELS ANDINSTALL NEW 122-389020-7 POWER PANELS AND REWIRE THE START RELAY TO PROVIDE BATTERYASSISTED AIR START FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED TO COMPLETE INSTALLATION, EITHER122-389020-7 POWER PANELS (3 EACH) OR 99-3406, 99-3407, 99-3408, 99-3409 AND 99-3410EATON KITS TO REWORK 122-389020-3 POWER PANEL INTO -7 POWER PANEL. CONTACTPRODUCT SUPPORT, BEFORE ORDERING THIS OPTIONAL KIT INSTALLED AT THECUSTOMER'S EXPENSE.

WT. CHANGE : WT: 18 LBS; MOMENT: 7254 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

122-3020-1 SANTENNA INSTALLATION, NAV VOR ATA :2000 NC-4 THRU NC-242000/2000A NC-25 AND AFTER SEE -3 S KITTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE AIRCRAFT, BYINSTALLING DORNE MARGOLIN ANTENNA SYSTEM AND REMOVING EXISTING ANTENNA SYSTEM. SEENOTE ON FMS, AS NOT FURNISHED WITH KIT.

NOTENOTENOTENOTE:::: INSTALLATION OF KIT WILL REQUIRE FMS P/N: 122-590013-37B1 OR SUBSEQUENT,ORDER SEPARATELY.

NOTENOTENOTENOTE:::: THE FOLLOWING ARE REQUIRED ITEMS BUT ARE NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. "ALODINE 1200" OR"MEK" CLEANER AND "890B4" PROSEAL ARE ITEMS NOT FURNISHED WITH KIT BUTREQUIRED FOR INSTALLATION.


122-3020-3 SANTENNA INSTALLATION, NAV, VOR LIMITATION REMOVAL ATA :2000 NC-4 THRU NC-24 SEE -1 S KIT, AS THESE

AIRCRAFT NEED KIT WITH ANTENNA2000 NC-252000A NC-26 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE AIRCRAFT, BYINSTALLATION OF RAYTHEON FABRICATED GASKET AND REMOVAL OF LIMITATIONS PLACARD ONAIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING ARE REQUIRED ITEMS BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. "ALODINE 1200" OR"MEK" CLEANER AND "890B4" PROSEAL. YOU WILL ALSO REQUIRE 1 EACH FLIGHTMANUAL SUPPLEMENT P/N: 122-590013-37B1 OR SUBSEQUENT, FOR USE OF THISSYSTEM, ORDER SEPARATELY.


122-3021-1 SEMI SUPPRESSION, AVIONICS INSTALLATION ATA :2000/2000ATHIS KIT PROVIDES PARTS AND INFORMATION NEEDED TO INSTALL SUPPRESSION CORES TO PROVIDEAVIONIC EMI SUPPRESSION FOR INSERVICE AIRCRAFT.WT. CHANGE : WT: 1.2 LBSEST. MAN/HRS: : 36 TO 42MEN : 2 (MEN)


KIT CATALOG

122-3022-1 SELECTRIC TRIM RETROFIT (YAW, ROLL AND PITCH TRIM PCB UPDATE) ATA :2000 NC-4 THRU NC-52THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE ALL SIX (6) TRIM CONTROL CARDS WITH NEWCARDS AND MAKES THE CORRESPONDING WIRING CHANGES.

NOTENOTENOTENOTE:::: THE FOLLOWING TOOLS WILL BE REQUIRED BUT NOT FURNISHED WITH THE KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: MS91067-2 INS/EXTTOOL, M22520/2-08 TURRET HEAD AND M22520/2-01 CRIMP TOOL.


122-3022-5ELECTRIC TRIM RETROFIT ATA :2000 AND 2000A NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE ALL SIX (6) TRIM CONTROL CARDS WITH NEWCARDS AND MAKES THE CORRESPONDING WIRING CHANGES. THIS KIT IS A REPLACEMENT FOR THE122-3022-1 S KIT.

NOTENOTENOTENOTE:::: FOR AIRCRAFT WITH KIT 122-3022-1 S INSTALLED REPLACE THE 122-340212-1 PCBASSEMBLIES WITH 122-340212-3 PCB ASSEMBLIES AND RETURN 2 EACH 122-340212-1PCB ASSEMBLIES TO FACTORY FOR REWORK INTO NEW -3 PCB ASSEMBLIES. CONTACTPRODUCT SUPPORT FOR ADDITIONAL INFORMATION ON PART RETURNS.


122-3023-1CABIN LIGHTS ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REWIRE THE ENTRY LIGHT CIRCUIT TO ALLOWPASSENGER EXIT AFTER ENGINE SHUTDOWN WITHOUT CLOSING BUS-TIES, FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

122-3024-1BAGGAGE LIGHT TIMER INSTALLATION-AFT BAGGAGE AREA ATA :2000 NC-4 THRU NC-20STARSHIP COMMUNIQUE NO. 9, DECEMBER, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE AIRCRAFT BYINSTALLING A LIGHT TIMER IN THE AFT BAGGAGE AREA.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS REQUIRED FOR INSTALLATION BUT NOT FURNISHED WITH KIT:CRIMP TOOL P/N'S: M27520/2-01, 47907 AND 90298-1, LOCATOR TOOL P/N: M22520/2-02,EXTRACTION TOOL P/N: 458994-1, INSERTION TOOL P/N'S: 455830-1 AND 91002-1. YOUWILL ALSO REQUIRE SEALER P/N: EA9309NA OR EA9309 QT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: FOR LATER SERIAL NUMBERS SEE 122-3024-3 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

122-3024-3BAGGAGE LIGHT TIMER INSTALLATION-AFT BAGGAGE AREA ATA :2000 AND 2000A NC-21 AND AFTERSTARSHIP COMMUNIQUE NO. 9, DECEMBER, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AIRCRAFT BY INSTALLING ALIGHT TIMER IN THE AFT BAGGAGE AREA ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS REQUIRED FOR INSTALLATION BUT NOT FURNISHED WITH KIT.CRIMP TOOL P/N'S: M27520/2-01, 47907 AND 90298-1, LOCATOR TOOL P/N: M22520/2-02,EXTRACTION TOOL P/N: 458994-1, INSERTION TOOL P/N'S: 455830-1 AND 91002-1. YOUWILL ALSO REQUIRE SEALER P/N: EA9309NA OR EA9309 QT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: FOR EARLIER SERIAL NUMBERS SEE 122-3024-1 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

122-3026-1NOSE GEAR CENTERING SQUAT SWITCH ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY INSERVICE AIRCRAFT, BY PROVIDINGPROVISIONS TO ADD LH GEAR SQUAT SWITCH TO NOSE GEAR CENTERING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 10MEN : 1 (MAN)

122-3027-1POWER PANEL ASSEMBLY - SPARES ATA :2000 AND 2000A NC-4 THRU NC-53STARSHIP COMMUNIQUE NO. 10 ON THIS "OPTIONAL" KITTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE MISFUNCTIONING 122-389020-3POWER PANELS WITH 122-389020-7 POWER PANELS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT CONTAIN 122-389020-7 PANELS, YOU ONLY NEED TO REPLACE THEDEFECTIVE -3 POWER PANEL, NOT ALL THREE PANELS ON THE AIRCRAFT. IF "O" STK ON-7 PANEL, THERE ARE EATON KITS TO REWORK -3 PANEL INTO A -7 PANEL. IF YOURAIRCRAFT DOES NOT HAVE BATTERY ASSISTED AIR START, YOU CAN BUY -3 OR"122-389020-3 OVH", OR "122-389020-3 RBL" OR "122-389020-3 REP" PANELS AS LONG ASAVAILABLE, AT "O" STOCK YOU CAN PURCHASE VENDOR REPAIR KIT FOR -3 PANEL.CONTACT PRODUCT SUPPORT FOR P/N AND ADDITIONAL INFORMATION ON THISMATTER, BEFORE ORDERING ANY PARTS WITHOUT COMMUNIQUE INSTRUCTION.


122-4001-1 SEMERGENCY EXIT MODIFICATION ATA :2000 NC-4 THRU NC-12THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REDUCE FREE PLAY IN THE EMERGENCYEXIT DOOR.

NOTENOTENOTENOTE:::: REQUIRED FOR USAGE WITH ALL 122-4002 SERIES KITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)


KIT CATALOG

122-4002-1 SSTRUCTURAL REPAIR ADHESIVE, *RESTRICTED ARTICLES* ATA :2000 NC-4 AND AFTERTHIS KIT FURNISHES ALL THE RESTRICTED ARTICLES AND ADHESIVES REQUIRED FOR USE WITHCOMPOSITE STRUCTURAL REPAIR KITS. USAGE OF THIS KIT WILL BE IN ACCORDANCE WITH STARSHIPREPAIR MANUAL P/N 122-590013-7 PROCEDURES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

122-4002-101 SSTRUCTURAL REPAIR, UPPER WING SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF UPPER WING SKIN DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-30.

NOTENOTENOTENOTE:::: 1 EACH 122-4002-1 S ADHESIVE KIT IS REQUIRED FOR USAGE WITH THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A








KIT CATALOG

122-4002-111 SSTRUCTURAL REPAIR, WING ROOT RIB ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF WING ROOT RIB DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-10.


122-4002-113 SSTRUCTURAL REPAIR, MAIN LANDING GEAR SPAR ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF MAIN LANDING GEAR SPAR DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-10.






122-4002-121 SSTRUCTURAL REPAIR, WING FORWARD SPAR ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF WING FORWARD SPAR DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-10.



KIT CATALOG

122-4002-125 SSTRUCTURAL REPAIR, WING AFT SPAR ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF WING AFT SPAR DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-10.


122-4002-129 SSTRUCTURAL REPAIR, WING AFT OUTBOARD SPAR ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF WING AFT OUTBOARD SPAR DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-10.


122-4002-137 SSTRUCTURAL REPAIR, WING AFT INBOARD SPAR ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF WING AFT INBOARD SPAR DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-10.


122-4002-139 SSTRUCTURAL REPAIR, WING FUEL TANK SKINS ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF WING FUEL TANK SKIN DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-30.


122-4002-141 SSTRUCTURAL REPAIR, FORWARD WING STRUCTURE ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF FORWARD WING STRUCTURE DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 55-10.



KIT CATALOG

122-4002-145 SSTRUCTURAL REPAIR, TIPSAIL INBOARD SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF TIPSAIL INBOARD SKIN DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 55-30.








122-4002-157 SSTRUCTURAL REPAIR, TIPSAIL OUTBOARD SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF TIPSAIL OUTBOARD SKIN DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 55-30.



KIT CATALOG





122-4002-163 SSTRUCTURAL REPAIR, ELEVON, ELEVATOR, RUDDER AND FLAP ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF CONTROL SURFACES, SUCH AS ELEVON,ELEVATOR, RUDDER AND FLAP DAMAGE TO AREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL,SECTION 55-00.


122-4002-165 SSTRUCTURAL REPAIR, NACELLE FORWARD LOWER SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NACELLE FORWARD LOWER SKIN DAMAGE TOAREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 54-30.


122-4002-167 SSTRUCTURAL REPAIR, NACELLE CENTER LOWER SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NACELLE CENTER LOWER SKIN DAMAGE TOAREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 54-30.

NOTENOTENOTENOTE:::: 1 EA. 122-4002-1 S ADHESIVE KIT IS REQUIRED FOR USAGE WITH THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

122-4002-169 SSTRUCTURAL REPAIR, NACELLE AFT SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NACELLE AFT SKIN DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 54-30.

NOTENOTENOTENOTE:::: 1 EACH. 122-4002-1 S ADHESIVE KIT IS REQUIRED FOR USAGE WITH THIS KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

122-4002-171 SSTRUCTURAL REPAIR, NACELLE ACCESS DOORS ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NACELLE ACCESS DOORS DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 54-30.


122-4002-173 SSTRUCTURAL REPAIR, ALL LANDING GEAR DOORS ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF ALL LANDING GEAR DOORS DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 52-80.


122-4002-207 SSTRUCTURAL REPAIR, TIPSAIL LEADING EDGE ATA :2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF TIPSAIL LEADING EDGE AREA DAMAGE ASSHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION: 55-30-00, PAGE 9, A1.

NOTENOTENOTENOTE:::: WILL REQUIRE 1 EACH 122-4002-1 S ADHESIVE*RA* KIT FOR USAGE WITH THIS KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-4002-209 SSTRUCTURAL REPAIR, VENTRAL STABILIZER LEADING EDGE ATA :2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF VENTRAL STABILIZER LEADING EDGE DAMAGETO AREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION: 55-60-00, PAGE 3, A1.

NOTENOTENOTENOTE:::: WILL REQUIRE 1 EACH 122-4002-1 S ADHESIVE*RA* KIT WHEN YOU INSTALL THIS KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4002-211 SSTRUCTURAL REPAIR, LOWER FORWARD, UPPER AND LOWER AFTCOWLING, EXTERIOR

ATA :

2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER FORWARD COWLING, UPPER ANDLOWER AFT COWLING EXTERIOR AREA AS SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL SECTION:54-30-00 PAGES 7, 8 AND 9, A1.

NOTENOTENOTENOTE:::: WILL REQUIRE USE OF ADHESIVE "EA934NA QT" FOR WET LAY-UP, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4002-217 SSTRUCTURAL REPAIR, LOWER FORWARD, UPPER AND LOWER AFTCOWLING INTERIOR

ATA :

2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER FORWARD COWLING, UPPER ANDLOWER AFT COWLING INTERIOR AREAS AS SHOWN IN STARSHIP STRUCTURAL REPAIR MANUALSECTION: 54-30-00 PAGES 7, 8 AND 9, A1.

NOTENOTENOTENOTE:::: WILL REQUIRE USE OF ADHESIVE "EA934NA QT" WITH THIS KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4002-219 SSTRUCTURAL REPAIR, LOWER FORWARD, UPPER AND AFT COWLINGINTERIOR

ATA :

2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER FORWARD COWLING, UPPER ANDLOWER AFT COWLING INTERIOR AREAS.

NOTENOTENOTENOTE:::: USE KIT 122-4002-217 S, REFERENCE DELTA NOTE "O" KIT DRAWING AND AS SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTIONS: 54-30-00 PAGES 7, 8 AND 9, A1.

NOTENOTENOTENOTE:::: WILL REQUIRE USE OF ADHESIVE "EA934NA QT" WITH THIS KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-4002-221 SSTRUCTURAL REPAIR, LOWER FORWARD, UPPER AND LOWER AFTCOWLING, EXTERIOR

ATA :

2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER FORWARD COWLING, UPPER ANDLOWER AFT COWLING EXTERIOR AREA DAMAGE.

NOTENOTENOTENOTE:::: USE KIT 122-4002-211 S, REFERENCE DELTA NOTE "O" KIT DRAWING AND AS SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION: 54-30-00, PAGES 7, 8 AND 9, A1.



122-4002-225 SSTRUCTURAL REPAIR, LOWER FORWARD, UPPER AND AFT COWLING,INTERIOR

ATA :

2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER FORWARD COWLING, UPPER ANDLOWER AFT COWLING INTERIOR AREA DAMAGE.

NOTENOTENOTENOTE:::: USE KIT 122-4002-217 S, REFERENCE DELTA NOTE "O" KIT DRAWING AND AS SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION: 54-30-00, PAGES 7, 8 AND 9, A1.



122-4002-227 SSTRUCTURAL REPAIR, UPPER FORWARD COWLING, EXTERIOR ATA :2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF UPPER FORWARD COWLING, EXTERIOR AREA INTHE FIELD AS SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL SECTION 54-30-00 PAGE 6, A1.

NOTENOTENOTENOTE:::: ADHESIVE "EA934NA QT" WILL BE REQUIRED FOR USAGE WITH THIS KIT, IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4002-231 SSTRUCTURAL REPAIR, UPPER FORWARD COWLING, INTERIOR ATA :2000/2000A NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF UPPER FORWARD COWLING INTERIOR AREA ASSHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION: 55-30-00 PAGE 6, A1.

NOTENOTENOTENOTE:::: WILL REQUIRE ADHESIVE "EA934NA QT" FOR WET LAY-UP, IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-4002-29 SSTRUCTURAL REPAIR, CABIN ENTRY DOOR ATA :THIS KIT PROVIDES PARTS TO REPAIR FUSELAGE SHELL DAMAGE TO AREA SHOWN IN STARSHIPSTRUCTURAL REPAIR MANUAL, SECTION 52-10.


122-4002-3 SSTRUCTURAL REPAIR, FUSELAGE SHELL ATA :THIS KIT PROVIDES PARTS TO REPAIR FUSELAGE SHELL DAMAGE TO AREA SHOWN IN STARSHIP REPAIRMANUAL, SECTION 53-30.


122-4002-37 SSTRUCTURAL REPAIR, F.S. 46 BULKHEAD ATA :THIS KIT PROVIDES PARTS FOR REPAIR OF BULKHEAD DAMAGE TO AREA SHOWN IN STARSHIPSTRUCTURAL REPAIR MANUAL, SECTION 53-10.


122-4002-41 SSTRUCTURAL REPAIR, F.S. 18 BULKHEAD ATA :THIS KIT PROVIDES PARTS FOR REPAIR OF BULKHEAD DAMAGE TO AREA SHOWN IN STARSHIPSTRUCTURAL REPAIR MANUAL, SECTION 53-10.


122-4002-43 SSTRUCTURAL REPAIR, NOSE SECTION B.L.D. 8.5 KEEL ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NOSE SECTION DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 53-10.



KIT CATALOG

122-4002-47 SSTRUCTURAL REPAIR, NOSE SECTION B.L.D. KEEL ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NOSE SECTION DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 53-10-00, FIGURE 3.


122-4002-49 SSTRUCTURAL REPAIR, NOSE SECTION B.L.D MID KEEL ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF MID KEEL DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 53-10.


122-4002-51 SSTRUCTURAL REPAIR, NOSE SECTION AVIONICS DOOR ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NOSE SECTION AVIONICS DOOR DAMAGE TOAREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 52-40.


122-4002-53 SSTRUCTURAL REPAIR, NOSE SECTION CHECK SKIN DOOR ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NOSE SECTION SKIN DOOR DAMAGE TO AREASHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 52-40.


122-4002-57 SSTRUCTURAL REPAIR, NOSE SECTION INTER-SHELF CONNECT BEAMS ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NOSE SECTION INTER-SHELF CONNECT BEAMSDAMAGE TO AREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 52-20.



KIT CATALOG

122-4002-59 SSTRUCTURAL REPAIR, NOSE SECTION FORWARD SKIN ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF NOSE SECTION FORWARD SKIN DAMAGE TOAREA SHOWN IN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 53-30.


122-4002-63 SSTRUCTURAL REPAIR, AFT FUSELAGE ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF AFT FUSELAGE DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 53-30.


122-4002-65 SSTRUCTURAL REPAIR, VENTRAL STABILIZER ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF VENTRAL STABILIZER DAMAGE TO AREA SHOWNIN STARSHIP STRUCTURAL REPAIR MANUAL, SECTION 55-60.


122-4002-67 SSTRUCTURAL REPAIR, LOWER WING SKIN ATA :THIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER WING SKIN DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-30.


122-4002-7 SSTRUCTURAL REPAIR, FUSELAGE SHELL ATA :THIS KIT PROVIDES PARTS TO REPAIR FUSELAGE SHELL DAMAGE TO AREA SHOWN IN STARSHIPSTRUCTURAL REPAIR MANUAL, SECTION 53-30.



KIT CATALOG









122-4002-79 SSTRUCTURAL REPAIR, LOWER WING SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER WING SKIN DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-30.



KIT CATALOG

122-4002-81 SSTRUCTURAL REPAIR, LOWER WING SKIN ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS NECESSARY FOR REPAIR OF LOWER WING SKIN DAMAGE TO AREA SHOWN INSTARSHIP STRUCTURAL REPAIR MANUAL, SECTION 57-30.






122-4002-9 SSTRUCTURAL REPAIR, FUSELAGE SHELL ATA :THIS KIT PROVIDES PARTS TO REPAIR FUSELAGE SHELL DAMAGE TO AREA SHOWN IN STARSHIPSTRUCTURAL REPAIR MANUAL, SECTION 53-30.





KIT CATALOG







122-4003-1 SRIB ATTACHMENT FLAP COVE ATA :2000 NC-4 THRU NC-41PER "C" REVISION TO KIT DRAWING, -1 S KIT HAS NOW BEEN REPLACED BY -3 S KIT.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE FLAP COVE CENTER RIB ATTACHMENTCLIPS AS REQUIRED BY INSPECTION.

NOTENOTENOTENOTE:::: THE FOLLOWING ADHESIVES WILL BE REQUIRED WHEN INSTALLING THIS KIT, IF NOTAVAILABLE IN YOUR STOCK UNDER PART NUMBERS "EA956 QT" OR "6373 QT", YOU CANPROCURE LOCALLY. ITEMS NOT FURNISHED AS PART OF THE KIT BECAUSE OF THEIRSHELF LIFE. RECOMMEND THEREFORE ORDER ONLY 30 DAYS BEFORE YOU SCHEDULEYOUR AIRCRAFT FOR INSTALLATION OF THIS KIT.

NOTENOTENOTENOTE:::: MEK OR ALCOHOL CLEANER SOLUTION WILL ALSO BE REQUIRED.WT. CHANGE : WT: 30 LBS; ARM: 442.5; MOMENT: 133 IN.-LBSEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)


KIT CATALOG

122-4003-3 SRIB ATTACHMENT FLAP COVE ATA :2000 NC-4 THRU NC-41THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL THE FLAP COVE CENTERRIB ATTACHMENT CLIPS AND IS A REPLACEMENT KIT FOR THOSE AIRCRAFT THAT HAVE ALREADYINSTALLED THE 122-4003-1 S KIT.

NOTENOTENOTENOTE:::: ONE OF THE FOLLOWING ADHESIVE MATERIALS WILL BE REQUIRED FOR USAGE WITHTHIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK UNDER PART NUMBERS "EA9394NAQT" OR "EA956 QT" OR "6373 QT", YOU CAN PROCURE LOCALLY. YOU WILL ALSOREQUIRE PART NUMBER "MEK" OR AN ALCOHOL CLEANING SOLUTION TO CLEAN BOTHTHE COMPOSITE AND TITANIUM. MEK CAN ALSO BE PROCURED LOCALLY.

WT. CHANGE : WT: .30 LBS; ARM: 442.5; MOMENT: 133 IN.-LBSEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

122-4005-1 SSOUND REDUCTION MODIFICATION ATA :2000 NC-21 THRU NC-28THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REDUCE CABIN SOUND LEVELS.

NOTENOTENOTENOTE:::: SEE 122-4006-1 S FOR NC-4 THRU NC-20.NOTENOTENOTENOTE:::: THE FOLLOWING MATERIAL WILL BE REQUIRED FOR INSTALLATION OF THIS KIT, BUT

ARE NOT FURNISHED AS PART OF THE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY: P/N "EC8471PT" OR "EC847 QT" ADHESIVE; P/N "MEK"METHYL ETHYL CLEANER; P/N "890B1/2 QT" PROSEAL ADHESIVE; P/N "EA9309 QT"ADHESIVE; AND P/N "SILAPREME6587" OR "M6587 QT" PLASTIC SILAPREME ADHESIVE.

WT. CHANGE : WT: -79.08 LBS; ARM: 313.63; MOMENT: 24802 IN.-LBSEST. MAN/HRS: : 120 TO 150MEN : 1 (MAN)

122-4006-1 SSOUND REDUCTION MODIFICATION ATA :2000 NC-4 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REDUCE CABIN SOUND LEVELS FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SEE 122-4005-1 S FOR NC-21 THRU NC-28.NOTENOTENOTENOTE:::: THE FOLLOWING MATERIAL WILL BE REQUIRED FOR INSTALLATION, BUT ARE NOT

FURNISHED AS PART OF THE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY: P/N "EC847 PT" OR "EC847 QT" ADHESIVE; P/N "MEK" METHYL ETHYLCLEANER; P/N "EA9309 QT" ADHESIVE; AND P/N "SILAPREME6587" OR "M6587 QT" PLASTICSILAPREME ADHESIVE.

NOTENOTENOTENOTE:::: THIS KIT FURNISHES 17 THERMAL BLANKET ASSEMBLIES AND 51 VIBRATIONABSORBERS, PLUS ADDITIONAL HARDWARE TO REDUCE SOUND LEVELS.

WT. CHANGE : WT: -79.08 LBS; ARM: 313.63; MOMENT: 24802 IN.-LBSEST. MAN/HRS: : 120 TO 150MEN : 1 (MAN)


KIT CATALOG

122-4007-1 SRIB ATTACHMENT, CENTER TRACK FLAP ATA :2000 NC-4 THRU NC-30THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE CENTER FLAP TRACK RIB ATTACHMENT.

NOTENOTENOTENOTE:::: EA934NA QT ADHESIVE WILL BE REQUIRED FOR INSTALLATION BUT IS NOT FURNISHEDWITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4008-1 PLENS LANDING LIGHT, HARD COATED (LH AND RH SIDES) - SPARES ATA :2000 NC-4 THRU NC-25THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A NEW HARD-COATINGLANDING LIGHT LENS.

NOTENOTENOTENOTE:::: OPTIONAL REPLACEMENT FOR 122-640045-3 AND -4 OR -5 AND -6 OR -11 AND -12 OR ANYCOMBINATION OF LH AND RH LANDING LIGHT LENS.


122-4009-1 SFUSELAGE DRAINAGE IMPROVEMENT BL 0.00 ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-532000A NC-26 THRU NC-53THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO IMPROVE WATER DRAINAGE IN THEFUSELAGE AT BL 0.00.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR INSTALLATION BUT ARE NOTFURNISHED WITH THE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY. "EC1300L PT" OR "EC1300L QT" CEMENT, "EA934NA QT" OR "EA9394NA QT"SEALER AND "890 PINT" PRO-SEAL 890 SEALANT.


122-4010-1 SHANDRAIL ASSEMBLY DOOR MOD, TORSION SPRING IMPROVEMENT ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE OPERATION OF THE HAND CABLEASSEMBLIES BY IMPROVING THE TORSION SPRING INSTALLATION ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 6MEN : 1 (MAN)


KIT CATALOG

122-4011-1 SEROSION BOOT, VERTICAL STABILIZER ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD EROSION BOOTS TO THE LEADINGEDGE ON THE VERTICAL STABILIZERS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

122-4015-1RADOME, LIGHTNING DIVERTER STRIP ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE RADOME AND LIGHTNING DIVERTERSTRIPS.

NOTENOTENOTENOTE:::: PART REQUIRED BUT NOT FURNISHED WITH KIT: EA934 OR EA9394NA QT. OR EA9394 QT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4015-3RADOME, LIGHTNING DIVERTER STRIP ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE LIGHTNING DIVERTER STRIPS.

NOTENOTENOTENOTE:::: PART REQUIRED BUT NOT FURNISHED WITH KIT: EA934 OR EA9394NA QT. OR EA9394 QT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4016-1DOOR REINFORCEMENT CABIN FOR MAJOR DELAMINATIONS/DISBONDS WITH TEC SUPPORT

ATA : 52

2000 NC-4 THRU NC-53"RECOMMENDED" SB NO. 52-3084THIS KIT PROVIDES PARTS AND INFORMATION TO REPAIR THE EXISTING CABIN DOOR THAT HASDELAMINATIONS AND/OR DISBONDS THAT EXCEED THE LIMITS DEFINED BY STEP ONE (1) OF THE -3 KITMODIFICATION INSTRUCTIONS. THIS REPAIR TO BE ACCOMPLISHED BY RAYTHEON AIRCRAFT CO

NOTENOTENOTENOTE:::: REFERENCE ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: EA960F QT AND EC9309 QT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-4016-3DOOR REINFORCEMENT CABIN FOR MAJOR DELAMINATIONS/DISBONDS WITH TEC SUPPORT

ATA : 52

2000 NC-4 THRU NC-53"RECOMMENDED" SB NO. 52-3084THIS KIT PROVIDES PARTS AND INFORMATION TO BEEF-UP THE EXISTING CABIN DOOR THAT HAS MINORDELAMINATIONS AND/OR DISBONDS DEFINED BY STEP ONE (1) OF THE -3 KIT MODIFICATIONINSTRUCTIONS.

NOTENOTENOTENOTE:::: REFERENCE ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: EA960F QT AND EC9309 QT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 1 LBS; MOMENT: 180 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

122-4017-1REINFORCEMENT, CABIN DOOR ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO REPAIR THE EXISTING CABIN DOOR THAT HASDELAMINATIONS AND/OR DISBONDS THAT EXCEED THE LIMITS DEFINED BY STEP ONE (1) OF THE -1 KITMODIFICATION INSTRUCTIONS. THIS REPAIR TO BE ACCOMPLISHED BY RAYTHEON AIRCRAFT CO

NOTENOTENOTENOTE:::: EA9309NA ADHESIVE AND EA960F FILLER REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: 1 LBS; MOMENT: 180 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

122-4018-1MODIFICATION, FWD MAIN GEAR CLOSURE PANEL ATA :2000 NC-34 THRU NC-53 EXCEPT NC-37THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE FWD WHEEL WELL CLOSURE PANEL TOREDUCE NOISE LEVELS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA9309NA REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.


122-4019-1RIB ATTACHMENT, CENTER FLAP TRACK ATA : 572000 NC-4 THRU NC-53"MANDATORY" SB NO. 57-3297THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE CENTER FLAP TRACK RIB ATTACHMENT ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA9309NA, EA9394NA, EA956NA ADHESIVE, EA960F, SURFACE FILLER, BS23731 SEALANTTAPE & BS23731 VACUUM BAG, REQUIRED BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

122-4019-3RIB ATTACHMENT, CENTER FLAP TRACK ATA : 572000 NC-4 THRU NC-53"MANDATORY" SB NO. 57-3297THIS KIT PROVIDES PARTS AND INFORMATION TO ADD THE 122-100058-113 AND 122-100058-114 GUSSETTO THE UPPER COVE SKIN AND WING UPPER SKIN AT CENTER RIB ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA9309NA, EA9394NA, EA956NA ADHESIVE, EA960F, SURFACE FILLER, BS23731 SEALANTTAPE & BS23731 VACUUM BAG, REQUIRED BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-4020-1 SMODIFICATION, FORWARD MAIN GEAR CLOSURE PANEL ATA :2000 NC-34 THRU NC-53, EXCEPT NC-37THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY THE FORWARD WHEEL WELL CLOSURE PANELTO REDUCE NOISE LEVELS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MICRO ULTRA 15-3 FILLER AND EA956 ADHESIVE REQUIRED BUT NOT FURNISHED WITHKIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-5003-1 SBLEED AIR VALVE AND CONTROLLER CHANGE ATA :2000 NC-4 TO EFFECTIVITY OF ECR 1709THIS KIT PROVIDES "INFORMATION ONLY" TO INSTALL UPDATED BLEED AIR VALVE AND CONTROLLERCHANGE.

NOTENOTENOTENOTE:::: SPECIAL INSTRUCTION FOR USE OF NC-8.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

122-5004-1 SUPHOLSTERED PANEL CHANGE ESCAPE HATCH ATA :2000 NC-5 AND NC-11THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL FIBERGLASS BACKED UPHOLSTERED PANELSAND ADD A HATCHED HANDLE GRIP.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)


KIT CATALOG

122-5004-3 SUPHOLSTERED PANEL CHANGE ESCAPE HATCH ATA :2000 NC-4, NC-6, NC-7, NC-8, NC-9 AND NC-10THIS KIT IS TO BE USED WHEN CONFORM PANELS 122-530363-1 AND 122-530363-3 ARE NOT AVAILABLE.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL IMPROVED ESCAPE HATCHUPHOLSTERED PANELS AND ADD A HATCH HANDLE GRIP.


122-5005-1 STRACK ROLLER MODIFICATION, CREW SEAT ATA :2000 NC-4 THRU NC-13THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW TRACK ROLLERS INTO THE CREWCHAIRS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

122-5006-1 SPEDESTAL SHROUD, CABIN CHAIR ATA :2000 NC-4 THRU NC-12THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A METHOD OF ATTACHMENT FOR THE CHAIRPEDESTAL SHROUDS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

122-5007-1 SAIR OUTLET UPDATE, CABIN OVERHEAD ATA :2000 NC-14 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ENLARGED CABIN AIR OUTLETS AND SUPPLYDUCTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

122-5007-3 SAIR OUTLET UPDATE, CABIN OVERHEAD ATA :2000 NC-4 THRU NC-13THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ENLARGED CABIN AIR OUTLETS AND SUPPLYDUCTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)


KIT CATALOG

122-5008-1 SFLAP BUSHING REPLACEMENT ATA :2000 NC-4 THRU NC-25THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LONGER BUSHINGS IN FLAP FITTINGS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

122-5009-1 SCABIN WINDOW DEFOG SYSTEM UPDATE WITH WINDOWS ATA :2000 NC-4 THRU NC-15THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW CABIN ANTI-FOG COATED WINDOWS ANDTO CHECK PROPER INSTALLATION OF SIDEWALL PLENUM AIR DUCTS AND DEFOG AIR DUCTS TO THECABIN WINDOW.

NOTENOTENOTENOTE:::: KIT COMES WITH WINDOWS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 32MEN : 1 (MAN)

122-5009-3 SCABIN WINDOW DEFOG SYSTEM UPDATE (LESS WINDOW) ATA :2000 NC-15 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW CABIN ANTI-FOG COATED WINDOWS ANDCHECK PROPER INSTALLATION OF SIDEWALL PLENUM AIR DUCTS AND DEFOG AIR DUCTS TO THE CABINWINDOW.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 20 TO 24MEN : 1 (MAN)

122-5011-1 SCLOSURE INSTALLATION ENVIRONMENTAL DOME ATA :2000 NC-4 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENVIRONMENTAL DOME CLOSUREASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

122-5012-1 SCABIN DOOR FRAME INSTALLATION ATA :2000 NC-4 THRU NC-33THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL BUFFED METAL TRIM AROUND THE CABINDOOR FRAME TO IMPROVE APPEARANCE.WT. CHANGE : N/AEST. MAN/HRS: : 4 TO 8MEN : 1 (MAN)


KIT CATALOG

122-5013-1 S5 OHM ADJUSTABLE RESISTER AND 12V CLUTCH COIL, COMPRESSORMOD

ATA :

2000 NC-4 THRU NC-16THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE OW-5A-2G 24 VDC CLUTCH ASSEMBLYON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

122-5015-1 SEVAPORATOR COIL INSTALLATION ATA :2000 NC-4 TO ECR 3054THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FORWARD AND AFT EVAPORATOR ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NEED TO ORDER EVAP-COILS SEPARATELY, NOT PART OF KIT, CAN USE NEW OR OVH;SEE 122-380021-3 OR -3 OVH AND 122-380026-3 OR -3 OVH, ORDER WHICHEVER IS INSTOCK.


122-5016-1 SCABIN PAGING AND STEREO SPEAKER INSTALLATION ATA :2000 NC-4 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE D6200 SPEAKERS ON INSERVICEAIRCRAFT. ONE KIT PER SPEAKER REPLACED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

122-5017-1 SCABIN WINDOW, DUAL PANE, ANTI-FOG ATA :2000 NC-6 THRU NC-11, NC-16, NC-17THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW CABIN DUAL PANE WINDOWS ANDCHECK PROPER INSTALLATION OF SIDEWALL PLENUM AIR DUCTS AND DEFOG AIR DUCTS TO THE CABINWINDOW ON INSERVICE AIRCRAFT WITH 122-5009 KIT INSTALLED.WT. CHANGE : WT: 9 LBS F. S. 276.2EST. MAN/HRS: : 16 TO 24MEN : 1 (MAN)

122-5017-3 SCABIN WINDOW, DUAL PANE, ANTI-FOG ATA :2000 NC-4, NC-5, NC-12 THRU NC-15, NC-18

THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW CABIN DUAL PANE WINDOWS ANDCHECK PROPER INSTALLATION OF SIDEWALL PLENUM AIR DUCTS AND DEFOG AIR DUCTS TO THE CABINWINDOW ON INSERVICE AIRCRAFT WITHOUT 122-5009 KIT INSTALLED.WT. CHANGE : WT: 9 LBS F. S. 276.2EST. MAN/HRS: : 16 TO 24MEN : 1 (MAN)


KIT CATALOG

122-5017-5 SCABIN WINDOW, DUAL PANE, ANTI-FOG ATA :2000 NC-21 TO ECR 4897THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW CABIN DUAL PANE WINDOWS ANDCHECK PROPER INSTALLATION OF SIDEWALL PLENUM AIR DUCTS AND DEFOG AIR DUCTS TO THE CABINWINDOW ON INSERVICE AIRCRAFTWT. CHANGE : WT: 9 LBS F. S. 276.2EST. MAN/HRS: : 16 TO 24MEN : 1 (MAN)

122-5018-1 SCOMPRESSOR ASSEMBLY, AIR CONDITIONER CHANGE ATA :2000 NC-4 THRU NC-34THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SD-508 AIR CONDITIONER COMPRESSOR ONINSERVICE AIRCRAFT. THIS OPTIONAL CHANGE IS TO IMPROVE OVERALL AIR CONDITIONERPERFORMANCE.WT. CHANGE : WT: 9 LBS F. S. 276.2EST. MAN/HRS: : 16 TO 24MEN : 1 (MAN)

122-5019-1 SWINDOW INSTALLATION, MANUAL POLARIZED WINDOW MOD ATA :2000 NC-4 THRU NC-20THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A MANUALLY OPERATEDPOLARIZED WINDOW INSTALLATION IN PLACE OF THE ELECTRIC SYSTEM ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)

122-5022-1 SCABIN TEMPERATURE TRANSDUCER RELOCATION, FORWARD CABIN ATA :2000 NC-4 THRU NC-53STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE FORWARD TEMPERATURETRANSDUCER TO THE FORWARD EVAPORATOR INLET TO IMPROVE SYSTEM PERFORMANCE ON MODELAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)


KIT CATALOG

122-5024-1 STHIRD ICE DETECTOR INSTALLATION ATA :2000 NC-4 THRU NC-9 AND NC-11 THRU NC-43"MANDATORY" SB NO. 2495, REF: STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993)THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A THIRD ICE DETECTOR FOR ON THE GROUNDSURFACE ICE DETECTION ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS TO ALERT THE CREW OF ICING CONDITION WHILE THE AIRCRAFT IS ON THEGROUND.

NOTENOTENOTENOTE:::: EA956 QT REQUIRED FOR USAGE BUT NOT PART OF THE KIT, IF YOU DO NOT HAVE INYOUR SHOP, PROCURE LOCALLY.

WT. CHANGE : WT: 3.4 LBS @ 154 MOMENTEST. MAN/HRS: : 60 TO 80MEN : 1 (MAN)

122-5025-1 SPASSENGER OXYGEN SYSTEM, MASK DROPOUT FUNCTION UPDATE ATA :2000 NC-4 THRU NC-20, FOR NC-21 THRU NC-40

SEE -3 S KIT.STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW, ROOMIER MASK STORAGECONTAINER WITH A STREAMLINED DOOR FOR SMOOTH OXYGEN MASK DEPLOYMENT OPERATION ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: EA 934NA QT ADHESIVE WILL BE REQUIRED FOR INSTALLATION BUT IS NOT FURNISHEDAS PART OF THE KIT. IF NOT AVAILABLE FROM YOUR SHOP, PLEASE PROCURE LOCALLY.


122-5025-3 SPASSENGER OXYGEN SYSTEM, MASK DROPOUT FUNCTION UPDATE ATA :2000, 2000A NC-21 THRU NC-40, FOR NC-4 THRU NC-20

SEE -1 S KITSTARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW, ROOMIER MASK STORAGECONTAINER WITH A STREAMLINED DOOR FOR SMOOTH OXYGEN MASK DEPLOYMENT OPERATION ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PN EA934NA QT ADHESIVE WILL BE REQUIRED FOR INSTALLATION BUT IS NOTFURNISHED AS PART OF THE KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.


122-5026-1 SFAIRLEAD RUDDER CABLE INSTALLATION, F.S. 196.63 ATA :2000/2000A NC-4 THRU NC-47THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A FAIRLEAD TO MAINTAINCLEARANCE BETWEEN RUDDER CABLE AND PLUMBING SUPPORT BRACKETS AT F.S. 196.63.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 5MEN : 1 (MAN)


KIT CATALOG

122-5027-1 PICE CHEST (REMOVABLE) INSTALLATION ATA :2000 NC-4 THRU NC-252000A NC-26, NC-53THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO REPLACE THE ICE CHEST WITHOVERBOARD DRAIN WITH A SELF CONTAINED ICE CHEST WHICH IS REMOVABLE FOR SERVICING.

NOTENOTENOTENOTE:::: KIT REPLACES HBIC0003-1 ICE CHEST WITH A REMOVABLE ICE CHEST AND REQUIREDINSTALLATION COMPONENTS REQUIRED.

WT. CHANGE : WT: 4 LBS; MOMENT: 400 IN ADDITIONEST. MAN/HRS: : 4MEN : 2 (MEN)

122-5028-1AIRSTAIR DOOR FRAME, OVERHEAD BUMPER PAD INSTALLATION ATA :2000 NC-4 THRU NC-53STARSHIP COMMUNIQUE NO. 8THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A BUMPER PAD ON THEOVERHEAD DOOR JAM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: WILL REQUIRE "EA9309NA" OR "EA9309 QT" ADHESIVE SEALER TO INSTALL THIS KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


122-5029-1SOUND DAMPENER BAGGAGE AREA ATA :2000 NC-4 THRU NC-202000, 2000A NC-21 THRU NC-26, SEE -5 KIT.2000A NC-27 AND AFTER SEE 122-5029-3 KIT.STARSHIP COMMUNIQUE NO. 9, DECEMBER, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE AIRCRAFT, BYINSTALLING SOUND DAMPENER IN THE BAGGAGE AREA .WT. CHANGE : WT: + 23.00 LBS,;ARM; MOMENT: + 8890 IN.-LBSEST. MAN/HRS: : 12MEN : 1 (MAN)

122-5029-3SOUND DAMPENER BAGGAGE AREA ATA :2000 NC-4 THRU NC-20 (SEE 122-5029-1)2000, 2000A NC-21 THRU NC-26 (SEE -5 KIT)2000A NC-27 THRU NC-53STARSHIP COMMUNIQUE NO. 9, DECEMBER, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE AIRCRAFT, BYINSTALLING SOUND DAMPENER IN THE BAGGAGE AREA .

NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED: 1 PT OF "EC1300L" ADHESIVE, AND "MEK" ORISOPROPYL ALCOHOL SOLVENT FOR CLEANING WITH CHEESE CLOTH. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 23.00 LBS; ARM; MOMENT: + 8890 IN.-LBSEST. MAN/HRS: : 12MEN : 1 (MAN)


KIT CATALOG

122-5029-5SOUND DAMPENER BAGGAGE AREA ATA :2000 NC-21 THRU NC-252000A NC-26STARSHIP COMMUNIQUE NO. 9, DECEMBER, 1995THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE AIRCRAFT, BYINSTALLING SOUND DAMPENER IN THE BAGGAGE AREA .

NOTENOTENOTENOTE:::: FOR EARLIER MODELS SEE 122-5022-1 KIT AND FOR LATER MODELS SEE 122-5022-3 KIT.NOTENOTENOTENOTE:::: NOT FURNISHED WITH KIT BUT REQUIRED: 1 PT OF "EC1300L" ADHESIVE, AND "MEK" OR

ISOPROPYL ALCOHOL SOLVENT FOR CLEANING WITH CHEESE CLOTH. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: +23.00 LBS; ARM; MOMENT: +8890 IN.-LBSEST. MAN/HRS: : 12MEN : 1 (MAN)

122-5030-1REFRIGERANT CHANGE AIR CONDITIONING ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CHANGE THE VAPOR CYCLE AIRCONDITIONING FROM REFRIGERANT R-12 TO REFRIGERANT R-134A FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT: "FLUSH OIL 5 GL" ANEROL FLUSH OIL AND"R134A" REFRIGERANT. APPROXIMATELY 5 GALLONS OF FLUSH OIL IS REQUIRED AND 8.5LBS. OF R134A REFRIGERANT TO CHARGE THE SYSTEM PROPERLY. A SUITABLE FLUSHCART IS CLASSIC TOOL, MANUFACTURED BY CLASSIC TOOL DESIGN, INC. NEWWINDSOR, NY. IF A REPLACEMENT COMPRESSOR IS REQUIRED USE A 9283COMPRESSOR.


122-5031-1WINDOW DESSICANT SYSTEM ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DESSICANT SYSTEM FOR THEEMERGENCY EXIT WINDOW.

NOTENOTENOTENOTE:::: 122-430030-42 WINDOW ASSEMBLY MUST BE INSTALLED PRIOR TO KIT MODIFICATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

122-5031-3WINDOW DESSICANT SYSTEM ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DESSICANT SYSTEM FOR THECABIN WINDOWS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 122-430030-39 AND -44 WINDOW ASSEMBLES MUST BE INSTALLED PRIOR TO KITMODIFICATION.



KIT CATALOG

122-5031-5WINDOW DESSICANT SYSTEM ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A DESSICANT SYSTEM FOR THELH CABIN WINDOWS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 122-430030-39. -41 AND -43 WINDOW ASSEMBLIES MUST BE INSTALLED PRIOR TO KITMODIFICATION.


122-5034-1DRAIN IMPROVEMENT, AFT EVAPORATOR CONDENSATION ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE AFT EVAPORATORCONDENSATION DRAIN SYSTEM TO REDUCE MOISTURE BUILD UP IN THE CABIN ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

122-5036-1OVERPRESSURE PROTECTION, HYDRAULIC POWER PACK ATA :2000 NC-4 THRU NC-53THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RESTRICTOR ON THE HYDRAULIC POWERPACK.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

122-8001-1 SWHEEL BEARING, MAIN LANDING GEAR ANTISKID IMPROVEMENT ATA :2000 NC-4 THRU NC-252000A NC-26 THRU NC-53THIS KIT PROVIDES INFORMATION AND PARTS TO BE INSTALLED FOR INSERVICE AIRCRAFT TO IMPROVEANTISKID TRANSDUCED SERVICING AND WHEEL BEARING PROTECTION ON.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS NOT FURNISHED WITH KIT ARE REQUIRED FOR INSTALLATION, IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "890B1/2QT"PROSEAL, "AMSOIL HEAVY DUTY "GREASE, "SN60WRMAP3.031" SOLDER FED-QQ-S-571,"M22520/1-01" CRIMP TOOL, "MS2520/1-02" POSITIONER AND AN INSERT EXTRACTIONTOOL "M81969/14-2. YOU WILL ALSO HAVE TO OBTAIN LOCALLY SOME ISOPROPYLALCOHOL (03170056). THESE ARE AS REQUIRED OR 1 EACH QUANTITY ITEMS.



KIT CATALOG

122-8002-1CHARGE VALVE RELOCATION POWER BRAKE ACCUMULATOR ATA :C2000 NC-4 THRU NC-34, NC-36 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO BE INSTALLED FOR INSERVICE AIRCRAFTTO IMPROVE SERVICING OF POWER BRAKE ACCUMULATOR.

NOTENOTENOTENOTE:::: THE FOLLOWING ADHESIVE WILL NOT BE FURNISHED WITH THIS KIT BUT ARE REQUIRED,IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "6371AB"ADHESIVE, "EA934NA QT" OR "EA939NA QT" ADHESIVE AND "87005A/BE60" EPOCASTCORE FILL.

WT. CHANGE : WT: 1 LB.; ARM: 55 IN.; MOMENT: 55 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : 1 (MAN)

122-9001-1 SDRAIN MAST, LONGER ATA :2000 NC-4 THRU NC-14THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LONGER DRAIN MASTS.

NOTENOTENOTENOTE:::: IF MANUALS AND SUPPLEMENTS CALLED OUT ON PRINT ARE NOT SET-UP IN SOARSYSTEM CONTACT TECHNICAL PUBLICATIONS, 316-676-4505 OR TECHNICAL SERVICES,TO SEE IF THEY WILL SET-UP IN SOAR OR SHIP TO YOU ON A SALES TICKET FROMRAYTHEON PUBLICATIONS.

NOTENOTENOTENOTE:::: SEE 122-9002-3 S KIT FOR NC-21 THRU NC-28.NOTENOTENOTENOTE:::: YOU WILL NEED TO ORDER 2 EACH SLZ7886 OVH STALL WARNING COMPUTERS FROM

RAYTHEON AIRCRAFT AT SAME TIME AS YOU ORDER KIT AND RETURN OLD SLZ7702-B-04COMPUTERS FOR CORE DEPOSIT IMMEDIATELY AFTER INSTALLATION OF THIS KIT. YOUWILL BE FURNISHED REPLACEMENT STACKS WITH THE KIT. PLEASE SCRAP OLDSTACKS.


122-9002-1 SGROSS WEIGHT INCREASE MOD 2000 TO 2000A LIMITS ATA :2000 NC-4 THRU NC-20 ONLY, INCREASE TO

14,900 LBS.STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPDATE INSERVICE AIRCRAFT TO MODEL2000A CONFIGURATION TO INCREASE GROSS TAKEOFF WEIGHT LIMITS ONLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 100 TO 120MEN : 2 (MEN)


KIT CATALOG

122-9002-3 SGROSS WEIGHT INCREASE MOD 2000 TO 2000A LIMITS ATA :2000 NC-21 THRU NC-28STARSHIP COMMUNIQUE NO. 4, AUGUST, 1993THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPDATE INSERVICE AIRCRAFT TO MODEL2000A CONFIGURATION INCREASED WEIGHT TAKE-OFF LIMITS OF 14,900 POUNDS.

NOTENOTENOTENOTE:::: IF MANUALS AND SUPPLEMENTS CALLED OUT ON PRINT ARE NOT SET-UP IN SOARSYSTEM, CONTACT TECHNICAL PUBLICATIONS, TECHNICAL SERVICES, TO SEE IF THEYWILL SET-UP IN SOAR OR SHIP TO YOU ON A SALES TICKET FROM RAYTHEONPUBLICATIONS

NOTENOTENOTENOTE:::: SEE 122-9002-1 S KIT FOR NC-4 THRU NC-20.NOTENOTENOTENOTE:::: SLZ7702-B-4 STALL WARNING COMPUTERS ON AIRCRAFT WILL HAVE TO BE REMOVED

FROM AIRCRAFT AND SENT BACK TO RAYTHEON AIRCRAFT CORPORATION FORUPDATING TO SLZ7886 OVH CONFIGURATION. THEREFORE RECOMMEND ORDER 2 EACHSLZ7886 OVH WHEN YOU PLACE KIT ON ORDER. THE AIRCRAFT EXHAUST STACKS WILLALSO BE CHANGED BUT REPLACEMENT STACKS WILL BE FURNISHED WITH THIS KIT.


122-9004-1 SPLACARD INSTALLATION - GLARESHIELD AFT EDGE PILOT SIDE ATA :2000 NC-24, NC-252000A NC-26 THRU NC-42THIS KIT PROVIDES A PLACARD TO INSTALL IN FRONT OF THE PILOT ON THE AFT EDGE OF THEGLARESHIELD BETWEEN THE MASTER CAUTION ANNUNCIATOR AND THE FIRE EXTINGUISHER CONTROLSWITCH ON INSERVICE AIRCRAFT AND A P/N: 122-590013-37 TC1 TEMPORARY REVISION PAGE TO B

NOTENOTENOTENOTE:::: COMPLIANCE WITH P AND WC SERVICE BULLETIN NO. 14144 WILL REMOVE THEREQUIREMENT FOR THE P/N: 129-320009-1 PLACARD AND THE TEMPORARY REVISIONPAGE P/N: 122-590013-1 PLACARD AND THE TEMPORARY REVISION PAGE P/N:122-590013-37TC1.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .3 TO .5MEN : 1 (MAN)

122-9005-1BRACKET ASSEMBLY REWORK, THROTTLE CONTROL CABLE ATA :2000 NC-3 AND AFTER400A RK-3 THRU RK-4THIS KIT PROVIDES "INFORMATION ONLY" ON HOW TO REWORK THE THROTTLE CONTROL CABLEBRACKET ASSEMBLY ON INSERVICE AIRCRAFT TO IMPROVE THE SYSTEM.

NOTENOTENOTENOTE:::: YOU WILL BE REFERRED TO STARSHIP MAINTENANCE MANUAL CHAPTER 71-00-00 ONREMOVAL AND INSTALLATION INSTRUCTIONS FOR THE SYSTEM AND WILL ALSO TO RE-CAD PLATE PROCEDURES PER QQ-P-416 TYPE III CLASS 2. YOU MAY WANT TO REVIEWBOTH BEFORE ORDERING THIS "INFORMATION ONLY" KIT.




Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberEXTERIOR MARKING "BEECHCRAFT" NEW STYLE LOGO - (101-2003-1 S) 1

PITCH TRIM CONTROLLER - (101-3045-1) 1



FLAP AERO SEAL, INSTL - (128-1001-0001) 2

SECTIONED LEADING EDGE, MAIN FLAP INSTALLATION - (128-1600-1) 2

GENERATOR CONTROL UNIT - (128-3001-1 P) 2

GENERATOR CONTROL UNIT - (128-3001-3 P) 3

VLF SYSTEM OPERATION ACTIVATION - (128-3002-1 S) 3

GENERATOR INSTALLATION - (128-3004-1 P) 3

GENERATOR INSTALLATION - (128-3004-3 P) 3

FLIGHT DISPLAY UPDATE - (128-3007-1 S) 4

FLIGHT DISPLAY UPDATE - (128-3007-3 S) 4

CATEGORY II APPROACH SYSTEM INSTALLATION - (128-3008-1 S) 4

CATEGORY II APPROACH SYSTEM INSTALLATION - (128-3008-3 S) 4

STALL RECOGNITION SUPPLEMENTARY SYSTEM - (128-3009-1 S) 4

TRANSPONDER DUAL INSTALLATION TDR-94 - (128-3011-1 S) 5

VLF OMEGA RECEIVER UPDATE - (128-3012-1 S) 5

FLIGHT CONTROL SYSTEM UPDATE INFORMATION - (128-3013-1 S) 5

ICC CARD CHANGE - (128-3015-1 S) 5

NAV TAIL LIGHT INSTALLATION - (128-3016-1 S) 6

WIRE HARNESS CLAMPING, MAIN LANDING GEAR WHEEL WELL - (128-3017-1 S) 6

AIR DATA SYSTEM MACH SPEED CORRECTION - (128-3019-1 S) 6

ROTOR BURST HAZARD MINIMIZATION UPDATE INSTALLATION - (128-3021-1 S) 6

ROTOR BURST HAZARD MINIMIZATION UPDATE INSTALLATION - (128-3021-3 S) 7

STANDBY LIGHTING IMPROVEMENT INSTALLATION - (128-3022-1 S) 7

AUTOPILOT AND RUDDER BOOST INTERLOCK UPDATE - (128-3023-1 S) 7

AUTOPILOT AND RUDDER BOOST INTERLOCK UPDATE - (128-3023-5 S) 8

STANDBY LIGHTING IMPROVEMENT - (128-3025-1 S) 8

STANDBY LIGHTING IMPROVEMENT - (128-3026-1 S) 8

FLIGHT HOUR METER IMPROVEMENT - (128-3027-1 S) 9

FLIGHT HOUR METER IMPROVEMENT - (128-3028-1 S) 9

AUTOPILOT UPDATE - (128-3030-1 S) 9

ELT-EMERGENCY LOCATOR TRANSMITTER INSTALLATION - (128-3031-1 S) 9

ELT-EMERGENCY LOCATOR TRANSMITTER INSTALLATION - (128-3031-3) 10

STANDBY BATTERY TEST CIRCUIT IMPROVEMENT - (128-3035-1) 10

STANDBY BATTERY TEST CIRCUIT IMPROVEMENT - (128-3036-1) 10



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFLIGHT DIRECTOR CROSSPOINTER DISPLAY - (128-3037-1) 11

IGNITOR WIRING CHANGE, BURST MODE IGNITION - (128-3038-1) 11



WING ANTI-ICE TEMPERATURE LOW, ANNUNCIATOR LIGHT - (128-3042-1) 12



WING ANTI-ICE TEMPERATURE LOW,ANNUNCIATOR LIGHT - (128-3043-1) 13

CIRCUIT BREAKER REPLACEMENT INSTALLATION - SPARES - (128-3044-1) 13

CIRCUIT BREAKER REPLACEMENT INSTALLATION - (128-3044-3) 14



EMI SUPPRESSION AVIONICS - (128-3049-3) 15

EMI SUPPRESSION AVIONICS - (128-3049-5) 15


WING ANTIICE SYSTEM, DUAL CONTROL - (128-3052-1) 16

HORIZONTAL STAB DE-ICE, GAP CONTACTOR - (128-3053-1) 16

HORIZONTAL STAB DE-ICE, GAP CONTACTOR - (128-3053-3) 16

DC CONVERTER - (128-3054-1)

17

DC CONVERTER - (128-3054-5) 17

ENGINE IGNITOR CIRCUIT IMPROVEMENT - (128-3055-1) 17




THIS KIT PROVIDES PARTS & INFORMATION FOR COCKPIT SPEAKER SWITCHED DISCONNECT FOR IN-SERVICE AIRCRAFT. - (128-3058-1)

19

COCKPIT VOICE RECORDER - (128-3059-1) 19

PLACARD ASSY, ENGINE FIRE EXTINGUISH - (128-3062-1) 20

LIGHT ASSY, LED TAIL POSITION-INFO ONLY - (128-3063-1) 20

TAIL DEICE SYSTEM SOLID STATE CONTACTOR - (128-3065-0001) 20

REMOTE OIL LEVEL SYSTEM, ENGINE - (128-3066-0001) 21

GALLEY ELECTRICAL WIRING - (128-3068-0001) 21

BATTERY FEEDER PROTECTION UNIT,INSTALLATION CHANGE - (128-3069-0001) 21

ELECTRICAL WIRING MODIFICATION, FLAP HYDRAULICSYSTEM-INFO ONLY - (128-3071-0001)

22

COLLINS TDR-94/94D MODE S ENHANCED SURVEILLANCE UPGRADE - (128-3413-0001) 22

HONEYWELL EGPWS SOFTWARE ENHANCEMENTS WITH OPTIONAL RAAS UPGRADE - (128-3415-0001) 23

HONEYWELL EGPWS SOFTWARE ENHANCEMENTS WITH OPTIONAL RAAS UPGRADE - (128-3415-0003) 23



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberHONEYWELL EGPWS SOFTWARE ENHANCEMENTS WITH OPTIONAL RAAS UPGRADE - (128-3415-0005)

24

INSULATION NOMEX BLANKETS - (128-4001-1 S) 24

FUEL DECAL, EXTERIOR INFORMATION MARKING - (128-4002-1 S) 24

FUSELAGE STIFFENER INSTALLATION - (128-4004-1 S) 25

PRECIPITATION STATIC - (128-4005-1 S) 25

PRECIPITATION STATIC - (128-4005-3 S) 25

INSULATION MODIFICATION - (128-4006-7 S) 25

STRUCTURAL REINFORCEMENT - (128-4010-1 S) 26





LEADING EDGE HORIZONTAL STABILIZER DEICE - (128-4014-1) 27





CONDENSER AIR INLET INSTALLATION - (128-4024-1) 28

ELT INSTALLATION - (128-4028-1) 28

ELT INSTALLATION - (128-4028-3) 29

CLOSEOUT ASSEMBLY CABIN/COCKPIT - (128-4031-1) 29

AFT WING SPAR FITTING, FATIGUE IMPROVEMENT - (128-4031-3) 29

ENGINE CARRY THRU BRACKET INSTALLATION - (128-4035-1) 29



BRACKET ATTACHMENT MODIFICATION, INSTL - (128-4038-0001) 30

BEARING ASSY-ENTRANCE DOOR HANDLE MOD INSTL - (128-4039-0001) 30

SUPPLEMENTAL INSULATION INSTALLATION - (128-4600-1) 30

LIGHT PANEL TREATMENT, INDIRECT LIGHTING - (128-5001-1 S) 31

LIGHT PANEL TREATMENT, INDIRECT LIGHTING - (128-5001-3 S) 31

AIR DUCT MODIFICATION - (128-5002-1 S) 31

AIR DUCT MODIFICATION - (128-5002-3 S) 32

THRUST REVERSE BEARING - (128-5003-1 S) 32

BLEED AIR ORIFICE - (128-5004-1 S) 32

AIR FLOW OUTLET DEFLECTOR - (128-5005-1 S) 32

GERMAN CERTIFICATION MODIFICATION - (128-5006-1 S) 33

SPEAKER, COCKPIT AND CABIN INSTALLATION - (128-5007-1 S) 33



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberSPEAKER, CABIN INSTALLATION - (128-5008-1 S) 33

STALL RECOGNITION MODIFICATION - (128-5009-1 S) 33

OXYGEN PLUMBING MODIFICATION - (128-5011-3 S) 33

ENVIRONMENTAL AIR VALVE REPLACEMENT - (128-5014-1 S) 34

ENVIRONMENTAL AIR VALVE REPLACEMENT - (128-5014-3 S) 34

DISTRIBUTION AIR MODIFICATION, LOWER CABIN DUCT SLOT REWORK - (128-5015-1 S) 34

CREW SEAT TRACKING MECHANISM - (128-5017-1 S) 34

CREW SEAT TRACKING MECHANISM IMROVEMENT INSTLN-KIT - (128-5017-3) 35

TAKEOFF PERFORMANCE IMPROVEMENT MODIFICATION - (128-5025-1 M) 35

TAKEOFF PERFORMANCE IMPROVEMENT MODIFICATION - (128-5025-3 M) 35

REFRIGERATION UNIT CONTROL SYSTEM INSTALLATION - UPGRADE - (128-5026-1) 36

REFRIGERATION UNIT CONTROL SYSTEM INSTALLATION - 1 ZONE TEMP CONTROL - (128-5026-3) 36

REFRIGERATION MOISTURE DRAIN REMOVAL AND ECU MOD - (128-5026-5) 37

REFRIGERATION ELECTRICAL SYSTEM COMPONENT MOD - (128-5026-7) 37

REFRIGERATION ELECTRICAL SYSTEM COMPONENT MOD - (128-5026-9) 37

GUST LOCK INSTALLATION - CONTROL COLUMN OPTION - (128-5027-1) 37

TEMPERATURE CONTROL VALVE INSTALLATION - ENVIRONMENTAL SYSTEM - SPARES - (128-5028-1) 38

TEMPERATURE CONTROL VALVE - CABIN, REPLACEMENT - (128-5028-3) 38

LOW LIMIT TEMPERATURE CONTROL VALVE INSTALLATION, ENVIRONMENTAL - SPARES - (128-5029-1) 38

NITROGEN GAUGE, FORWARD FUSELAGE INSTALLATION - (128-5033-1) 38

OXYGEN GAUGE, FORWARD FUSELAGE - (128-5034-1) 39

AIR CONDITIONING EVAPORATOR CONDENSATION DRAIN INSTALLATION - (128-5037-1) 39

RELOCATION OF GALLEY DRAIN - (128-5039-1) 39

INTERIOR IMPROVEMENTS - (128-5040-1) 39




VENT COOLER-400A - (128-5043-1) 40

CABIN TEMP SENSOR RELOCATION - (128-5044-1) 41

WINDOW DRY AIR SYSTEM REMOVAL - (128-5044-3) 41

AFT EVAPORATOR DRAIN IMPROVEMENT - (128-5045-1) 41

AIRCRAFT OWNERSHIP PLATES - INFORMATION ONLY - (128-5046-1) 41

AIRCRAFT OWNERSHIP PLATES - INFORMATION ONLY - (128-5046-3) 42

CREW SEAT TRACKING MECHANISM - (128-5047-1) 42

CREW SEAT TRACKING MECHANISM - (128-5047-3) 42

ANTI-ICE INSULATION CHANGE-INFO ONLY - (128-5051-1) 42

ANTI-ICE INSULATION CHANGE-INFO ONLY - (128-5051-2) 43



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberANTI-ICE INSULATION CHANGE - INFO ONLY - (128-5051-5) 43

INCREASED GROSS TAKEOFF WEIGHT/200 POUNDS - (128-5052-1) 43

EVAPORATOR DRAIN - (128-5059-0001) 43

EVAPORATOR DRAIN - (128-5059-0003)

44

PLUG ARM REST HEAT-INFO ONLY - (128-5060-1)

44

128-5303-0001 - (128-5303-0001) 44

CLEAN FLUSH TOILET INSTALLATION - (128-5305-0001) 44

CLOSET/GALLEY FINISH PROTECTION - (128-5306-0001) 45

CLOSET/GALLEY FINISH PROTECTION - (128-5306-0003) 45

CRASH AXE INSTALLATION (JAP-OPS) - (128-5311-1) 45

INSTL IMPROVEMENT, HEADLINER-INFO ONLY - (128-5313-1) 45

INTERIOR MARKING INSTL, PORTUGUESE CERT - (128-5314-0001) 45

PORTUGUESE PLACARD INSTL-EMERGENCY EXIT HANDLE, EXIT SIGN - (128-5316-0001) 46

PORTUGUESE PLACARD INSTL-EMERGENCY EXIT HANDLE, EXIT SIGN - (128-5316-0007)

46

PRESSURIZATION AIR DEFLECTOR MODIFICATION - (128-5400-1 S) 46

PRESSURIZATION CONTROL - SPARES - (128-5402-1 S) 46



VENT COOLER - (128-5403-1) 47

WINDSHIELD WIPER REMOVAL-INFO ONLY - (128-5405-1) 47

WINDSHIELD WIPER REMOVAL-INFO ONLY - (128-5405-3) 48

NITROGEN GUAGE INSTALLATION - (128-5406-1) 48

PNEUMATIC RELAY BRACKET - (128-5407-0001) 48

PNEUMATIC RELAY BRACKET - (128-5407-0003) 48

OXYGEN SERVICE DOOR, INSTL - (128-5600-1) 48

JEPPESEN HOLDER ASSY W/PROTECTIVE BREATHING EQUIP - (128-6000-0001)

49

SCREW REPLACEMENT TABLE INSTL, CABIN - (128-6001-0001) 49

FLASHLIGHT INSTL, COCKPIT, COPILOT - (128-6002-0001)

49

LANDING WEIGHT INCREASE MODIFICATION - (128-8001-1 S) 49

EMERGENCY GEAR DOOR HANDLE REPOSITION - (128-8002-1 S) 50

DUAL RATE SPEED BRAKE MANIFOLD, HYDRAULIC SYSTEM INSTALLATION - (128-8003-1 S) 50

LANDING GEAR PLACARD MOD-INFO ONLY - (128-8010-0001)

50

ENGINE OIL BREATHER DRAIN MODIFICATION - (128-9001-1 S) 50

FLAPPER VALVE FLOAT VALVE INSTALLATION - (128-9004-1) 51



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberFLAPPER VALVE FLOAT VALVE INSTALLATION - (128-9004-3) 51

FLAPPER VALVE FLOAT VALVE REPLACEMENT INSTALLATION - (128-9004-3 S) 51

ACCESS DOOR INSTL, REMOTE OIL CHECK - (128-9007-0001) 51

RAC MOD TO INSTL OIL TO FUEL ENG HEAT EXCHANGER - (128-9008-0001) 52

PROVISIONS FOR ELIMINATION OF ANTI-ICE INHIBITOR FUEL ADDITIVE - (128-9009-0001) 52

HMU BLEED AIR IMPROVEMENT - (128-9110-1) 52

HMU BLEED AIR IMPROVEMENT - (128-9110-3) 53

FUEL CAPS, MEDECO LOCK - (128-9202-0003) 53

HORIZONTAL STAB DEICER GAP CONTACTOR - (132-3019-1 S) 53

FASTENER MODIFICATION INLET DUCT ASSEMBLY-INFO ONLY - (132-9100-0001) 53

FASTENER MODIFICATION INLET DUCT ASSEMBLY-INFO ONLY - (132-9100-0002) 54

COVER PLATE - (140-8004-0001)

54

WINDSHIELD DEFOGGER - (400-3003-1 S) 54

CHIME INSTALLATION - (400-5005-1 S) 54

BEARING REWORK, NOSE WHEEL - (400-8001-1 S) 55

INTAKE DUCT, ENGINE - (400-9001-1 S) 55


KIT CATALOG

101-2003-1 SEXTERIOR MARKING "BEECHCRAFT" NEW STYLE LOGO ATA :400, 400A ADDED TO EFFECTED AIRCRAFT PER CO

NO.G41580 7/16/92THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SPARES REPLACEMENT FOR THE101-531347-1 PLACARD.

NOTENOTENOTENOTE:::: MASKS FURNISHED IN THIS KIT ARE DESIGNED FOR SINGLE COLOR LETTER PAINTING.NOTENOTENOTENOTE:::: PAINT IS NOT INCLUDED IN THE KIT. WILL NEED TO PURCHASE PAINT "BEECHCRAFT

RED" PART NUMBER 2351, IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


101-3045-1PITCH TRIM CONTROLLER ATA : 27400A RK-45, RK-49 THRU RK-97, RK-99 THRU

RK-109SB NO. 27-3005THIS KIT PROVIDES SUPPLIES AND INFORMATION TO INSTALL HORIZONTAL STABILIZER PITCH TRIMWIRING FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REFERENCE ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: INS/EXT TOOLS;M81969/14-02, M81969/14-02, M81969/14-11 & M81969-1-2, EXTRACTION TOOL: 305183.CRIMP TOOLS: 90067-4, M2250/1-01, M22520,M22520/5-01. DIE M22520/5-103. SOLDER:SN60WRMAP3.031. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.





KIT CATALOG

128-1001-0001FLAP AERO SEAL, INSTL ATA :400A RJ-1 THRU RJ-65, RK-1 THRU ECR 14898THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL WING TRAILING EDGE PROTECTOR SEAL FORIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "SILPAK A400" ADHESIVE, "MIL-C-5541" CHEMFILM, "S2260" & "MIL-P-13377G" PRIMERREQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

WT. CHANGE : +2.6 LB. MOMENT: +822.0 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-1600-1SECTIONED LEADING EDGE, MAIN FLAP INSTALLATION ATA : 57400 RJ-1 THRU RJ-65400A RK-1 AND AFTER400T (T-1A) TT-1 AND AFTER400T (TX) TX-1 AND AFTER"OPTIONAL" SB NO. 2588, REV. I, SEPTEMBER, 1996THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY INSERVICE 400, 400A, AND 400TMAIN FLAP LEADING EDGES FROM (3) SINGLE PIECE SECTIONS TO (3) MULTI-PIECE SECTIONS FOREASIER ACCESS TO MAIN FLAP TRACKS AND BEARINGS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MIL-S-8802 TYPE II, CLASS "B" SEALER SUCH AS "890 PINT" OR "PR1440A1/2" OREQUIVALENT IS REQUIRED TO INSTALL THIS KIT. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.


128-3001-1 PGENERATOR CONTROL UNIT ATA : 24400 RJ-1 THRU RJ-65MU-300 1001 AND UP"M"S.B.#24-3713THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH AND RH GENERATOR CONTROL UNIT ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT INSTALLS 2 LUCAS GCU'S, PART NUMBER 45AS88801-019, AND DOES NOTREQUIRE INSTALLATION OF LUCAS STARTER-GENERATORS, PART NUMBER45AS88801-017 WHICH ARE PART OF KIT 128-3004-1 P. 128-3004-1 P MUST BE USED INCONJUNCTION WITH 128-3001-1 P OR -3 P KIT



KIT CATALOG

128-3001-3 PGENERATOR CONTROL UNIT ATA : 24400A RK-1 THRU RK-23"M"S.B.#24-3713THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A LH AND RH GENERATOR CONTROL UNIT ONINSERVICE AIRCRAFT. 128-3004-1 P MUST BE USED IN CONJUNCTION WITH 128-3001-3 P.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES 2 LUCAS GCU'S, PART NUMBER 45AS88801-019. THIS KIT IS NOTREQUIRED FOR INSTALLATION OF LUCAS STARTER-GENERATORS WHICH ARECONTAINED IN KIT 128-3004-1 P. USAGE OF THIS KIT WILL LOWER STARTER WIND-UP OFAIRCRAFT WHICH CURRENTLY HAVE LUCAS STARTER-GENERATORS AND SHINKOGCU'S.


128-3002-1 SVLF SYSTEM OPERATION ACTIVATION ATA :400A RK-2 THRU RK-5THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT FOR VLF OPERATION ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

128-3004-1 PGENERATOR INSTALLATION ATA : 24400 RJ-1 THRU RJ-65400A RK-1 THRU RK-23MU-300 1001 AND UPTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 45AS88801-023 STARTER-GENERATOR ONINSERVICE AIRCRAFT AS A REPLACEMENT FOR 45AS88801-013.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES ONE STARTER-GENERATOR. LUCAS STARTER-GENERATOR45AS99901-017 PROVIDED IN THIS KIT MAY BE USED WITH SHINKO STARTER-GENERATOR ON THE OTHER ENGINE. THIS KIT DOES REQUIRE INSTALLATION OF KIT128-3001-1 P OR -3 P KIT WHICH CONTAINS 2 LUCAS GCU'S, P/N 45AS88801-019 THAT WILLLOWER STARTER WIND-UP BACK TO NORMAL READINGS. STARTER WIND-UP SPEC'SWILL BE HIGHER WITH A LUCAS AND SHINKO MIX BUT WILL BE ACCEPTABLE RAYTHEONSPEC'S OPERATION LIMITS.


128-3004-3 PGENERATOR INSTALLATION ATA :400 RJ-1 THRU RJ-65400A RK-1 THRU RK-23MU-300 1001 AND UPTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A 45AS88801-023 STARTER GENERATOR ONINSERVICE AIRCRAFT. THIS KIT REPLACES 45AS88801-013. LUCAS STARTER-GENERATOR 45AS88801-017PROVIDED IN THIS KIT MAY BE USED WITH SHINKO STARTER-GENERATOR ON OTHER ENGWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)


KIT CATALOG

128-3007-1 SFLIGHT DISPLAY UPDATE ATA :400A RK-1 THRU RK-8, RK-10 THRU RK-18THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A THREE TUBE FLIGHTDISPLAY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

128-3007-3 SFLIGHT DISPLAY UPDATE ATA :400A RK-1 THRU RK-8, RK-10 THRU RK-18THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A FOUR TUBE FLIGHTDISPLAY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

128-3008-1 SCATEGORY II APPROACH SYSTEM INSTALLATION ATA :400A RK-1 THRU RK-44, RK-46 THRU RK-48THIS KIT PROVIDES "INFORMATION ONLY" TO MODIFY AIRCRAFT WITH THREE TUBE FLIGHT DISPLAYSFOR CATEGORY II OPERATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24 TO 28MEN : 1 (MAN)

128-3008-3 SCATEGORY II APPROACH SYSTEM INSTALLATION ATA : 22400A RK-1 THRU RK-44, RK-46 THRU RK-48THIS KIT PROVIDES "INFORMATION ONLY" TO MODIFY AIRCRAFT WITH FOUR TUBE FLIGHT DISPLAYS FORCATEGORY II OPERATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 24 TO 28MEN : 1 (MAN)

128-3009-1 SSTALL RECOGNITION SUPPLEMENTARY SYSTEM ATA :400A RK-1 THRU RK-23THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SUPPLEMENTAL STALL RECOGNITIONSYSTEM TO THE AOA SYSTEM FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS PART OF THE 128-8001-1 S KIT, AND MAY BE REQUIRED AS A REPLACEMENTONLY AFTER THE 128-8001-1 S KIT HAS BEEN INSTALLED.



KIT CATALOG

128-3011-1 STRANSPONDER DUAL INSTALLATION TDR-94 ATA : 34400A RK-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DUAL TDR-94 (MODE S) TRANSPONDERS.

NOTENOTENOTENOTE:::: CORE DEPOSIT FOR 2 EACH TDR90 TRANSPONDERS AT $3,800.00 CREDIT EACH AND 2EACH CAD870 ADAPTER AT $1,200.00 CREDIT EACH WILL BE ISSUED AFTER OLD UNITSARE RETURNED ON MANUALLY APPROVED OVH PART RETURN.

WT. CHANGE : WT: 8.9 LBS; MOMENT; 641 IN.-LBSEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

128-3012-1 SVLF OMEGA RECEIVER UPDATE ATA : 23400 RJ-61400A RK-1 THRU RK-23THIS KIT PROVIDES "INFORMATION ONLY", NECESSARY FOR VLF UPDATE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 5MEN : 1 (MAN)

128-3013-1 SFLIGHT CONTROL SYSTEM UPDATE INFORMATION ATA : 27400 RJ-61400A RK-1 THRU RK-23THIS KIT PROVIDES "INFORMATION ONLY", NECESSARY FOR FLIGHT CONTROL SYSTEM UPDATE ONINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 5MEN : 1 (MAN)

128-3015-1 SICC CARD CHANGE ATA : 34400A RK-1 THRU RK-44, RK-46 THRU RK-48"RECOMMENDED" SB NO. 2505, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CHANGE CARD CAGE ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT DOES NOT CONTAIN CARD CAGE, YOU NEED TO CONTACT: COLLINS RADIOPRODUCT SUPPORT DEPT., CEDAR RAPIDS, IA. TO SCHEDULE AN EXCHANGE UNIT PARTNUMBER: 622-9342-002 CARD CAGE WHEN YOU ORDER THIS KIT FOR THE 622-9342-001CARD CAGE YOU WILL REMOVE FROM AIRCRAFT.

NOTENOTENOTENOTE:::: YOUR WILL NEED A M22520/1-01 CRIMPER WITH AN M22520/1-04 POSITIONER TO INSTALLTHE SOCKET CONTACTS. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



KIT CATALOG

128-3016-1 SNAV TAIL LIGHT INSTALLATION ATA : 33400A RK-45, RK-49 THRU RK-78400T (T-1A) TT-1 THRU TT-49T-1A SI NO.: T-1A-0015THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL A NAV TAIL POSITION LIGHTON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 895B1/2 QT PROSEAL WILL BE REQUIRED WHEN REPLACING THE A555V-28 NAV TAILLIGHT, BUT IS NOT FURNISHED WITH THIS KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK,YOU CAN PROCURE LOCALLY.


128-3017-1 SWIRE HARNESS CLAMPING, MAIN LANDING GEAR WHEEL WELL ATA : 32400A RK-1 THRU RK-41400T JAYHAWK (T-1A) TT-2 THRU TT-19"MANDATORY" SB NO. 2479, JANUARY 29, 1993THIS KIT WILL PROVIDE THE PARTS AND INFORMATION NECESSARY INFORMATION TO ADD ADDITIONALCLAMPS TO THE LH AND RH WHEEL WELL WIRE HARNESSES. THIS KIT IS TO PREVENT MAIN LANDINGGEAR TIRES FROM DAMAGING WIRES THAT PROVIDE CURRENT TO THE BOOSTPUMPS, LOW FUELWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

128-3019-1 SAIR DATA SYSTEM MACH SPEED CORRECTION ATA : 34400A RK-52, RK-65 THRU RK-73THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO CHANGE AIR DATA COMMUTERS ANDSTRAPPING DEFINITION OF MATING CONNECTORS ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: YOU WILL NEED TO CONTACT COLLINS RADIO PRODUCT SUPPORT DEPARTMENT,CEDAR RAPIDS, IA TO SCHEDULE AN EXCHANGE FOR TWO EACH ADC-850D (CPN822-0398-118) IN COMPLIANCE WITH COLLINS SERVICE BULLETIN NO. 19 FOR ADC-850D.


128-3021-1 SROTOR BURST HAZARD MINIMIZATION UPDATE INSTALLATION ATA : 71400A RK-45, RK-49 THRU RK-75"MANDATORY" SB NO. 2517THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO UPGRADE MODEL 400A AIRCRAFT TOMINIMIZE THE CHANCE OF FUEL IGNITION IN THE EVENT OF A ROTOR BURST FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR EARLIER SERIAL NUMBERS SEE 128-3021-3 S KIT.NOTENOTENOTENOTE:::: THE FOLLOWING MATERIAL REQUIRED FOR INSTALLATION, BUT NOT FURNISHED WITH

KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. NAPTHAPART NUMBER "NAPTHA TT-N-95A"; CHEM-FILM PART NUMBER "ALODINE 1200" ANDEPOXY PRIMER PART NUMBER "MILP23377D GL".



KIT CATALOG

128-3021-3 SROTOR BURST HAZARD MINIMIZATION UPDATE INSTALLATION ATA : 71400A RK-1 THRU RK-44, RK-46 THRU RK-48"MANDATORY" SB NO. 2517THIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO UPGRADE MODEL 400A AIRCRAFT TOMINIMIZE THE CHANCE OF FUEL IGNITION IN THE EVENT OF A ROTOR BURST FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR LATER MODEL 400A SERIAL NUMBERS SEE 128-3021-1 S KIT.NOTENOTENOTENOTE:::: THE FOLLOWING MATERIAL REQUIRED FOR INSTALLATION, BUT NOT FURNISHED WITH

KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. NAPTHAPART NUMBER "NAPTHA TT-N-95A"; CHEM-FILM PART NUMBER "ALODINE 1200" ANDEPOXY PRIMER PART NUMBER "MILP23377D GL."


128-3022-1 SSTANDBY LIGHTING IMPROVEMENT INSTALLATION ATA : 33400A RK-45, RK-49 THRU RK-69SB NO. 2563THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE THE AIRCRAFT STANDBY LIGHTING FOR THEINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR SERIAL NUMBERS RK-1 THRU RK-44, AND RK-46 THRU RK-48 SEE 128-3026-1 S KIT.NOTENOTENOTENOTE:::: FOR SERIAL NUMBERS RK-70 THRU RK-80 SEE 128-3025-1 S KIT.


128-3023-1 SAUTOPILOT AND RUDDER BOOST INTERLOCK UPDATE ATA : 22400A RK-45, RK-49 THRU RK-92THIS KIT PROVIDES PARTS AND INFORMATION TO CHANGE CARDS IN CARD CAGE, ADD RELAYS TO J-BOX AND WIRING INFORMATION SO REMOVAL OF PLACARD FROM IP CAN BE AUTHORIZED ONAPPLICABLE MODEL 400A AIRCRAFT. FOR OTHER MODELS AND SERIAL NUMBERS SEE 128-3023-5 S AND

NOTENOTENOTENOTE:::: CONTACT COLLINS - WICHITA FOR SCHEDULING OF YOUR FCC850 FOR MODIFICATIONSREQUIRED TO UNIT FOR USAGE IN CONJUNCTION WITH THIS KIT INSTALLATION.

NOTENOTENOTENOTE:::: IF YOU HAVE ANY QUESTIONS ON UPDATING AIRCRAFT FLIGHT MANUAL PART NUMBER128-590001-109 PER KIT INSTRUCTIONS, CONTACT TECHNICAL PUBLICATIONS FORASSISTANCE.

NOTENOTENOTENOTE:::: MS3367-1-9 CABLE TIE STRAPS OR EQUIVALENT ARE REQUIRED FOR USE BUT ARE NOTPART OF KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

128-3023-5 SAUTOPILOT AND RUDDER BOOST INTERLOCK UPDATE ATA : 22400A RK-1 THRU RK-44, RK-46 THRU RK-48"MANDATORY" SB NO. 2533, REV. 1, APRIL, 1995THIS KIT PROVIDES PARTS AND INFORMATION TO CHANGE CARDS IN CARD CAGE, ADD RELAYS TO J-BOX AND WIRING INFORMATION SO REMOVAL OF PLACARD FROM IP CAN BE AUTHORIZED ONAPPLICABLE AIRCRAFT.

NOTENOTENOTENOTE:::: CONTACT COLLINS - WICHITA FOR SCHEDULING OF YOUR FCC850 FOR MODIFICATIONSREQUIRED TO UNIT FOR USAGE IN CONJUNCTION WITH THIS KIT INSTALLATION.

NOTENOTENOTENOTE:::: FOR OTHER MODELS AND SERIAL NUMBERS SEE 128-3023-1 S AND 128-3023-7 S KITS.NOTENOTENOTENOTE:::: IF YOU HAVE ANY QUESTIONS ON UPDATING AIRCRAFT FLIGHT MANUAL PART NUMBER:

128-590001-109 PER KIT INSTRUCTIONS, CONTACT TECHNICAL PUBLICATIONS.NOTENOTENOTENOTE:::: MS3367-1-9 CABLE TIE STRAPS OR EQUIVALENT ARE REQUIRED FOR USE BUT ARE NOT

PART OF KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN BE OBTAINEDLOCALLY.


128-3025-1 SSTANDBY LIGHTING IMPROVEMENT ATA : 33400A RK-70 THRU RK-80SB NO. 2536THIS KIT PROVIDES PARTS AND INFORMATION TO UPGRADE THE AIRCRAFT STANDBY LIGHTING FORINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR EARLIER MODEL 400A'S SEE 128-3026-1 S KIT.NOTENOTENOTENOTE:::: INSTALLATION OF THIS KIT ALLOWS FOR THE USE OF EL PRODUCTS PART NUMBER

76699-01 OR PACIFIC SYSTEMS PART NUMBER 866-1-1 POWER SUPPLIES AS AREPLACEMENT FOR POWER SUPPLY PART NUMBER PS104 ON THE AIRCRAFT.


128-3026-1 SSTANDBY LIGHTING IMPROVEMENT ATA : 33400A RK-1 THRU RK-44, RK-46 THRU RK-48SB NO. 2563THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPGRADE AIRCRAFT STANDBY LIGHTINGFOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR RK-70 THRU RK-80 SEE 128-3025-1 S KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5 TO 2.5MEN : 1 (MAN)


KIT CATALOG

128-3027-1 SFLIGHT HOUR METER IMPROVEMENT ATA : 31400A RK-45, RK-49 THRU RK-77, RK-79 THRU

RK-86THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPGRADE AIRCRAFT FLIGHT HOURMETER CIRCUIT FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR OTHER 400A AIRCRAFT SEE KIT 128-3028-1 S.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)

128-3028-1 SFLIGHT HOUR METER IMPROVEMENT ATA : 31400A RK-1 THRU RK-44, RK-46 THRU RK-48THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPGRADE AIRCRAFT FLIGHT HOURMETER CIRCUIT FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR OTHER MODEL 400A SEE 128-3027-1 S KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 1.5MEN : 1 (MAN)

128-3030-1 SAUTOPILOT UPDATE ATA :400A RK-58, RK-65, RK-73, RK-79THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH ICC-851 CARD CAGEAUTOPILOT SYSTEM INSTALLED.

NOTENOTENOTENOTE:::: WILL NEED TO CONTACT VENDOR: ROCKWELL INTERNATIONAL CORP., COLLINSAVIONICS CEDAR RAPIDS, IOWA, SERVICE CENTER FOR EXCHANGE/MODIFICATION OFYOUR EXISTING PARTS 622-7410-302 FCC-850 FLIGHT CONTROL COMPUTER TO MOD-STATUS PER SERVICE BULLETIN -20 REQUIREMENTS.


128-3031-1 SELT-EMERGENCY LOCATOR TRANSMITTER INSTALLATION ATA :400A RK-71, RK-79 THRU RK-86 (EXCLUDING

RK-80)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN EMERGENCY LOCATORTRANSMITTER ON INSERVICE AIRCRAFT (WITH PROVISIONAL WIRING).

NOTENOTENOTENOTE:::: FOLLOWING REQUIRED FOR INSTALLATION BUT NOT FURNISHED WITH KIT: "ALODINE1200" COATING AND TRICHLOROETHANE CLEANING SOLVENT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. TRICHLOROETHANE IS NO LONGEROFFERED BY RAYTHEON, IT'S EQUIVALENT FOR THIS INSTALLATION TASK, "MEK" OR"NAPTHA TT-N-95A" ARE STILL OFFERED.



KIT CATALOG

128-3031-3ELT-EMERGENCY LOCATOR TRANSMITTER INSTALLATION ATA :400 RK-45, RK-49 THRU RK-77 (EXCLUDING

RK-71)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL AN EMERGENCY LOCATORTRANSMITTER ON INSERVICE AIRCRAFT (WITH PROVISIONAL WIRING).

NOTENOTENOTENOTE:::: FOLLOWING REQUIRED FOR INSTALLATION BUT NOT FURNISHED WITH KIT: "ALODINE1200" COATING AND TRICHLOROETHANE CLEANING SOLVENT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. TRICHLOROETHANE IS NO LONGEROFFERED BY RAYTHEON, IT'S EQUIVALENT FOR THIS INSTALLATION TASK, "MEK" OR"NAPTHA TT-N-95A" ARE STILL OFFERED.


128-3035-1STANDBY BATTERY TEST CIRCUIT IMPROVEMENT ATA : 24400A RK-45, RK-49 THRU RK-80400A RK-81 THRU RK-121"OPTIONAL" SB NO. 24-3004, REV. 1THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH AN IMPROVED STANDBYBATTERY TEST CIRCUIT.

NOTENOTENOTENOTE:::: INSTALLATION NOT COMPLETE UNTIL AIRCRAFT FLIGHT MANUAL OR PILOTS OPERATINGHANDBOOK REVISION (OR SUPPLEMENT) HAS BEEN INCORPORATED. IF NOT AVAILABLEIN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. YOU MUST BE USING -109 OR -167AFM (UPDATED PER NOTES ON DRAW XXXXXXXXXXXXX (SEE EDOCS 2001 FOR THEUPDATE)

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, "SN60WRMAP3.031" SOLDER FED QQ-S-571AND NYLON TIE TAPE, "MILT43435 BLACK", OR "MILT43435 WHITE" TYPE 1, FIN:B OR MIL-T43435 TYPE 1, FIN:C. IF NOT IN AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


128-3036-1STANDBY BATTERY TEST CIRCUIT IMPROVEMENT ATA : 24400 RJ-1 THRU RJ-65400A RK-1 THRU RK-48, EXCEPT RK-45"OPTIONAL" SB NO. 24-3004, REV 1THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY MODEL 400 AND 400A SERIES SERVICEAIRCRAFT WITH AN IMPROVED TEST CIRCUIT.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED QUANTITY ITEMS NOT FURNISHED WITH THE KIT, IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY. NYLON TIE TAPE"MILT43435 BLACK" OR "MILT43435 WHITE" TYPE 1, FIN:B OR MIL-T43435TYPE 1, FIN:C,AND "SN60WRMAP3.031" SOLDER FED QQ-S-571

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION HAS BEEN INCORPORATED. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

128-3037-1FLIGHT DIRECTOR CROSSPOINTER DISPLAY ATA : 34400A RK-93, RK-96THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH A FOUR TUBE CROSSPOINTERDISPLAY.

NOTENOTENOTENOTE:::: NOT FURNISHED BUT REQUIRED WITH KIT, PILOT'S OPERATING MANUAL SUPPLEMENT129-590001-179. MUST ORDER SEPARATELY.


128-3038-1IGNITOR WIRING CHANGE, BURST MODE IGNITION ATA : 74400 RJ-1 THRU RJ-65SB NO. 2582THIS KIT PROVIDES PARTS AND INFORMATION TO UPGRADE AIRCRAFT IGNITOR INDICATOR CIRCUIT TOACCOMMODATE BURST MODE OR STANDARD MODE IGNITION FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: 4 EA. "115110D6" TERMINAL, 2 EACH"M39029/4-110" PIN CONTACT AND "SN60WRMAP.-31" SOLDER QQ-S-571. YOU WILL ALSOREQUIRE THE FOLLOWING TOOLS: "47386" SPLICE CRIMP TOOL, "M22520/1-01" CRIMPTOOL, "M2520/1-02"POSITIONER TOOL (TURRET) AND "M81969/14-01" EXTRA/INSERTTOOL. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.


128-3039-1IGNITOR WIRING CHANGE, BURST MODE IGNITION ATA : 74400A RK-1 THRU RK-44, RK-46 THRU RK-48SB NO. 2582THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT IGNITOR INDICATOR CIRCUIT TOACCOMMODATE BURST MODE OR STANDARD MODE IGNITION FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

128-3039-3IGNITOR WIRING CHANGE, BURST MODE IGNITION ATA : 74400A RK-45, RK-49 THRU RK-87SB NO. 2582THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT IGNITOR INDICATOR CIRCUIT TOACCOMMODATE BURST MODE OR STANDARD MODE IGNITION FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

128-3042-1WING ANTI-ICE TEMPERATURE LOW, ANNUNCIATOR LIGHT ATA : 30400 RJ-1 THRU RJ-65THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO RECONFIGURE THE WING ANTI-ICEOPERATIONAL LIGHT TO ILLUMINATE ONLY WHEN WING ANTI-ICE BLEED AIR PRESSURE IS DETECTEDAND TO ADD A WING ICE TEMPERATURE LOW ANNUNICATOR LIGHT TO THE RIGHT ANNUNCIATOR PANEL

NOTENOTENOTENOTE:::: "AA52080-B-3" "MILT43435 BLACK" TYING TAPE; "SN60WRMAP3" SOLDER;"M39029/4-110"PIN; "M39029/5-115" SOCKET; "M39029/30-217" CONTACT; "M81824/1-1" &"M81824/1-2 "SPLICE; "115110D6" & "115110D8 "TERMINAL; "M22520/1-01" "M22520/1-01" &"M22520/5-01"CRIMP TOOL; "M22520/1-02"RED&BLUE POSITIONER;"M22520/5-103"DIETOOL;HEAT SHRINK;"47386" SPLICE TOOL;"M81969/14-02" & "M1969/14/03 "INSERT/EXTRACTION TOOL. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPROPRIATE AIRCRAFT FLIGHTMANUAL REVISION (OR SUPPLEMENT) HAS BEEN INCORPORATED. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : 1.0 LB; MOMENT: 240 LB-INEST. MAN/HRS: : 92 HRS.MEN : 1 (MAN)

128-3042-3WING ANTI-ICE TEMPERATURE LOW, ANNUNCIATOR LIGHT ATA : 30400A RK-1 THRU RK-19"O" S.B. #30-3007 ISSUED 1/05THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO RECONFIGURE THE WING ANTI-ICEOPERATIONAL LIGHT TO ILLUMINATE ONLY WHEN WING ANTI-ICE BLEED AIR PRESSURE IS DETECTEDAND TO ADD A WING ICE TEMPERATURE LOW ANNUNICATOR LIGHT TO THE RIGHT ANNUNCIATOR PANEL

NOTENOTENOTENOTE:::: "AA52080-B-3" "MILT43435 BLACK" TYING TAPE; "SN60WRMAP3" SOLDER;"M39029/4-110"PIN; "M39029/5-115" SOCKET; "M39029/30-217" CONTACT; "M81824/1-1" &"M81824/1-2" SPLICE; "115110D6" & "115110D8" TERMINAL; "M22520/1-01" "M22520/1-01" &"M22520/5-01" CRIMP TOOL; "M22520/1-02" RED&BLUE POSITIONER; "M22520/5-103" DIETOOL; HEAT SHRINK; "47386" SPLICE TOOL; "M81969/14-02" & "M1969/14/03" INSERT/EXTRACTION TOOL. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


WT. CHANGE : 1.0 LB; MOMENT: 240 LB-INEST. MAN/HRS: : 92 HRSMEN : 1 (MAN)


KIT CATALOG

128-3042-5WING ANTI-ICE TEMPERATURE LOW, ANNUNCIATOR LIGHT ATA : 30400A RK-20 THRU RK-44, RK-46, RK-47 & RK-48THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO RECONFIGURE THE WING ANTI-ICEOPERATIONAL LIGHT TO ILLUMINATE ONLY WHEN WING ANTI-ICE BLEED AIR PRESSURE IS DETECTEDAND TO ADD A WING ICE TEMPERATURE LOW ANNUNICATOR LIGHT TO THE RIGHT ANNUNCIATOR PANEL


NOTENOTENOTENOTE:::: "AA52080-B-3" "MILT43435 BLACK" TYING TAPE; "SN60WRMAP3" SOLDER; "M39029/4-110"PIN; "M39029/5-115" SOCKET; "M39029/30-217" CONTACT; "M81824/1-1" & "M81824/1-2"SPLICE; "115110D6" & "115110D8" TERMINAL; "M22520/1-01" "M22520/1-01" & "M22520/5-01"CRIMP TOOL; "M22520/1-02" RED&BLUE POSITIONER; "M22520/5-103" DIE TOOL; HEATSHRINK; "47386" SPLICE TOOL; "M81969/14-02" & "M1969/14/03" INSERT/EXTRACTIONTOOL. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : 1.0 LB; MOMENT: 240 LB-INEST. MAN/HRS: : 92 HRSMEN : 1 (MAN)

128-3043-1WING ANTI-ICE TEMPERATURE LOW,ANNUNCIATOR LIGHT ATA : 30400A RK-45 & RK-49 THRU RK-354"O" S.B. #30-3007 ISSUED 1/05THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO RECONFIGURE THE WING ANTI-ICEOPERATIONAL LIGHT TO ILLUMINATE ONLY WHEN WING ANTI-ICE BLEED AIR PRESSURE IS DETECTEDAND TO ADD A WING ICE TEMPERATURE LOW ANNUNCIATOR LIGHT TO THE RIGHT ANNUNCIATOR PANEL

NOTENOTENOTENOTE:::: "AA52080-B-3" & "MIL-T-43435B" TAPE, TYING & SOLDER REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANY OUTLET.

WT. CHANGE : 1.0 LB MOMENT: 240 LB-INEST. MAN/HRS: : 92 HRSMEN : 1 (MAN)

128-3044-1CIRCUIT BREAKER REPLACEMENT INSTALLATION - SPARES ATA :400 RJ-1 THRU RJ-65400A RK-1 THRU RK44, RK-46 THRU RK-48400T (T-1A) TT-1 THRU TT-146400T (TX) TX-1 THRU TX- 8DIAMOND 1A/2 003 THRU 999PENDING SI T-1A-0067 FOR MODEL 400T'STHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL REPLACEMENT CIRCUIT BREAKERS FOR6363-1-35 BREAKERS FOR THE LEFT AND RIGHT NONESSENTIAL BUSSES FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: RK-45, RK-49 THRU RK-111, TX-1 THRU TX-8, AND TT-1 THRU TT-146 SEE 128-3044-3.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

128-3044-3CIRCUIT BREAKER REPLACEMENT INSTALLATION ATA : 24400A RK-45, RK-49 THRU RK-111400T (T-1A) TT-1 THRU TT-146400T (TX) TX-1 THRU TX- 8SI NO. T-1A-0067 FOR MODEL 400T'STHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL REPLACEMENT CIRCUITBREAKERS FOR THE LEFT AND RIGHT NONESSENTIAL BUSSES FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR MU300 DIAMONDS, 400 AND EARLY 400A MODELS SEE 128-3044-1 KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12MEN : 1 (MAN)

128-3045-1PITCH TRIM CONTROLLER ATA : 27400A RK-45,RK-49 THRU RK-166SB NO. 27-3005THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HORIZONTAL STABILIZER PITCH TRIM WIRINGFOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR REFERENCE ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: INS/EXT TOOLS;M81969/14-02, M81969/14-03, M81969/14-11 AND M81969-1-2. EXTRACTION TOOL: 305183.CRIMP TOOLS; 90067-4, M22520/1-01, M22520/5-01, DIE M22520/5-103, SOLDER;SN60WRMAP3.031. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


128-3045-5PITCH TRIM CONTROLLER ATA : 27400A RK-98, RK-110 AND AFTERSB NO. 27-3005THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HORIZONTAL STABILIZER PITCH TRIM WIRINGFOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REFERENCE ITEMS REQUIRED BUT NOT SUPPLIED WITH KIT: INS/EXT TOOLS;M81969/14-02, M81969/14-03, M81969/14-11 AND M81969-1-2. EXTRACTION TOOL: 305183.CRIMP TOOLS; 90067-4, M22520/1-01, M22520/5-01, DIE M22520/5-103, SOLDER;SN60WRMAP3.031. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



KIT CATALOG

128-3049-3EMI SUPPRESSION AVIONICS ATA : 34400 RJ-61400A RK-1 AND AFTER"RECOMMENDED" SB NO. 34-3006THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SUPPRESSION CORES TO PROVIDE AVIONICEMI SUPPRESSION FOR INSERVICE 4 TUBE AIRCRAFT.WT. CHANGE : WT: + 1.6 LBS, MOMENT: 123 IN.-LBSEST. MAN/HRS: : 8MEN : 1 (MAN)

128-3049-5EMI SUPPRESSION AVIONICS ATA : 34400 RJ-61400A RK-1 AND AFTER"RECOMMENDED "SB NO. 34-3006THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SUPPRESSION CORES TO PROVIDE AVIONICEMI SUPPRESSION FOR INSERVICE 2 TUBE AIRCRAFT.WT. CHANGE : WT: + .8 LBS, MOMENT: 62 IN.-LBSEST. MAN/HRS: : 6MEN : 1 (MAN)

128-3051-1PITCH TRIM CONTROLLER ATA : 27400A RK-1 THRU RK-44, RK-46 THRU RK-48SB NO. 27-3005THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PITCH TRIM CONTROLLER AND PITCH TRIMWIRING FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 47386, M22520/1-01, M22520/5-01 CRIMP TOOLS; M81969-1-02, M81969/14-02 INS/EXT TOOL;M22520/1-02 TURRET; M22520/5-10 DIE; SN60WRMAP3.031 SOLDER; MILT43435 TYINGNYLON TAPE REQUIRED, BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

128-3052-1WING ANTIICE SYSTEM, DUAL CONTROL ATA : 30MU-300 A003SA THRU A091SATHIS KIT PROVIDES PARTS AND INFORMATION TO ADD A SECOND (DUAL) CONTROL SYSTEM FOR WINGANTIICE, RECONFIGURE WING ANTIICE OPERATIONAL LIGHT TO ILLUMINATE ONLY AFTER THE MINIMUMBLEED AIR PRESSURE IS DETECTED, & ADD "WING ICE TEMP LO" CAUTION (YELLOW) ANNUN

NOTENOTENOTENOTE:::: 128-5041-1 IS INCLUDED IN THIS KITNOTENOTENOTENOTE:::: "M81969/14-03""M81969/14-02" INS/EXT TOOL, "M22520/5-103""M22520/5-100" OR

"M22520/10-101" DIE, "M22520/5-01"OR"M22520/10-01""M22520/1-01" CRIMP TOOL,"M22520/1-02" POSITIONER, "MS20995C20" LOCK WIRE, "MS3367-4-9""MS3367-1-9" TIE-DOWN STRAP, "MIL-T-43435" TYING TAPE, NYLON, "SN60WRMAP3" SOLDER REQUIREDBUT NOT INCLUDED IN KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE AIRPLANE FLIGHT MANUALSUPPLEMENT (MU-300FMS96) HAS BEEN INCORPORATED. PROCURE SEPERATELY FROMANY COMPANY AUTHORIZED OUTLET.


128-3053-1HORIZONTAL STAB DE-ICE, GAP CONTACTOR ATA : 30MU-300 A003SA THRU A005SA, A007SA THRU

A021SA"RECOMMENDED" SB NO. 30-3204THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HORIZONTAL STAB DE-ICE WIRING FOR US ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SN60WRMAP3 SOLDER, M81969/14-02, M22520/5-01, M22520/1-01, MS25441, 600850-1TOOLS, M22520/5-100, MS23002 DIE, M22520/1-02 RED POSITIONER, MILT43435 NYLONTAPE AND 515-700 EPOXY PRIMER-GREEN REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: +5.0 LBS MOMENT: 2114 IN.-LBSEST. MAN/HRS: : 30MEN : 1 (MAN)

128-3053-3HORIZONTAL STAB DE-ICE, GAP CONTACTOR ATA : 30MU-300 A006SA, A022SA THRU A091SA"RECOMMENDED" SB NO. 30-3204THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HORIZONTAL STAB DE-ICE WIRING FOR US ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SN60WRMAP3 SOLDER, M81969/14-02, M22520/5-01, M22520/1-01, MS25441, 600850-1TOOLS, M22520/5-100, MS23002 DIE, M22520/1-02 RED POSITIONER, MILT43435 NYLONTAPE AND 515-700 EPOXY PRIMER-GREEN REQUIRED BUT NOT FURNISHED WITH KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: +5.0 LBS MOMENT: 2114 IN.-LBSEST. MAN/HRS: : 30MEN : 1 (MAN)


KIT CATALOG

128-3054-1DC CONVERTER ATA : 24

400A RK-98, RK-110 THRU RK-244"RECOMMENDED" SB NO. 24-3574THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A DC CONVERTER AND WIRING FOR LAPTOPCOMPUTER ON IN-SERVICE AIRCRAFT.

WT. CHANGE : +5.0 LB. MOMENT: +1.037 LB-IN.EST. MAN/HRS: : 48MEN : 1 (MAN)

128-3054-5DC CONVERTER ATA : 24400A RK-245 THRU RK-352"RECOMMENDED" SERVICE BULETIN NO. 24-3574THIS KIT PROVIDES PARTS AND INFORMATION TO REWORK DC POWER SUPPLY INSTALLATION ON IN-SERVICE AIRCRAFT.WT. CHANGE : +5.0 LB. MOMENT: +1.037 LB-INEST. MAN/HRS: : 16MEN : 1 (MAN)

128-3055-1ENGINE IGNITOR CIRCUIT IMPROVEMENT ATA : 74400A RK-45, RK-49 THRU RK-87 (DELIVERED

WITHOUT BURST MODE IGNITION IGNITORWIRING CHANGE AND WITHOUT FIELDINSTALLATION OF BURST MODE IGNITIONIGNITOR WIRING CHANGE KIT 128-3039)

"RECOMMENDED" SB NO. 74-3290 ISSUED 01/01THIS KIT PROVIDES PARTS AND INFORMATION TO REWIRE THE IGNITOR CIRCUIT TO ALLOW IGNITORS TOFIRE EARLIER IN THE ENGINE START SEQUENCE ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SN60WRMAP3 SOLDER, M81969/14-02, M81969/14-03, M21097/18-01 TOOL, M22520/5-103DIE, M22520/1-02 RED POSITIONER, M22520/5-01, M22520/1-01, 90083, 90005, 47386 CRIMPTOOLS, MIL-T-43435 NYLON TYING TAPE REQUIRED BUT NOT FURNISHED WITH KIT. THISKIT IS NOT COMPLETE UNTIL THE AIRCRAFT FLIGHT MANUAL AND PILOT’S OPERATINGMANUAL REVISIONS HAVE BEEN INCORPORATED. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

128-3055-3ENGINE IGNITOR CIRCUIT IMPROVEMENT ATA : 74400A RK-45, RK-49 THRU RK-87 (DELIVERED

WITH FIELD INSTALLATION OF BURSTMODE IGNITION IGNITOR WIRING CHANGEKIT 128-3039)RK-88 THRU RK-220(DELIVERED WITH BURST MODE IGNITIONIGNITOR WIRING CHAN

"RECOMMENDED" SB NO. 74-3290 01/01THIS KIT PROVIDES PARTS AND INFORMATION TO REWIRE THE IGNITOR CIRCUIT TO ALLOW IGNITORS TOFIRE EARLIER IN THE ENGINE START SEQUENCE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SN60WRMAP3 SOLDER, M81969/14-02, M81969/14-03, M21097/18-01 TOOL, M22520/5-103DIE, M22520/1-02 RED POSITIONER, M22520/5-01, M22520/1-01, 90083, 90005, 47386 CRIMPTOOLS, MIL-T-43435 NYLON TYING TAPE REQUIRED BUT NOT FURNISHED WITH KIT. THISKIT IS NOT COMPLETE UNTIL THE AIRCRAFT FLIGHT MANUAL AND PILOT’S OPERATINGMANUAL REVISIONS HAVE BEEN INCORPORATED. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.


128-3056-1ENGINE IGNITOR CIRCUIT IMPROVEMENT ATA : 74400 RJ-1 THRU RJ-65400A RK-1 THRU RK-44, RK-46 THRU RK-48

(WITHOUT FIELD INSTALLATION OF BURSTMODE IGNITION IGNITOR WIRING CHANGEKIT 128-3038 OR 128-3039)

"RECOMMENDED" SB NO. 74-3290THIS KIT PROVIDES PARTS AND INFORMATION TO REWIRE THE IGNITOR CIRCUIT TO ALLOW IGNITORS TOFIRE EARLIER IN THE ENGINE START SEQUENCE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SN60WRMAP3 SOLDER, M81969/14-02 INSERT/EXTRACTION TOOL, MS22520/5-103 DIE,M22520/1-02 RED POSITIONER, M22520/5-01, M22520/1-01, 47386 CRIMP TOOL, MIL-T-43435NYLON TYING TAPE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPROPRIATE AIRCRAFT FLIGHTMANUAL REVISION AND PILOT'S OPERATING MANUAL REVISION HAVE BEENINCORPORATED. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



KIT CATALOG

128-3056-3ENGINE IGNITOR CIRCUIT IMPROVEMENT ATA : 74400 RJ-1 THRU RJ-65400A RK-1 THRU RK-44, RK-46 THRU RK-48

(WITH FIELD INSTALLATION OF BURSTMODE IGNITION IGNITOR WIRING CHANGEKIT 128-3038 OR 128-3039)

"RECOMMENDED" SB NO. 74-3290THIS KIT PROVIDES PARTS AND INFORMATION TO REWIRE THE IGNITOR CIRCUIT TO ALLOW IGNITORS TOFIRE EARLIER IN THE ENGINE START SEQUENCE ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SN60WRMAP3 SOLDER, M81969/14-02 INSERT/EXTRACTION TOOL, MS22520/5-103 DIE,M22520/1-02 RED POSITIONER, M22520/5-01, M22520/1-01, 47386 CRIMP TOOL, MIL-T-43435NYLON TYING TAPE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPROPRIATE AIRCRAFT FLIGHTMANUAL REVISION AND PILOT'S OPERATING MANUAL REVISION HAVE BEENINCORPORATED. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.


128-3058-1THIS KIT PROVIDES PARTS & INFORMATION FOR COCKPIT SPEAKERSWITCHED DISCONNECT FOR IN-SERVICE AIRCRAFT.

ATA :

400A RK-1 THRU RK-295NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPLICABLE FAA APPROVED

AIRPLANE FLT. MANUAL REVISIONS (OR SUPPLEMENTS) HAVE BEEN INCORPORATED.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12-16MEN : 1 (MAN)

128-3059-1COCKPIT VOICE RECORDER ATA :THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 120 MINUTE VOICE RECORDER FOR IN-SERVICE AIRCRAFT.WT. CHANGE : WT. CHANGE: -12.5 MOMENT: -6,000 WHEN 93-A100-83 CVR IS REPLACED

WT. CHANGE: -4.00 MOMENT: -1,920 WHEN S100-0080-00 CVR IS REPLACEDEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-3062-1PLACARD ASSY, ENGINE FIRE EXTINGUISH ATA :MU-300,400,400A,400T(T-1A) & 400T(TX) A003 THRU A091, RJ-1 THRU RJ-65, RK-1

AND AFTER UP TO THE EFFECTIVITY OFECR13267, TT-1 THRU TT-180 & TX-1 THRUTX-12

THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE EXISTING 45A88861-3ENGINE FIRE EXTINGUISH PLACARD ATTACHED TO THE INSTRUMENT PANEL INDICATOR SHROUD ASSYWITH AN IMPROVED PLACARD ASSY ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309NA" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET


128-3063-1LIGHT ASSY, LED TAIL POSITION-INFO ONLY ATA :400 RJ-1 THRU RJ-65400A RK-1 & AFTER UP TO THE EFF OF

ECR13729400T (T-1A) TT-1 AND AFTER UP TO THE EFF OF

ECR13730400T (TX) TX-1 AND AFTER UP TO THE EFF OF

ECR13731.MU300 A003SA THRU A091SACOMMUNIQUE NO. 56THIS KIT PROVIDES INFORMATION ONLY TO INSTALL A LED TAIL POSITION LIGHT ASSEMBLY IN PLACE OFTHE EXISTING INCANDESCENT/HALOGEN TAIL POSITION LIGHT ASSEMBLIES ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-3065-0001TAIL DEICE SYSTEM SOLID STATE CONTACTOR ATA :400 RJ-1 THRU RJ-65400A, 400T (TX) RK-1 THRU ECR14113 WITH HORIZONTAL

TAIL DE-ICE SYSTEM INSTALLED BY RACPRODUCTION INSTALLATION OR BY FIELDINSTALLATIONS PER FIELD SERVICE KITS128-4014, 128-4016 OR 132-4004

COMMUNIQUE#65THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE ONE 128-384054-5 OR -7HORIZONTAL TAIL DE-ICE SYSTEM SOLID STATE CONTACTOR WITH A 128-380102-0001 SOLID STATECONTACTOR AND MODIFY AIRCRAFT WIRING. EACH AIRCRAFT UTILIZES FOUR SOLID STATE CONTACT

NOTENOTENOTENOTE:::: "M81969/14-11" INSERT/EXTRACT,"M22520/1-01" CRIMP TOOL, & "TH278" TURRETHEAD,"M22520/5-01" CRIMP TOOL & "M22520/5-103" DIE;"AA-52080-B-3" "MIL-T-43435" TYPEI,FIN B,SIZE 3 TAPE,TYING;"MS3367-4-9""MS3367-1-9" TIE STRAP REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANYOUTLET.



KIT CATALOG

128-3066-0001REMOTE OIL LEVEL SYSTEM, ENGINE ATA : 73400A RK-78, RK-87 THROUGH RK-392"O"S.B.73-3813THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN ENGINE REMOTE OIL LEVEL SYSTEM FORIN-SERVICE AIRCRAFT. THIS KIT INSTALLS THE REMOTE OIL LEVEL HARDWARE ON THE ENGINE (VIAPRATT & WHITNEY SB) AND MAKES MODIFICATION TO THE ENGINE AND L & R AFT FUSELAG

NOTENOTENOTENOTE:::: "MIL-T-43435" NYLON TYING TAPE, "M22520/1-01""M22520/5-01""91515-1" & "47386" CRIMPTOOL, "M81969/14-02" & "91002-1" INSERT/EXTRACTION TOOL REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANYOUTLET.

WT. CHANGE : +8.6 LB MOMENT: +2.995 LB-INEST. MAN/HRS: : 24 HRSMEN : 1 (MAN)

128-3068-0001GALLEY ELECTRICAL WIRING ATA : 25400A RK-98, RK-110 THRU RK-386, RK-389 THRU

RK-400 & RK-406"M"S.B.25-3758THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REWIRE LH (P/N 20917) & RH (P/N 20918)GALLEYS MANUFACTURED BY PRECISION PATTERN INC., WICHITA, KS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "69959" CRIMP TOOL, "59974-1" CRIMP TOOL, "48752-1" DIE, "MIL-T-43435" NYLON TYINGTAPE, & "SN60WRMAP3" SOLDER REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : FOR INITIAL GALLEY CABINET ASSY WIRING INSP:0.5 HR; PER GALLEY CABINET ASSY REWORK: 7 HRS.MEN : 1 (MAN)

128-3069-0001BATTERY FEEDER PROTECTION UNIT,INSTALLATION CHANGE ATA :400A RK-78, RK-87 THRU THE EFFECTIVITY OF

ECR14856COMMUNIQUE #80, MARCH '07THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INVERT THE BATTERY FEEDERPROTECTION UNIT INSTALLATION TO PROVENT MOISTURE INGRESS BETWEEN THE COVER AND THEBASE PLATE OF THE UNIT.



KIT CATALOG

128-3071-0001ELECTRICAL WIRING MODIFICATION, FLAP HYDRAULICSYSTEM-INFO ONLY

ATA :

400 RJ-1 THRU RJ-65400A RK-1 & AFTER UP TO THE EFFECTIVITY OF

ECR15567MU-300 A003 THRU A091“O”S.B.27-3805THIS KIT PROVIDES INFORMATION REQUIRED TO MODIFY THE ELECTRICAL WIRING TO THE FLAPHYDRAULIC SOLENOID VALVE PACKAGE. HYDRAULIC PRESSURE WILL BE CONTINUOUSLY APPLIED TOTHE FLAP ACTUATOR IN THE RETRACTED POSITION FOR IN-SERVICE AIRCRAFT.


128-3413-0001COLLINS TDR-94/94D MODE S ENHANCED SURVEILLANCE UPGRADE ATA : 34MODEL 400A RK-118, RK-140 THRU RK-353;MODEL 400A, HAWKER 400XP RK-354 THRU RK-417"O"S.B.34-3716THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE TDR-94/94D TRANSPONDERSAND THE IOC-4000 INPUT/OUTPUT CONCENTRATOR-IAPS CIRCUIT CARDS TO PROVIDE ENHANCEDSURVEILLANCE CAPABILITIES FOR 3-TUBE & 4-TUBE CONFIGURATIONS ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-T-43435""AA-52080-B-3" NYLON TYING TAPE, "MS3367-4-9 TIE DOWN STRAP(MINIATURE),"MS3367-1-9" TIE DOWN STRAP (STANDARD),"M83519/2-7""M83519/2-8"SHIELD TERMINATION, "M81714/17-A44" TERMINAL JUNCTION,"372-2514-110""M39029/1-507""M39029/57-354" CONTACT, & "D-436-43" SPLICE REQUIREDBUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT MAINTENANCEMANUAL AND CREW MANUAL HAVE BEEN INCORPORATED. MANUALS MAY BE OBTAINEDFROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

128-3415-0001HONEYWELL EGPWS SOFTWARE ENHANCEMENTS WITH OPTIONALRAAS UPGRADE

ATA : 34

400A RK-329 THRU RK-529 WITH FACTORYINSTALLED EGPWS AND 3-TUBECONFIGURATIONS

"O"S.B.#34-3834THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPDATE THE EXISTING EGPWSCOMPUTER SOFTWARE AND CONFIGURATION DATABASE TO -224-224 STATUS AND ADD ENHANCEMENTSFOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT ADDS "PEAKS" MODE AND ENHANCED NIGHT VISABILITY FOR VARIOUS EGPWSOVERRIDE/INHIBIT SWITCHES AND REQUIRES A WIRING CHANGE WITH ADDITIONALCOMPONENTS.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 11 HRS (2 MEN)MEN : 2 (MEN)


ATA : 34

400A RK-490 AND AFTER; MODEL 400A S/N:RK-490 THRU RK-529 REQUIREINSTALLATION OF -0001 KIT PRIOR TOINSTALLATION OF -0003 KIT

"O"S.B.#34-3834THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPDATE THE EXISTING FACTORYINSTALLED EGPWS SYSTEM (3-TUBE CONFIGURATION) TO ADD RUNWAY AWARENESS AND ADVISORYSYSTEM (RAAS) ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: INSTALLATION OF KIT -0003 REQUIRES ADDITIONAL COMPONENTS TO BE INSTALLEDAND WIRING CHANGES.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPROPRIATE AIRCRAFT FLIGHTMANUAL REVISION (OR SUPPLEMENT) HAS BEEN INCORPORATED. MANUAL REVISIONS(OR SUPPLEMENTS) MAY BE OBTAINED FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: "718-1597-001" RAAS ENABLE KEY CARD & "718-1597-506" RAAS CONFIG DATABASEREQUIRED BUT NOT SUPPLIED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : WT: +1.5 LB MOMENT: +76 LB-INEST. MAN/HRS: : 6 HRS (2 MEN)(IN ADDITION TO HOURS REQUIRED FOR KIT 128-3415-0001 INSTALLATION).MEN : 2 (MEN)


KIT CATALOG


ATA : 34

400A RK-329 THRU RK-489; INSTALLATION OF-0001 KIT IS REQUIRED PRIOR TOINSTALLATION OF -0005 KIT.

"O"S.B.#34-3834THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO UPDATE THE EXISTING FACTORYINSTALLED EGPWS SYSTEM (3-TUBE CONFIGURATION) TO ADD RUNWAY AWARENESS AND ADVISORYSYSTEM (RAAS) ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 718-1597-001" RAAS ENABLE KEY CARD & "718-1597-506" RAAS CONFIG DATABASEREQUIRED BUT NOT SUPPLIED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE APPROPRIATE AIRCRAFT FLIGHTMANUAL REVISION (OR SUPPLEMENT) HAS BEEN INCORPORATED. MANUAL REVISIONS(OR SUPPLEMENTS) MAY BE OBTAINED FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: INSTALLATION OF KIT -0005 REQUIRES ADDITIONAL MECHANICAL CHANGES,COMPONENTS TO BE INSTALLED AND WIRING CHANGES.

WT. CHANGE : WT: +1.5 LB MOMENT: +76 LB-INEST. MAN/HRS: : 23 HRS (2 MEN)(IN ADDITION TO HOURS REQUIRED FOR KIT 128-3415-0001 INSTALLATION).MEN : 2 (MEN)

128-4001-1 SINSULATION NOMEX BLANKETS ATA : 25400 AND DIAMOND II RJ-1 THRU RJ-65DIAMOND II RJ-1001 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ADDITIONAL WINDOW NOMEX BLANKETINSULATION FOR INCREASED CABIN COMFORT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 2 (MEN)

128-4002-1 SFUEL DECAL, EXTERIOR INFORMATION MARKING ATA : 28400 RJ-1 THRU RJ-65MU300-10 A1001SA THRU A1011SATHIS KIT PROVIDES THE PARTS AND INFORMATION NECESSARY TO INSTALL DECALS CONTAININGINFORMATION ABOUT APPROVED FUELS AT THE WING AND FUSELAGE FILLER PORTS ON INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)


KIT CATALOG

128-4004-1 SFUSELAGE STIFFENER INSTALLATION ATA :400A RK-2 THRU RK-14, RK-17 THRU RK-19THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIRCRAFT WITH FOUR TUBE FLIGHT DISPLAYSFOR CATEGORY II OPERATION.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8MEN : 1 (MAN)

128-4005-1 SPRECIPITATION STATIC ATA : 23400 RJ-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ELECTRICAL CONDUCTIVE PAINTAND NECESSARY BONDING STRAPS TO THE AIRCRAFT TO PREVENT PRECIPITATION STATIC BUILDUP ONINSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REF TO CHEM-FILM PER MIL-C-5541 MEANS THAT ANY CHEM-FILM THAT MEETS THIS MIL-SPEC PROCESS CAN BE USED; PART NUMBER: "ALODINE 1200" IS ONE OF MANY THATCOMPLY TO THE MIL-SPEC AND CAN BE PROCURED LOCALLY.

NOTENOTENOTENOTE:::: REF TO DESOTO 528-104 OR 528-306, DESOTO IF MANUFACTURE, PART NUMBER: 528-104CAN BE PROCURED LOCALLY.

NOTENOTENOTENOTE:::: THE -1 S KIT CONTAINS ALSO -3 S KIT WHICH IS FOR MODEL 400A SERIAL NUMBERS RK-1THRU RK-15 AND RK-17 THRU RK-19, SO YOUR 400 WILL HAVE LATEST 400APRECIPITATION BUILDUP.


128-4005-3 SPRECIPITATION STATIC ATA : 23400A RK-1 THRU RK-15, RK-17 THRU RK-19THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ELECTRICAL BONDING STRAPSTO THE OUTBOARD LANDING GEAR DOORS TO PREVENT PRECIPITATION STATIC BUILDUP.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 4MEN : 1 (MAN)

128-4006-7 SINSULATION MODIFICATION ATA :400A RK-2, RK-4 THRU RK-24THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL VINYL SOUND DAMPENERMATERIAL IN CABIN WINDOW AREAS ON INSERVICE AIRCRAFT. THIS KIT INCLUDES 128-4006-1 S AND -9 SKITS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10 TO 12MEN : 1 (MAN)


KIT CATALOG

128-4010-1 SSTRUCTURAL REINFORCEMENT ATA :400A RK-1 THRU RK-22THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REINFORCE STRINGER 45AS33251-57AFTER OF THE ESCAPE HATCH ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

128-4010-3 SSTRUCTURAL REINFORCEMENT ATA :400A RK-1 THRU RK-22THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REINFORCE STRINGER 45AS33251-55FORWARD OF THE ESCAPE HATCH ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)

128-4010-5 SSTRUCTURAL REINFORCEMENT ATA :400A RK-1 THRU RK-22THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE FLOORBOARD SUPPORT128-430072-7 ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 TO 12MEN : 1 (MAN)




KIT CATALOG

128-4014-1LEADING EDGE HORIZONTAL STABILIZER DEICE ATA : 30400A RK-20 THRU RK-48, EXCEPT RK-45THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HORIZONTAL STABILIZER LEADING EDGEDEICER SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CHEM-FILM MIL-S- 5002 AND MIL-C-5541 EQUIVALENT IS "ALODINE 1200". THE FOLLOWINGITEMS WILL BE REQUIRED FOR INSTALLATION OF KIT, BUT NOT FURNISHED. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "50-71OR QT" BLACKPAINT, "22-11274" CLEAR FL XXXXXXXXXXXXXXXXXXXXX


128-4014-3LEADING EDGE HORIZONTAL STABILIZER DEICE ATA : 30400A RK-45, RK-49 THRU RK-86, EXCEPT RK-78THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HORIZONTAL STABILIZER LEADING EDGEDEICER SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CHEM-FILM (MIL-S-5002 AND MIL-C-5541) EQUIVALENT IS "ALODINE 1200". IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED QUANTITY ITEMS ARE NOT FURNISHED WITH THIS KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "50-71OR QT"BLACK PAINT, "22-11274" CLEAR FLAT EPOXY PAINT, "EA9309 QT" SEALER, "PS30 PT"CEMENT AND "PRO SEAL 895" OR XXXXXXXXXXXXXXXXXXXXX

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 320MEN : 2 TO 4 (MEN)

128-4014-5LEADING EDGE HORIZONTAL STABILIZER DEICE ATA : 30400A RK-78, RK-87 THRU RK-107"PENDING" SB NO.2600THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HORIZONTAL STABILIZER LEADING EDGEDEICER SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR OTHER 400A SERIAL NUMBERS SEE 128-4014-1, -3 OR 128-4016-1 KITS AND FORSERIAL NUMBERS RJ-1 THRU RJ-65 SEE 128-4016-3 KIT.

NOTENOTENOTENOTE:::: THE FOLLOWING AS REQUIRED QUANTITY ITEMS ARE NOT FURNISHED WITH THIS KIT. IFNOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "50-71OR QT"BLACK PAINT, "22-11274" CLEAR FLAT EPOXY PAINT, "EA9309 QT" SEALER, "PS30 PT"CEMENT AND "PRO SEAL 895" OR XXXXXXXXXXXXXXXXXXX



KIT CATALOG

128-4016-1LEADING EDGE HORIZONTAL STABILIZER DEICE ATA : 30400A RK-1 THRU RK-19SB NO. 2600THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HORIZONTAL STABILIZER LEADING EDGEDEICER SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: FOR MODEL 400 SEE -3 KIT, FOR OTHER 400A'S SEE 128-4014 KITS OR 128-4015-1.NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR INSTALLATION OF KIT. IF NOT

AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "50-71OR QT" BLACKPAINT, "22-11274" CLEAR FLAT EPOXY PAINT, "EA9309 QT" SEALER, "PS30 PT" CEMENTAND "PRO SEAL 895" OR "895B1/2 QT XXXXXXXXXXXXXXXX


128-4016-3LEADING EDGE HORIZONTAL STABILIZER DEICE ATA : 30400 RJ-1 THRU RJ-65THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A HORIZONTAL STABILIZER LEADING EDGEDEICER SYSTEM ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THE FOLLOWING ITEMS WILL BE REQUIRED FOR INSTALLATION OF KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY: "50-71OR QT" BLACKPAINT, "22-11274" CLEAR FLAT EPOXY PAINT, "EA9309 QT" SEALER, "PS30 PT" CEMENTAND "PRO SEAL 895" OR "895B1/2 QT XXXXXXXXXXXXXXXXX


128-4024-1CONDENSER AIR INLET INSTALLATION ATA : 21400A RK-78, RK-87 THRU RK-109, EXCEPT RK-98THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL ADDITIONAL AIR SCOOPS ON THE AFTFUSELAGE SECTION OF AIRCRAFT TO ENHANCE THIS VAPOR CYCLE COOLING SYSTEM.WT. CHANGE : WT: + 1.5 LBS; MOMENT; + 694 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

128-4028-1ELT INSTALLATION ATA : 25400A RK-78, RK-87 THRU RK-109, EXCEPT RK-98THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN EMERGENCY LOCATOR TRANSMITTER ONINSERVICE AIRCRAFT.WT. CHANGE : WT: 5 LBS; MOMENT; 2176 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

128-4028-3ELT INSTALLATION ATA : 25400A RK-98, RK-110 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN EMERGENCY LOCATOR TRANSMITTER ONINSERVICE AIRCRAFT.WT. CHANGE : WT: 5 LBS; MOMENT; 2176 IN.-LBSEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

128-4031-1CLOSEOUT ASSEMBLY CABIN/COCKPIT ATA : 25400A RK-98, RK-110 THRU TK-140THIS KIT PROVIDES COMPONENTS AND INFORMATION TO MODIFY THE CLOSEOUT ASSEMBLY CABIN/COCKPIT TO IMPROVE COCKPIT VAPOR CYCLE SYSTEMS COOLING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-4031-3AFT WING SPAR FITTING, FATIGUE IMPROVEMENT ATA : 57400A RK-110 THRU RK-140THIS KIT PROVIDES COMPONENTS AND INFORMATION TO MODIFY THE CLOSEOUT ASSEMBLY CABIN/COCKPIT TO IMPROVE COCKPIT VAPOR CYCLE SYSTEMS COOLING.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-4035-1ENGINE CARRY THRU BRACKET INSTALLATION ATA :MU-300 A003 THRU A065COMMUNIQUE NO. 58 (ISSUED TO UPDATE COMMUNIQUE NO. 189)THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY MODEL MU-300 SERIES IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-4035-3ENGINE CARRY THRU BRACKET INSTALLATION ATA :MU-300 A066 & UPCOMMUNIQUE NO. 58 (ISSUED TO UPDATE COMMUNIQUE NO. 189)THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY MODEL MU-300 SERIES IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-4035-5ENGINE CARRY THRU BRACKET INSTALLATION ATA :400 RJ-1 & UP400A RK-1 & UP400T (T-1A) TX-1 & UP400T (TX) TT-1 & UPCOMMUNIQUE NO. 58 (ISSUED TO UPDATE COMMUNIQUE NO. 189)THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY IN-SERVICE AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-4038-0001BRACKET ATTACHMENT MODIFICATION, INSTL ATA :400, 400A & 400XPTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL 2 NUTPLATES AT ONE CABIN ENTRANCE AFTDOOR LATCH PIN LOCATION TO ALLOW STEP CABLE BRACKET TO BE REPLACED WITHOUT REMOVINGDOORLAND PANELS, L/H AFT WINDOW PANEL AND OVERHEAD CABIN PANEL ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-4039-0001BEARING ASSY-ENTRANCE DOOR HANDLE MOD INSTL ATA :400A RK-100 THRU RK-459400T (TT) TT-109 THRU TT-180400T (TX) TX-7 THRU TX-13THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLANGED BEARING ASSY IN CABIN DOORHANDLE ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MS20425AD5" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.


128-4600-1SUPPLEMENTAL INSULATION INSTALLATION ATA : 25400A RK-78, RK-87 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO ADD SUPPLEMENTAL INSULATION TO ELIMINATE HEATDAMAGE TO AREA SURROUNDING ELBOWS IN WING ANTI-ICE SYSTEM.

NOTENOTENOTENOTE:::: EC1357 ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOURSHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

128-5001-1 SLIGHT PANEL TREATMENT, INDIRECT LIGHTING ATA :400A RK-1 AND AFTER, THAT DO NOT HAVE A

LEFT-HAND FORWARD CABINET"OPTIONAL" SB NO. 2450THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW LIGHT PANEL TREATMENT FOR THECABIN INDIRECT LIGHTING FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT PANELS ARE UNUPHOLSTERED SO YOU WILL NEED TO ORDER 5 LY OF THEMATERIAL REQUIRED TO COVER 3 PANELS DUE TO THE LENGTH OF PANELS IN KIT. YOUALSO WILL NEED 1 QUART OF EC1781 QT CEMENT AND 1 QUART OF EC1300L QT YELLOWEDGE COATING ADHESIVE TO UPHOLSTER THE PANELS IN THE FIELD.

NOTENOTENOTENOTE:::: WILL ALSO REQUIRE 1 PINT OF EPOCAST 87269 WHICH IS AVAILABLE FROM FURANCEPLASTICS, INC., LOS ANGELES, CAL., IF YOU CAN NOT OBTAIN FROM YOUR LOCALPLASTICS MANUFACTURERS.


128-5001-3 SLIGHT PANEL TREATMENT, INDIRECT LIGHTING ATA :400A RK-1 AND AFTER THAT HAVE A LEFT-HAND

FORWARD CABINET INSTALLED"OPTIONAL" SB NO. 2450THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW LIGHT PANEL TREATMENT FOR THECABIN INDIRECT LIGHTING FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT PANELS ARE UNUPHOLSTERED SO YOU WILL HAVE TO ORDER 5 LY OF THEMATERIAL REQUIRED TO COVER 3 PANELS DUE TO THE LENGTH OF PANELS IN KIT. YOUALSO WILL NEED 1 QUART OF EC1781 QT CEMENT AND 1 QUART OF EC1300L QT YELLOWEDGE COATING ADHESIVE TO UPHOLSTER T XXXXXXXXXXXXXXXXXXXXXXXXX

NOTENOTENOTENOTE:::: WILL ALSO REQUIRE 1 PINT OF ECOCAST 87269 WHICH IS AVAILABLE FROM FURANCEPLASTICS, INC., LOS ANGELES, CAL. IF YOU CAN NOT LOCATE AT YOUR LOCAL PLASTICSMANUFACTURERS.

NOTENOTENOTENOTE:::: FOLLOWING RESTRICTED ARTICLES NOT FURNISHED WITH KIT, IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY UNDER PART NUMBER "LOCTITE 22250CC" BOTTLE NO.15-31 LOCTITE 222 AND "LOCQUIC PRIMER T" SPRAY CAN 6 OZ.,LOCTITE PRIMER TYPE T.

NOTENOTENOTENOTE:::: SERIAL NUMBERS SA1001 THRU SA1011 ARE MHI SERIAL NUMBERS FOR RAYTHEONSERIAL NUMBERS RJ-1 THRU RJ-11.


128-5002-1 SAIR DUCT MODIFICATION ATA :400A RK-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL NEW PANEL ASSEMBLY, GASKETAND ADAPTER TO PROVIDE CABIN FLOOD AIR FOR INSERVICE AIRCRAFT THAT HAVE AN UPPER VANITYINSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)


KIT CATALOG

128-5002-3 SAIR DUCT MODIFICATION ATA :400A RK-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL NEW PANEL ASSEMBLY, GASKETAND ADAPTER TO PROVIDE CABIN FLOOD AIR FOR INSERVICE AIRCRAFT THAT DO NOT HAVE AN UPPERVANITY INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 12 TO 16MEN : 1 (MAN)

128-5003-1 STHRUST REVERSE BEARING ATA : 78400 RJ-12 THRU RJ-65400A RK-1 THRU RK-43MU-300 A003 THRU A091MU-300-10 SA1001 THRU SA1011"MANDATORY" SB NO. 2462THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO IMPROVE THE RETENTION OF THE THRUSTREVERSER CAM ROLLERS IN THE ENGINE CONTROL PEDESTAL FOR AIRCRAFT HAVING THRUSTREVERSERS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

128-5004-1 SBLEED AIR ORIFICE ATA : 29400 RJ-15 THRU RJ-65400A RK-1 THRU RK-81THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A HYDRAULIC RESERVOIR BLEEDAIR PRESSURE LINE DRAIN ORIFICE AND INCREASED PRESSURE RELIEF VALVE FOR INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)

128-5005-1 SAIR FLOW OUTLET DEFLECTOR ATA :THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL NEW DEFLECTOR ASSEMBLIESTO PROVIDE FOR A MORE UNIFORM AIRFLOW FROM THE OUTLET DUCTS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6 TO 8MEN : 1 (MAN)


KIT CATALOG

128-5006-1 SGERMAN CERTIFICATION MODIFICATION ATA :400A RK-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY AIRCRAFT FOR GERMANCERTIFICATION, EFFECTIVE OPTIONAL ON RK-10 ONLY PER KIT DRAWING .

NOTENOTENOTENOTE:::: COLLINS COMPONENTS WILL HAVE TO BE OBTAINED FROM THE COLLIN'S EVH POOL TOCOMPLETE INSTALLATION OF THIS KIT AS PER KIT INSTRUCTIONS.

NOTENOTENOTENOTE:::: WILL REQUIRE P.O.M. SUPPLEMENT PART NUMBER 128-590001-159, NOT FURNISHEDWITH KIT, BUT REQUIRED FOR FLIGHT OF THE AIRCRAFT AFTER KIT IS INSTALLED.


128-5007-1 SSPEAKER, COCKPIT AND CABIN INSTALLATION ATA : 23400A RK-1 AND AFTERMU-300 003 S.A. THRU 091 S.A.THIS KIT IS THE SPARES REPLACEMENT FOR 45AS80006-11 SPEAKER ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 2MEN : 1 (MAN)

128-5008-1 SSPEAKER, CABIN INSTALLATION ATA : 23400 RJ-1 AND AFTER400A RK-1 AND AFTERTHIS KIT IS THE SPARES REPLACEMENT FOR D6200 AND D6300 SPEAKERS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

128-5009-1 SSTALL RECOGNITION MODIFICATION ATA :400A RK-1 THRU RK-23THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL PROVISIONS FOR STALL RECOGNITIONLIGHTS ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 3MEN : 1 (MAN)

128-5011-3 SOXYGEN PLUMBING MODIFICATION ATA : 35400A RK-2, RK-4 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF OXYGEN PLUMBING THAT ISCOMPATIBLE WITH 1.5|P' EYE BALL AIR DUCT INSTALLATION ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1 TO 2MEN : 1 (MAN)


KIT CATALOG

128-5014-1 SENVIRONMENTAL AIR VALVE REPLACEMENT ATA : 21MU-300THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF THE SPARES REPLACEMENT FORTHE 45A63019-003 ENVIRONMENTAL AIR VALVES ON INSERVICE AIRCRAFT WITH NEW DUKES VALVES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 TO 8MEN : 1 (MAN)

128-5014-3 SENVIRONMENTAL AIR VALVE REPLACEMENT ATA : 21400A RJ-1 AND AFTER400A RK-1 THRU RK-31THIS KIT PROVIDES PARTS AND INFORMATION FOR INSTALLATION OF THE SPARES REPLACEMENT FORTHE 45A63019-005 ENVIRONMENTAL AIR VALVES ON INSERVICE AIRCRAFT WITH NEW DUKES VALVES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 6MEN : 1 (MAN)

128-5015-1 SDISTRIBUTION AIR MODIFICATION, LOWER CABIN DUCT SLOT REWORK ATA : 21400A RK-1 THRU RK-15, RK-17 THRU RK-37THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY AIR DISTRIBUTION DUCTS FOR AN IMPROVEDPERFORMANCE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5 TO 3MEN : 1 (MAN)

128-5017-1 SCREW SEAT TRACKING MECHANISM ATA : 25400 RJ-1 THRU RJ-65400A RK-1 THRU RK-93MU-300 A003SA THRU A091SAMU-300-10 A1001SA THRU A1011SA"M"SB #25-2536 REV 2THIS KIT PROVIDES PARTS AND INFORMATION TO MAKE CREW SEAT TRACKING MECHANISM CHANGESFOR THE PILOT AND CO-PILOT.

SEATS FOR IN SERVICE AIRCRAFTNOTENOTENOTENOTE:::: FOR AN IMPROVED HANDLE ASSEMBLY WHICH WILL IMPROVE OVERALL CABLE LIFE OF

SYSTEM SEE 128-5017-3 KIT.NOTENOTENOTENOTE:::: TAKES ONE KIT PER AIRCRAFT.

WT. CHANGE : +1 LBS. MOMENT: +115 LBS-INEST. MAN/HRS: : 24 HRSMEN : 1 (MAN)


KIT CATALOG

128-5017-3CREW SEAT TRACKING MECHANISM IMROVEMENT INSTLN-KIT ATA : 25400 RJ-1 THRU RJ-65400A RK-1 THRU RK-93MU-300 A003SA THRU A091SAMU-300-10 A1001SA THRU A1011SATHIS KIT PROVIDES PARTS & INFORMATION TO MAKE CREW SEAT TRACKING MECHANISM CHANGES FORPILOT AND CO-PILOT SEATS FOR IN-SERVICE AIRCRAFT

NOTENOTENOTENOTE:::: THIS KIT FURNISHES AN IMPROVED HANDLE ASSEMBLY WHICH INCREASES THEOVERALL CABLE LIFE OF THE SYSTEM USED IN THE 128-5017-1 S IMPROVEMENT KIT.

WT. CHANGE : +1 MOMENT +115 LBS-INEST. MAN/HRS: : 24MEN : 1 (MAN)

128-5025-1 MTAKEOFF PERFORMANCE IMPROVEMENT MODIFICATION ATA : 27400A RK-45, RK-49 THRU RK-92THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY AIRCRAFT TO IMPROVE THETAKEOFF PERFORMANCE OF THE INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: AFM REVISION 128-590001-167 WILL BE REQUIRED FOR AIRCRAFT WITH 3 OR 4 TUBEDISPLAY SYSTEM AND 128-590001-169 FOR AIRCRAFT WITH 2 TUBE DISPLAY SYSTEM.YOU WILL HAVE TO CONTACT TECHNICAL PUBLICATIONS FOR REQUIRED M.F.D. CHECKLIST DISC FOR USAGE WITH INITIA XXXXXXXXXXXX

NOTENOTENOTENOTE:::: FOR EARLIER SERIAL NUMBERS SEE 128-5025-3 M KIT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50 TO 70MEN : 2 (MEN)

128-5025-3 MTAKEOFF PERFORMANCE IMPROVEMENT MODIFICATION ATA : 27400A RK-24 THRU RK-44, RK-46 THRU RK-48400A RK-1 THRU RK-23 WITH LANDING WT.

INCREASE MOD KIT 128-8001-1 INSTALLED.THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY AIRCRAFT TO IMPROVE THETAKEOFF PERFORMANCE OF THE INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT CONSIST OF PANELS, SWITCH ASSEMBLIES, WIRE ASSEMBLIES AND A FLAPSEAL ASSEMBLY.

NOTENOTENOTENOTE:::: AFM REVISION 128-590001-167 FOR 3 OR 4 DISPLAY TUBE AIRCRAFT AND -169 FOR 2TUBE AIRCRAFT PLUS APPROPRIATE MFD CHECK LIST DISC WILL BE REQUIRED AFTERKIT INSTALLATION. MUST ORDER SEPARATELY AND CONTACT TECHNICALPUBLICATIONS FOR DISC.

NOTENOTENOTENOTE:::: KIT 128-8001-1 CAN BE INSTALLED IN CONJUNCTION WITH THIS KIT IN ORDER TOACCOMPLISH THIS INSTALLATION ON RK-1 THRU RK-23.



KIT CATALOG

128-5026-1REFRIGERATION UNIT CONTROL SYSTEM INSTALLATION - UPGRADE ATA : 21400 RJ-1 TO RJ-50, RJ-52 THRU RJ-65400A RK-1 THRU RK-104MU300 066 THRU 091MU300 003 THRU 065 (WITH THE "OPTIONAL" 2

ZONE TEMPERATURE CONTROL SYSTEM)MU300 003 THRU 065 (WITH ONE ZONE

TEMPERATURE CONTROL SYSTEM SEE128-50026-3 KIT)

THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO UPGRADE THE REFRIGERATION UNITTEMPERATURE CONTROL SYSTEM ON THE INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MU300 SERIAL NUMBERS 003 THRU 065 WITH 1 ZONE TEMP CONTROL SYSTEM SEE128-5026-3 KIT.

NOTENOTENOTENOTE:::: WILL REQUIRE 128-5026-5, -7 OR -9 KIT WITH -1 KIT DEPENDING ON AIRCRAFT SERIALNUMBER.

NOTENOTENOTENOTE:::: TUBE "RT106" SEALER AND DOW CORNING CORP. "CD44" GREASE 5.3 OZ TUBE WILL BEREQUIRED TO INSTALL KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.

WT. CHANGE : TO BE DETERMINEDEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5026-3REFRIGERATION UNIT CONTROL SYSTEM INSTALLATION - 1 ZONE TEMPCONTROL

ATA : 21

MU300 003 THRU 065 WITH SINGLE ZONE TEMPCONTROL SYSTEM

THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO UPGRADE THE REFRIGERATION UNITTEMPERATURE CONTROL SYSTEM ON THE INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: TUBE "RT106" SEALER AND DOW CORNING CORP. "CD44" GREASE 5.3 OZ TUBE WILL BEREQUIRED TO INSTALL KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CANPROCURE LOCALLY.

NOTENOTENOTENOTE:::: FOR TWO ZONE TEMPERATURE CONTROL SYSTEM AIRCRAFT SEE 128-5026-1 KIT.NOTENOTENOTENOTE:::: WILL REQUIRE -7 FOR USE WITH THIS KIT TO COMPLETE INSTALLATION ON AIRCRAFT.NOTENOTENOTENOTE:::: YOU WILL HAVE TO LOCAL MANUFACTURE 1 EACH OF 128-555140-1 AND 128-555141-1

TUBE ASSEMBLY PER KIT DRAWING INSTRUCTIONS OR ORDER TUBES AS SEPARATEITEMS, AS THEY ARE NOT PART OF THE KIT.

WT. CHANGE : TO BE DETERMINEDEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-5026-5REFRIGERATION MOISTURE DRAIN REMOVAL AND ECU MOD ATA : 21400A RK-1, RK-6 THRU RK-104THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE MOISTURE DRAIN PLUMBING LINESFROM THE "ECU" PACK AND MODIFIES THE ECU MOISTURE DRAIN PAN OVERBOARD PLUMBING LINE ININSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT IS TO BE USED IN CONJUNCTION WITH THE 128-5026-1 KIT INSTALLATION,XXXXXXXXXXXXXXXXXX

NOTENOTENOTENOTE:::: RTV106 SEALANT WILL BE REQUIRED FOR USE BUT IS NOT PART OF THE KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, PROCURE LOCALLY.


128-5026-7REFRIGERATION ELECTRICAL SYSTEM COMPONENT MOD ATA : 21400 RJ-1 THRU RJ-50, RJ-52, THRU RJ-65400A RK-1 THRU RK-44, RK-46, THRU RK-48.MU300 003 THRU 091THIS KIT PROVIDES PARTS AND INFORMATION TO ADD THE ELECTRICAL SYSTEM COMPONENTSREQUIRED FOR KITS 128-5026-1 AND/OR 128-5026-3 ASSOCIATED WITH INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SOME RK SERIES AIRCRAFT WILL REQUIRE BOTH -5 AND -7 KITS FOR USE WITH128-5026-1 KIT.


128-5026-9REFRIGERATION ELECTRICAL SYSTEM COMPONENT MOD ATA : 21400A RK-45, RK-49 THRU RK-104THIS KIT PROVIDES PARTS AND INFORMATION TO ADD THE ELECTRICAL SYSTEM COMPONENTSREQUIRED FOR THE 128-5026-1 KIT ON THE INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SOME AIRCRAFT WILL REQUIRE BOTH A -7 AND -9 KIT TO INSTALL THE 128-5026-1 KIT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5027-1GUST LOCK INSTALLATION - CONTROL COLUMN OPTION ATA : 10400 RJ-1 THRU RJ-65400A RK-1 THRU RK-109MU300 003 THRU 092MC 44THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL PROVISIONS FOR -51 GUST LOCKASSEMBLY ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-5028-1TEMPERATURE CONTROL VALVE INSTALLATION - ENVIRONMENTALSYSTEM - SPARES

ATA : 21

400 RJ-1 THRU RJ-65400A RK-1 AND AFTERMU300THIS KIT PROVIDES PARTS AND INFORMATION TO FURNISH A REPLACEMENT TO UPGRADE THE COCKPITTEMPERATURE CONTROL VALVE PART NUMBER: 979580-5 OR 45AS63018-079 LOCATED ON THEAIRCYCLE MACHINE ON INSERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5028-3TEMPERATURE CONTROL VALVE - CABIN, REPLACEMENT ATA : 21400 RJ-1 THRU RJ-65400A RK-1 AND AFTERMU300THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE 979558-3 CABIN TEMP OR 45AS63018-181CABIN TEMP CONTROL VALVE WITH A NEW 100% INCONNEL CABIN TEMP CONTROL UNIT OF ALLIEDSIGNAL FOR OVERALL IMPROVEMENT OF THE AIR CYCLE UNIT USAGE LIFE.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5029-1LOW LIMIT TEMPERATURE CONTROL VALVE INSTALLATION,ENVIRONMENTAL - SPARES

ATA : 21

400 RJ-1 THRU RJ-65400A RK-1 AND AFTERMU-300 003 THRU 092THIS KIT PROVIDES PARTS AND INFORMATION TO UP GRADE THE ENVIRONMENTAL SYSTEM LOW LIMITTEMPERATURE CONTROL VALVE ON INSERVICE AIRCRAFT.WT. CHANGE : TO BE DETERMINEDEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5033-1NITROGEN GAUGE, FORWARD FUSELAGE INSTALLATION ATA : 32400 RJ-1 THRU RJ-65400A RK-1 AND AFTERMU300 003 THRU 092"OPTIONAL" SB NO. 2628THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL PROVISIONS FOR -3 NITROGENGAUGE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-5034-1OXYGEN GAUGE, FORWARD FUSELAGE ATA : 35400 RJ-1 THRU RJ-65400A RK-1 THRU RK-155MU300 A003SA THRU A091SATHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL PROVISIONS FOR 45AS95002-7OXYGEN GAUGE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5037-1AIR CONDITIONING EVAPORATOR CONDENSATION DRAININSTALLATION

ATA : 21

400A RK-78, RK-87, THRU RK-97, RK-99 THRURK-109

SB NO. 2667THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A SEPARATE DRAIN INSTALLATION FOR THEFORWARD AND AFT EVAPORATORS OF THE VAPOR CYCLE AIR CONDITIONING SYSTEM, WHICH WEREINSTALLED AS AN OPTIONAL INSTALLATION ON THE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 HRS.MEN : 1 (MAN)

128-5039-1RELOCATION OF GALLEY DRAIN ATA : 25400A RK-98, RK-110 THRU RK-134THIS KIT PROVIDES PARTS AND INFORMATION TO IMPROVE THE GALLEY DRAIN PROVISION WHEN THEAIRCRAFT IS UNPRESSURIZED ON THE RAMP FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MIL-S-8802 SEALANT NOT FURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOPSTOCK, YOU CAN PROCURE LOCALLY.


128-5040-1INTERIOR IMPROVEMENTS ATA : 21400A RK-98, RK-110 THRU RK-123, RK-125 THRU

RK-129, RK-131 THRU RK-133THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO SECURE THE AIR RETURN LOUVERS WITHSCREWS.

NOTENOTENOTENOTE:::: 3708 FLAT BLACK URETHANE, 3549 ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG


RK-129, RK-131 THRU RK-133THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO SECURE THE WIRES FOR THE INDIRECTLIGHTING WITH CLIPS.

NOTENOTENOTENOTE:::: TAK PAK 7452 ACCELERATOR AND LOCTITE 454 ADHESIVE REQUIRED BUT NOTFURNISHED WITH KIT. IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURELOCALLY.



RK-129, RK-131 THRU RK-133THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO SECURE THE SHOULDER HARNESSPLACARD AND INHIBIT TWISTING OF THE SHOULDER HARNESS STRAP (CABIN SEATS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


RK-129, RK-131 THRU RK-133THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO SECURE THE SEAT BACK COVER TO THESEAT FRAME USING SCREWS AND NUTPLATES (CABIN SEATS).WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5043-1VENT COOLER-400A ATA : 21400A RK-98 THRU RK-226 AND RK-228 THRU

RK-247"RECOMENDED" SB NO. 21-3289THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO INSTALL AN AIR MIXER (128-540150-1) THAT WILLREDUCE MAX TEMP OF FLOOR VENT OUTLET IN THE VANITY ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)


KIT CATALOG

128-5044-1CABIN TEMP SENSOR RELOCATION ATA : 21400A RK-149 THRU RK-224"RECOMMENDED" SB NO. 21-3283THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE CABIN WINDOW DRY AIR SYSTEM FORIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 90277-1, 47386-2, M22520/5-01, M22520/1-01 HAND CRIMP TOOL, M22520/5-100,M22520/5-103 CRIMP INSERT DIE, MS20995C32 LOCK WIRE, MS3367-4-9 TIEDOWN STRAP,M222520/1-02 RED POSITIONER, M81969/14-03 INSERT/EXT TOOL, MIL-T-43435 TYING TAPEREQUIRED BUT NOT FUR XXXXXXXXXXXXXXXXXXXXXX


128-5044-3WINDOW DRY AIR SYSTEM REMOVAL ATA : 21400A RK-149 THRU RK-256THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE CABIN WINDOW DRY AIR SYSTEM FORINSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5045-1AFT EVAPORATOR DRAIN IMPROVEMENT ATA : 21400A RK-98, RK-110 THRU RK-102, RK-194 THRU

RK-202"RECOMMENDED" SB NO. 21-3258THIS KIT PROVIDES PARTS AND INFORMATION TO RECONFIGURE THE AFT EVAPORATOR CONDENSATEDRAIN FOR IMPROVED DRAINAGE ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4MEN : 1 (MAN)

128-5046-1AIRCRAFT OWNERSHIP PLATES - INFORMATION ONLY ATA : 11400A RK-1 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY REQUIRED TO INSTALL, REPLACE, AND/OR REMOVEOWNERSHIP PLACARDS ON LEASED OR FINANCED IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MS9914-06","MS9914-07" OR "AN3-3" BOLTS, "3012674" NUT, "MS9320-09" OR"NAS1149G0363P" WASHER, "CCR274SS3-02" RIVET, "132626-1A" & "132626-5A" PLACARDSREQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM RAPID ORYOUR LOCAL SUPPLIER



KIT CATALOG

128-5046-3AIRCRAFT OWNERSHIP PLATES - INFORMATION ONLY ATA : 11400A RK-1 AND AFTERTHIS KIT PROVIDES INFORMATION ONLY REQUIRED TO INSTALL, REPLACE AND/OR REMOVE OWNERSHIPPLACARDS ON MORTGAGED AIRCRAFT.

NOTENOTENOTENOTE:::: "MS9914-06","MS9914-07" OR "AN3-3" BOLTS, "3012674" NUT, "MS9320-09" OR"NAS1149G0363P" WASHER, "CCR274SS3-02" RIVET, "132626-3A" AND "132626-7A"PLACARDS REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROMRAPID OR YOUR LOCAL SUPPLIER.


128-5047-1CREW SEAT TRACKING MECHANISM ATA : 25400 RJ-1 THRU RJ-65400A RK-1 THRU RK-93MU-300 A003SA THRU A-091SAMU-300-10 A1001SA THRU A1011SA"M" SB #25-2536 REV 2THIS KIT PROVIDES PARTS AND INFORMATION TO MAKE CREW SEAT TRACKING MECHANISM CHANGESFOR PILOT AND CO-PILOT SEATS FOR IN-SERVICE AIRCRAFT.WT. CHANGE : +1 LBSMOMENT: +115 LBS-INEST. MAN/HRS: : 24MEN : 1 (MAN)

128-5047-3CREW SEAT TRACKING MECHANISM ATA : 25400 RJ-1 THRU RJ-65400A RK-1 THRU RK-93MU-300 A003SA THRU A-091SAMU-300-10 A1001SA THRU A1011SA"MANDATORY" SB NO. 25-2536, REV 2THIS KIT PROVIDES PARTS AND INFORMATION TO MAKE CREW SEAT TRACKING MECHANISM CHANGESFOR PILOT AND CO-PILOT SEATS FOR IN-SERVICE AIRCRAFT.WT. CHANGE : WT. +1 LBSMOMENT: +115 LBS-INEST. MAN/HRS: : 24MEN : 1 (MAN)

128-5051-1ANTI-ICE INSULATION CHANGE-INFO ONLY ATA :MU-300, 400, AND 400A THROUGH RK-441COMMUNIQUÉ 77THIS KIT PROVIDES INFORMATION TO CUT AND RESHAPE THE INSULATION BAGS USED IN THEIMMEDIATE AREA OF THE BLEED AIR DUCTING FOR THE LEADING EDGE ANTI-ICE SYSTEM FOR ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-5051-2ANTI-ICE INSULATION CHANGE-INFO ONLY ATA :400A RK-166 THRU RK-452, RK-455 & RK-458THIS KIT PROVIDES INFORMATION TO REPLACE THE DUCTING INSULATION FOR THE ANTI-ICE BLEED AIRDUCTING. THE MATERIAL CHANGE IS FROM FIBERFAX 970-J TO CLAREMAT 1200. FOR IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5051-5ANTI-ICE INSULATION CHANGE - INFO ONLY ATA :400A RK-440 THRU RK-452, RK-455 & RK-458COMMUNIQUÉ 77

THIS KIT PROVIDES INFORMATION FOR REPLACEMENT OF THE DUCTING INSULATION FOR THE CABINAND COCKPIT ENVIRONMENTAL HEAT AND THE REMOVAL OF SELF ADHESIVE TAPE FOR IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5052-1INCREASED GROSS TAKEOFF WEIGHT/200 POUNDS ATA :

RK-1 THRU RK-23 MODIFIED BY KIT128-8001 & 128-5025-3RK-24 THRU RK-92 MODIFIED BY KIT128-5025-1 OR 128-5025-3RK-93 & AFTER

RK-1 THRU RK-23 MODIFIED BY KIT 128-8001 & 128-5025-3. RK-24 THRU RK-92 MODIFIED BY KIT 128-5025-1OR 128-5025-3. RK-93 & AFTERKIT CONSISTS OF DWG 128-5052, AFM SUPPLEMENT 128-590001-269, POM SUPPLEMENT 128-590001-273AND PCL 128-590001-289.

NOTENOTENOTENOTE:::: ***SOLD THROUGH TMDC - 1-800-796-2665 OR 316-676-8238 OR [email protected]

MEN : N/A

128-5059-0001EVAPORATOR DRAIN ATA : 21400A RK-98, RK-110 THRU ECR 16046"O"S.B. 21-3844

THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY EXISTING FORWARD AIR CONDITIONINGEVAPORATOR MODULE AND DRAIN FOR IMPROVED DRAIN CAPABILITY FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "1134310" EVAPORATOR ASSY REQUIRED BUT NOT FURNISHED WITH KIT. PROCUREFROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

128-5059-0003EVAPORATOR DRAIN ATA : 21

400A RK-98, RK-110 THRU ECR 16046"O"S.B. 21-3844THIS KIT PROVIDES PARTS AND INFORMATION TO MODIFY EXISTING AFT AIR CONDITIONINGEVAPORATOR MODULE AND DRAIN FOR IMPROVED DRAIN CAPABILITY FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "1134310" EVAPORATOR ASSY REQUIRED BY NOT FURNISHED WITH KIT. PROCUREFROM ANY COMPANY AUTHORIZED OUTLET.


128-5060-1PLUG ARM REST HEAT-INFO ONLY ATA :

400A RK-110 AND AFTERMODEL COMMUNIQUE 81THIS KIT PROVIDES INFORMATION TO PLUG THE HEAT DUCT FOR THE LEFT AND RIGHT HAND ARM RESTJUST AFT OF THE ENTRANCE DOOR AND THE EMERGENCY EXIT DOOR.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5303-0001128-5303-0001 ATA :400A RK-98, RK-110 & AFTER UP TO THE EFF OF

ECR15170INSTL LOUVER AFT-HEADLINER-INFO ONLYTHIS KIT PROVIDES INFORMATION TO INSTALL THE 128-380107-0001 LOUVER IN PLACE OF THE EXISTINGAFT CABIN HEADLINER LOUVER 128-380089-1 ON IN-SERVICE AIRCRAFT.


128-5305-0001CLEAN FLUSH TOILET INSTALLATION ATA : 25400A RK-98, RK-110 THRU RK-542“O” S.B. 25-3852THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL AN UPGRADED CLEAN FLUSHTOILET FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "URALANE 5774-A/C" & "ATR-525 A/B" ADHESIVE REQUIRED, BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : WT. -1.0 LBS MOMENT: -309.0 LB-INEST. MAN/HRS: : 5 HRSMEN : 1 (MAN)


KIT CATALOG

128-5306-0001CLOSET/GALLEY FINISH PROTECTION ATA :400A RK-98, RK-110 THRU RK-548THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A DOOR STAY ON THE UPPERLIQUOR CABINET DOOR AND A PREPCO GUIDE ON SELECT PRECISION PATTERN 20918 CLOSET/GALLEYCABINETS. THESE ADDITIONS WILL PROTECT THE FINISH ON CABINETS.

NOTENOTENOTENOTE:::: VERIFY CUSTOMER HAS OPTIONS NOTED ABOVE ON AIRCRAFT CLOSET GALLEY.INSTALLATION OF THE CABINET IS OPTIONAL AND DRIVEN BY CUSTOMERSPECIFICATION UPON DELIVERY OF AIRCRAFT.

MEN : N/A

128-5306-0003CLOSET/GALLEY FINISH PROTECTION ATA :400A RK-98, RK-110 THRU RK-548THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A DOOR STAY ON THE UPPERLIQUOR CABINET DOOR ON SELECT PRECISION PATTERN 20918 CLOSET/GALLEY CABINETS. THISADDITION WILL PROTECT THE FINISH ON CABINETS.

NOTENOTENOTENOTE:::: VERIFY CUSTOMER HAS OPTION NOTED ABOVE ON AIRCRAFT CLOSET GALLEY.INSTALLATION OF THIS CABINET IS OPTIONAL AND DRIVEN BY CUSTOMERSPECIFICATION UPON INITIAL DELIVERY OF AIRCRAFT.

MEN : N/A

128-5311-1CRASH AXE INSTALLATION (JAP-OPS) ATA :400A RK-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION FOR THE ADDITION OF A CRASH AXE WITH COVER TO THEFWD RIGHT HAND PARTITION, FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "242" LOCTITE & "EA9394" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : CHANGE: 2.86 LB MOMENT: 390.2 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5313-1INSTL IMPROVEMENT, HEADLINER-INFO ONLY ATA :400A RK-98, RK-110 AND AFTER.THIS KIT PROVIDES INFORMATION ONLY TO PROVIDE ADDITIONAL FASTENING FOR OUTBOARD ENDS OFCABIN HEADLINER ON IN-SERVICE AIRCRAFT.WT. CHANGE : 1.5 LBS MOMENT: TBDEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-5314-0001INTERIOR MARKING INSTL, PORTUGUESE CERT ATA :400XP RK-393 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL INTERIOR PLACARDS ON IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

128-5316-0001PORTUGUESE PLACARD INSTL-EMERGENCY EXIT HANDLE, EXIT SIGN ATA :MODEL 400A RK-98, RK-110 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL REPLACEMENT EMERGENCY EXIT PLACARDSWITH PORTUGUESE TRANSLATION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EPON828" ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


128-5316-0007PORTUGUESE PLACARD INSTL-EMERGENCY EXIT HANDLE, EXIT SIGN ATA :

400A RK-98, RK-110 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL REPLACEMENT EMERGENCY EXIT

NOTENOTENOTENOTE:::: EPON 828" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


128-5400-1 SPRESSURIZATION AIR DEFLECTOR MODIFICATION ATA :400A RK-1 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A PRESSURIZATION AIR DEFLECTOR IN THEAFT COMPARTMENT OVERHEAD FOR INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 TO 4MEN : 1 (MAN)

128-5402-1 SPRESSURIZATION CONTROL - SPARES ATA :400 RJ-1 THRU RJ-65MU300 A003 THRU A092THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE PRESSURIZATIONCONTROL VALVES S2 & S3 FOR INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: MS20995C32 LOCKWIRE REQUIRED BUT NOT FURNISHED WITH KIT. IF NOT AVAILABLE INYOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.



KIT CATALOG

128-5402-3 SPRESSURIZATION CONTROL - SPARES ATA :400A RK-1 THRU RK-44, RK-46, RK-47 AND RK-48THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE PRESSURIZATIONCONTROL VALVES S2 & S3 FOR INSERVICE AIRCRAFT.



128-5402-5 SPRESSURIZATION CONTROL - SPARES ATA :400A RK-45, RK-49 THRU RK-174400T (T-1A) TT-1 THRU TT-180400T (TX) TX-1 THROUGYH TX-9THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REPLACE THE PRESSURIZATIONCONTROL VALVES S2 & S3 FOR INSERVICE AIRCRAFT.



128-5403-1VENT COOLER ATA :400A S/N: RK-1 THRU RK-97 AND RK-99 THRU

RK-109THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO INSTALL AN AIR DILUTION SYSTEM THAT WILLREDUCE MAX TEMP OF FLOOR VENT OUTLET IN THE VANITY. KIT IS FOR MODEL 400A EQUIPPED WITH128-530129 VANITY INSTL ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 1 (MAN)

128-5405-1WINDSHIELD WIPER REMOVAL-INFO ONLY ATA :400 RJ-1 THRU RJ-65400A RK-1 THRU RK-242MU300 A003SA THRU A065SA, A067SA & A068SA

MODIFIED BY SERVICERECOMMENDATION SR 71-001 AND A066SA& A069SA THRU A091SA.

THIS KIT PROVIDES INFORMATION ONLY TO REMOVE THE WINDSHIELD WIPERS AND WIPER MOTORSFROM AIRCRAFT WITH WINDSHIELDS THAT HAVE BEEN TREATED WITH SURFACE SEAL ON IN-SERVICEAIRCRAFT.WT. CHANGE : -14.4 LBS. MOMENT: -1048 IN-LBSEST. MAN/HRS: : 40-50 HRSMEN : 1 (MAN)


KIT CATALOG

128-5405-3WINDSHIELD WIPER REMOVAL-INFO ONLY ATA :400 RJ-1 THRU RJ-65400A RK-1 THRU RK-242MU300 A003SA THRU A065SA, A067SA & A068SA

MODIFIED BY SERVICERECOMMENDATION SR 71-001 AND A066SA& A069SA THRU A091SA.

THIS KIT PROVIDES INFORMATION ONLY TO REMOVE THE WINDSHIELD WIPERS FROM AIRCRAFT WITHWINDSHIELDS THAT HAVE BEEN TREATED WITH SURFACE SEAL ON IN-SERVICE AIRCRAFT.WT. CHANGE : -2.9 LBS, MOMENT: -256.9 IN-LBSEST. MAN/HRS: : 25-30MEN : N/A

128-5406-1NITROGEN GUAGE INSTALLATION ATA :WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

128-5407-0001PNEUMATIC RELAY BRACKET ATA :400A RK-1 THRU RK-529"O" S.B. 21-3828THIS KIT INSTALLS A REDESIGNED BRACKET THAT SUPPORTS THE AIR RELAY.


128-5407-0003PNEUMATIC RELAY BRACKET ATA :400A RK-1 THRU RK-529"O" S.B. 21-3828THIS KIT REPLACES THE 131823E6 PLASTIC TUBE WITH 128-380022 RUBBER HOSE


128-5600-1OXYGEN SERVICE DOOR, INSTL ATA :400A S/N RK-156 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL OXYGEN SERVICE DOOR IN NOSECOMPARTMENT ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 3950" EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

128-6000-0001JEPPESEN HOLDER ASSY W/PROTECTIVE BREATHING EQUIP ATA :

400A RK-98, RK-110 AND AFTER. 410+ AIRCRAFTAFFECTED

COMMUNIQUE 81THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE THE EXISTING 20925-1 HOLDERASSEMBLY WITH 20925-7 HOLDER ASSEMBLY WHICH WILL ALLOW FOR INSTALLATION OF 802300-14PROTECTIVE BREATHING EQUIPMENT ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "802300-14" BREATHING DEVICE, EMERGENCY ESCAPE REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +5.8 LB. MOMENT: +771 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-6001-0001SCREW REPLACEMENT TABLE INSTL, CABIN ATA :400A RK-98, RK-110 THRU RK-421THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO REPLACE EXISTING AN525-10R14PROTRUDING HEAD SCREW WITH MS24694-S53 COUNTERSUNK HEAD SCREW ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-6002-0001FLASHLIGHT INSTL, COCKPIT, COPILOT ATA :

400A RK-308 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A FLASHLIGHT IN THE COCKPIT FOR COPILOTUSE FOR IN-SERVICE AIRCRAFT.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : MAN/HRS: CONTACT PRODUCT SUPPORTMEN : N/A

128-8001-1 SLANDING WEIGHT INCREASE MODIFICATION ATA : 32400A RK-1 THRU RK-23THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LANDING GEAR PARTS, WHEELS, BRAKES,ANTI-SKID COMPONENTS, AND STRUCTURE REQUIRED TO RAISE THE MAXIMUM LANDING WEIGHT TO15,700 LBS. ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: ALODINE 1200 AND EA9309 QT REQUIRED, NOT FURNISHED WITH KIT.NOTENOTENOTENOTE:::: FLIGHT MANUAL SUPPLEMENT 128-590001-107 OR -109 ARE NOT FURNISHED WITH THIS

KIT. YOU NEED TO DETERMINE WHICH IS APPLICABLE TO YOUR AIRCRAFT ANDCONTACT TECHNICAL PUBLICATIONS AND ADVISE SERIAL NUMBER OF KIT INSTALLED,DATE SHIPPED, AND THAT YOU NOW REQUIRE XXXXXXXXXXXXXXXXX

WT. CHANGE : WT: 22 LBS @ 290.91EST. MAN/HRS: : 350 TO 360 INCLUDING AVIONICSMEN : 1 (MAN)


KIT CATALOG

128-8002-1 SEMERGENCY GEAR DOOR HANDLE REPOSITION ATA :400A RK-49, RK-50, RK-51, RK-53THIS KIT PROVIDES PARTS AND DATA REQUIRED TO REPOSITION THE EMERGENCY GEAR DOWNHANDLE TO FURNISH MORE CLEARANCE TO THE PILOT'S LEGS AND KNEES ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 TO 3MEN : 1 (MAN)

128-8003-1 SDUAL RATE SPEED BRAKE MANIFOLD, HYDRAULIC SYSTEMINSTALLATION

ATA : 27

400A RK-2 THRU RK-44, RK-46 THRU RK-48THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO BE INSTALLED FOR INSERVICE AIRCRAFTTO CONVERT FROM SINGLE RATE SPEED BRAKE TO DUAL RATE SPEED BRAKE SYSTEM.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 20 TO 24MEN : 1 (MAN)

128-8010-0001LANDING GEAR PLACARD MOD-INFO ONLY ATA :

400A RK-1 THRU RK-23 WITH KIT 128-8001INSTALLED, RK-24 THRU ECR 16069. 517+AIRCRAFT

THIS KIT PROVIDES INFORMATION FOR MODIFICATION OF MAIN AND NOSE LANDING GEAR STRUTSERVICING PLACARDS TO REMOVE UNNECCESSARY INFORMATION ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

128-9001-1 SENGINE OIL BREATHER DRAIN MODIFICATION ATA : 71400 RJ-1 THRU RJ-65400A RK-1 THRU RK-18"OPTIONAL" SB NO. 2401THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO REROUTE THE OIL BREATHER TUBEFROM THE ENGINE BY-PASS DUCT TO THE OVERBOARD FAIRLEAD ON ONE ENGINE ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: REQUIRES ONE KIT PER ENGINE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 HRS. PER ENGMEN : 1 (MAN)


KIT CATALOG

128-9004-1FLAPPER VALVE FLOAT VALVE INSTALLATION ATA : 28400A RK-1 THRU RK-90"RECOMMENDED" SB NO. 28-3237, MARCH, 2001THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE VENT VALVES IN THE CENTER SECTIONAND THE FLAPPER VALVES IN EACH WINGTIP SURGE TANK ON IN-SERVICE AIRCRAFT.


128-9004-3FLAPPER VALVE FLOAT VALVE INSTALLATION ATA : 28400A RK-91 THRU RK-217"RECOMMENDED" SB NO. 28-3237THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE VENT VALVES IN THE CENTER SECTIONFUEL TANKS ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 20MEN : 1 (MAN)

128-9004-3 SFLAPPER VALVE FLOAT VALVE REPLACEMENT INSTALLATION ATA : 28THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE VENT VALVES IN THE CENTER SECTIONAND THE FLAPPER VALVES IN EACH WING TIP SURGE TANK ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 18 TO 20MEN : 1 (MAN)

128-9007-0001ACCESS DOOR INSTL, REMOTE OIL CHECK ATA : 73400A RK-78 & RK-87 UP TO ECR14185"O"S.B.73-3813THIS KIT PROVIDES INFORMATION & PARTS TO ADD A REMOTE OIL ACCESS DOOR ON THE RIGHT ANDLEFT ENGINE NACELLE ON ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "3960" EDGE SEALER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY AUTHORIZED COMPANY OUTLET.



KIT CATALOG

128-9008-0001RAC MOD TO INSTL OIL TO FUEL ENG HEAT EXCHANGER ATA : 73400A RK-106 THRU RK-507"O"S.B.73-3813THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL AN OIL TO FUEL ENGINE HEATEXCHANGER, ENGINE CONVERSION FROM JT15D-5 TO JT15D-5R, FOR IN SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MS21266-1T""MS21266-1F""MS21266-3T" & "MS21266-3F" PLASTIC EDGING, "EC1357"CEMENT, "P/S 700" SEALANT, "EA934" ADHESIVE, "M22520/1-02" TURRET (REDPOSITIONER), "M22520/1-01""M22520/5-01" CRIMP TOOL, "M81969/14-02" INS/EXT TOOL,"M22520/5-103" DIE, "128-590001-205TC3""128-590001-149TC2" PILOTS OPERATINGMANUALS, "128-590001-167" AIRCRAFT FLIGHT MANUAL, & (SB)7605 P&WC SERVICEBULLETIN REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

WT. CHANGE : WITH ENGINE MODIFICATION: 133 HRS (2 MEN), WITH AIRPLANE MODIFICATIONS: 212 HRS (2 MEN)MEN : 2 (MEN)

128-9009-0001PROVISIONS FOR ELIMINATION OF ANTI-ICE INHIBITOR FUELADDITIVE

ATA : 73

400A RK-106 THRU RK-529"O'S.B.73-3813THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED FOR ELIMINATION OF THE REQUIREMENT OFFUEL SYSTEM ICE INHIBITOR FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: SHIPS S/N RK-106 THRU RK-507, KIT INSTALLATION 128-9008-0001, MODIFICATIONS TOINSTALL OIL TO FUEL ENGINE HEAT EXCHANGER, MUST BE COMPLETED CONCURRENTWITH OR PRIOR TO THIS KIT INSTALLATION.

NOTENOTENOTENOTE:::: THIS KIT INSTALLATION MAY BE INSTALLED WITH NO FURTHER MODIFICATIONS FORSHIP S/N RK-508 THRU RK-529.

NOTENOTENOTENOTE:::: PILOTS OPERATING MANUAL & AIRCRAFT FLIGHT MANUAL REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


128-9110-1HMU BLEED AIR IMPROVEMENT ATA : 73400 RJ-1 THROUGH RJ-65400A RK-1 THROUGH RK-90MU-300-10 A1001SA THROUGH A1011SA"RECOMMENDED" SB NO. 73-3354THIS KIT PROVIDES PARTS AND INFORMATION TO CHANGE FROM A PRATT AND WHITNEY MOISTURETRAP TO A RAYTHEON AIRCRAFT CONTINOUS MOISTURE BLOW DOWN LINE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: REQUIRED BUT NOT FURNISHED WITH KIT, P&WC SB 7568. MAY BE OBTAINED FROMPRATT AND WHITNEY CUSTOMER SUPPORT.



KIT CATALOG

128-9110-3HMU BLEED AIR IMPROVEMENT ATA : 73400A RK-91 THRU RK-256"RECOMMENDED" SB NO. 73-3354THIS KIT PROVIDES PARTS AND INFORMATION TO CHANGE FROM A PRATT AND WHITNEY MOISTURETRAP TO A RAYTHEON AIRCRAFT CONTINUOUS MOISTURE BLOW DOWN LINE FOR IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3MEN : 1 (MAN)

128-9202-0003FUEL CAPS, MEDECO LOCK ATA :400, 400A ALLMU-300, MU-300-10 ALLTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL LOCKING MEDECO FUEL CAPS IN LIEU OFEXISTING FUEL CAPS FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

132-3019-1 SHORIZONTAL STAB DEICER GAP CONTACTOR ATA :400T (TX) TX-1 THRU TX-9THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HORIZONTAL STAB DE-ICE WIRING FOR USEON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: M81969/14-02, M22520/5-100, MS2252015-103, M22520/5-01, M22520/1-02, M22520/1-01,MS25441, MS23002, MILT43435, 515-700 REQUIRED BUT NOT FURNISHED WITH KIT. IF NOTAVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.

WT. CHANGE : WT: + 4.6 LBS; MOMENT: 1945.0 IN.-LBSEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

132-9100-0001FASTENER MODIFICATION INLET DUCT ASSEMBLY-INFO ONLY ATA :

& CUSTOMER HELD SPARES400 RJ-1 THRU RJ-65;400 RK-1 & UPTHIS KIT PROVIDES INFORMATION TO REPLACE FIVE DSUZ FASTENERS WITH SCREWS AND NUTPLATES.INFORMATION SHOWN IS FOR LEFT ENGINE NACELLE ONLY. RIGHT ENGINE NACELLE IS OPP.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 7 HOURS PER ENGINEMEN : N/A


KIT CATALOG

132-9100-0002FASTENER MODIFICATION INLET DUCT ASSEMBLY-INFO ONLY ATA :

CUSTOMER HELD SPARES.400 RJ-1 THRU RJ-65400A RK-1 & UP400T (T-1A); TT-1 THRU TT-180400T (TX) TX-1 & UPTHIS KIT PROVIDES INFORMATION TO REPLACE FIVE DSUZ FASTENERS WITH SCREWS AND NUTPLATES.INFORMATION SHOWN IS FOR LEFT ENGINE NACELLE ONLY. RIGHT ENGINE NACELLE IS OPP.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 7 HOURS PER ENGINEMEN : N/A

140-8004-0001COVER PLATE ATA :

HS, BH, BAE 125 SERIES 1-1000 & HAWKER800, 800 (U125A), 800XP, 850XP, & 1000 SOEQUIPPED.THIS KIT PROVIDES PARTS AND INFORMATION FOR SPARES REPLACEMENT ON P/N 25-9UN15-1,25-8UN675-3, 25-UN99 AND/OR 25-8UN259-1 AXLE BEARING COVER PLATES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE::::


400-3003-1 SWINDSHIELD DEFOGGER ATA : 30MU300, 400THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE 1 COCKPIT SIDE WINDOW DEFOG BLOWERPART NUMBER AFE-7000.WT. CHANGE : N/AEST. MAN/HRS: : 10MEN : 1 (MAN)

400-5005-1 SCHIME INSTALLATION ATA : 23400 RJ-1 THRU RJ-48MU300 (DIA 1/1A) 0003SA THRU 092SATHIS KIT PROVIDES SPARES REPLACEMENT FOR EC350 OR 45A80588-001 CHIME ASSEMBLY.WT. CHANGE : N/AEST. MAN/HRS: : 4MEN : 1 (MAN)


KIT CATALOG

400-8001-1 SBEARING REWORK, NOSE WHEEL ATA : 32MU33, 400, 400ATHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL REPLACEMENT WHEEL BEARINGS ON THENOSE WHEEL.

NOTENOTENOTENOTE:::: NEED TO REMOVE AND DISCARD (2) 45031-5 NOSE WHEEL AXLE SPACES, (2) SKF13685XLNOSE WHEEL BEARINGS AND (2) SKF13621XL NOSE WHEEL CUP BEARINGS (PARTNUMBER TYSON) FROM REFERENCE MODEL AIRCRAFT TO ACCOMPLISH REWORK ANDINSTALL REPLACEMENTS.


400-9001-1 SINTAKE DUCT, ENGINE ATA :400 RJ-1 THRU RJ-50MU300-10 A1001SA THRU A1011SASB NO. 2251 OR SUBSEQUENTTHIS KIT PROVIDES PARTS REQUIRED FOR REPLACEMENT OF ENGINE AIR INTAKE DUCT WITH ANIMPROVED ASSEMBLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 60MEN : 2 (MEN)



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberELECTRICAL BONDING EQUIPMENT - (101-3232-1) 1

INSTALLATION, AURAL WARNING FLAP, AILERON AND ELEVATOR - (136-3600-1) 1

INSTALLATION AIRBRAKE ANNUNCIATOR - (136-3601-1) 1

INSTALLATION OF TURBINE VIBRATION INDICATOR SYSTEM - (136-9100-1) 1

INSTL, WINGLET, 800XP - (140-1703-1)

2

WINGLET,800XP INSTL - (140-1703-5)

2

LEAD ACID BATTERIES - INFORMATION ONLY - (140-3002-1) 2

REPLACEMENT OF FIRE WARNING BELL - (140-3003-1) 3

KIT-REPLACEMENT OF FIRE WARNING BELL - (140-3004-1) 3

KIT - ADDITION OF SUPPRESSION TO APU - (140-3005-1) 3

REPLACEMENT OF CIRCUIT BREAKERS - (140-3006-1)

4

REPLACEMENT OF CIRCUIT BREAKERS - (140-3006-3) 4

REPLACEMENT OF CIRCUIT BREAKERS - (140-3006-5) 4

REPL OF PITOT PROBE - (140-3009-1) 5

TO DISABLE 'CW' MODE ON THE HF CONTROLLER - (140-3010-1) 5

CONTROL DISPLAY UNIT REPLACEMENT - (140-3014-1) 5



INTRO OF ALTERNATIVE TKS TIMER - (140-3015-1) 6

DEEC OVERSPEED PROTECT SWITCH WIRING - (140-3016-1) 6

ILLUMINATION OF PANEL 'PVA' - (140-3018-1) 6

FIRE EXTINGUISHER MARKER BANDS - (140-3025-0001) 6

PROLINE 21 AIR BRAKE BAULK FOR CANADIAN CERTIFICATION - (140-3026-0001) 7

REPLACEMENT, TIME DELAY RELAY ASSY - (140-3027-0001) 7

REPLACEMENT, TDA310 TIME DELAY RELAY ASSY - (140-3028-0001) 7





CONVERTING MEGG MK1 TO MK2 INSTL - (140-3606-1) 9

ELECTRICAL WIRE PROTECTION INSTL - (140-3607-0001) 10

ELECTRICAL WIRE PROTECTION INSTL - (140-3607-0003) 10

CONVERTING STBY AIRSPEED/ALT/ATTITUDE TO MEGGITT-MK2 INSTL - (140-3608-1) 10

TO INTRODUCE MODIFIED GUTTER ARRANGEMENT ON FRAME - (140-4001-1) 11

REPLACEMENT OF FLAP SHROUD RUB STRIP - (140-4002-1) 11

VENTRAL TANK ACCESS PANEL - (140-4003-0001) 11



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberVENTRAL TANK ACCESS PANEL - (140-4003-0002) 11

FRAME 12 & 14 REINFORCEMENT - (140-4004-0001) 12

EMI SHIELDING INSTL - (140-4005-1) 12



STATIC PLATE DOUBLER - (140-4006-0001) 13

INSTALLATION OF HYDRAULIC PIPING, WING OUTER SECTION - (140-5001-1) 13

HYDRAULIC PIPING BYPASS OF AIRBRAKE WITH RESTRICTOR - (140-5003-1) 13

HYDRAULIC PIPING BYPASS OF AIRBRAKE WITH RESTRUCTOR - (140-5003-3) 14

EXTENDED OXYGEN SYSTEM, 3RD OXYGEN BOTTLE - (140-5004-1) 14

AIR CONDITIONING CONNECTING SLEEVE - (140-5006-1)

14

KIT - INTRODUCTION OF RUDDER BIAS RUDDER - (140-5008-1) 14

INTRODUCTION OF MANUALLY OPERATED PRESSURE RELEASE VALVES - (140-5015-1) 15

A/C LOUVER REPLACEMENT,COCKPIT SIDE CONSOLE (L/H LOUVER INSTALLATION) - (140-5017-0001) 15

A/C LOUVER REPLACEMENT,COCKPIT SIDE CONSOLE (R/H LOUVER INSTALLATION) - (140-5017-0002) 15

AIR CONDITIONING OUTLET - (140-5018-0001) 15

AIR CONDITIONING OUTLET - (140-5018-0003) 16

FLAP ASSEMBLY, INSTL OF COUNTERSUNK BOLT - (140-7001-0001) 16

FLAP ASSEMBLY, INSTL OF COUNTERSUNK BOLT - (140-7001-0003) 16

KIT - LANDING GEAR TORQUE LINK BUSHING - (140-8003-1) 17

LANDING GEAR-TORQUE LINK BUSHING - (140-8003-3) 17

NLG, TORQUE LINK BUSHINGS AND SPACERS - (140-8121-1) 17

MAIN GEAR FAIRING ASSY - (140-8124-0004)

18

APU SYSTEM - INFORMATION ONLY - (140-9001-1) 18

INDICATORS FOR FUEL TEMP & FILTER - (149-3011-0001) 18

STRUCTURAL PROVISIONS FOR INSTL OF CDU UNITS W/WEATHER GRAPHICS (822-1485-102) -(149-3411-0001)

18

KIT INSTALLATION-DA-A C B INSTL,LOCATOR - (149-3412-0001) 19

KIT-BUSSING UPGRADE, FUEL STATUS DISPLAY - (149-3413-0001) 19

AUDIO PANEL UPDATE - (149-3414-0001) 19






COLLINS TDR-94D MODE S ENHANCED SURVEILLANCE UPGRADE - (149-3417-0001)

21



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberELEMENTARY SURVEILLANCE FLIGHT ID UPGRADE-INFO ONLY - (149-3418-0001) 22

COLLINS FMS-6000 FLIGHT MGMT SYS V.3.0.3 UPDATE-INFO ONLY - (149-3419-0001) 22

COLLINS FMS-6000 FLIGHT MGMT SYS V.3.0.3 UPDATE-INFO ONLY - (149-3419-0003) 22

RELOCATION OF ARTEX C406-2 E.L.T. - (149-3421-0001)

22

AURAL WARN,FLAP AILERON & ELEVATOR INSTALLATION - (149-3601-1)

23

INSTL TURBINE VIBRATION IND SYS - (149-9100-1) 23

800 SRS TOOL KIT - (25-7-Y19 AB) 23

AUDIO/OXYGEN/LIGHTING - (401-3010-0001) 23

OBSERVER SEAT - SYSTEMS INSTALLATION - (401-3010-0003) 24

KIT - AUDIO PANEL AND MUTE - (401-3011-0007) 24

GROSS WEIGHT INCREASE 39,500 LB - (401-4000-0001) 24

GROSS WEIGHT INCREASE 39,500 POUNDS - (401-4000-0003) 24

PROVISIONS INSTL CIRCUIT BREAKER - (401-4001-0001) 25

SHROUD REWORK, WHEEL WELL, MLG - (401-4002-0001) 25

GASKET FABRICATION AND REPLACEMENT - (401-5501-0001) 25

FUEL SYSTEM ICING INHIBITOR ELIMINATION - (401-9000-0001) 25

INSTALLATION - FUEL WIRING SEPARATION - (401-9012-0001) 25

EME SUPPRESION INSTALLATION KIT - (401-9013-0001) 26


KIT CATALOG

101-3232-1ELECTRICAL BONDING EQUIPMENT ATA :THIS KIT PROVIDES SUPPLIES FOR PROPER ELECTRICAL BONDING TO METALS ON ALL NON-COMPOSITERAYTHEON AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

136-3600-1INSTALLATION, AURAL WARNING FLAP, AILERON AND ELEVATOR ATA :800XP 258279, 258283HAWKER SB NO. 01-24)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO WIRE THE FLAPS, AILERONS ANDELEVATOR INTO SHIPS AURAL WARNING SYSTEM FOR TAKE OFF CONFIGURATION ON INSERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT TO BE INSTALLED IN CONJUNCTION WITH KITS 136-3601-1 AND 136-9100-1.NOTENOTENOTENOTE:::: REFERENCE ITEM REQUIRED, BUT NOT SUPPLIED WITH KIT: SOLDER: SN60WRMAP3.031.

IF NOT AVAILABLE IN YOUR SHOP STOCK, YOU CAN PROCURE LOCALLY.NOTENOTENOTENOTE:::: THIS KIT TO BE INSTALLED IN CONJUNCTION WITH KITS 136-3600-1 AND 136-9100-1.


136-3601-1INSTALLATION AIRBRAKE ANNUNCIATOR ATA :800XP 258279, 258283HAWKER SB NO. 01-23. (09/17/96)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A AIRBRAKE ANNUNCIATORLIGHT ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

136-9100-1INSTALLATION OF TURBINE VIBRATION INDICATOR SYSTEM ATA :800XP 258279, 258283HAWKER SB NO. 01-22 (DTD: 09/17/96)THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A TURBINE VIBRATIONINDICATOR SYSTEM ON INSERVICE AIRCRAFT.WT. CHANGE : WT: 6.08 LBS; MOMENT -1.2125 FT.EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

140-1703-1INSTL, WINGLET, 800XP ATA : 57

800XP 258604 THRU 258609, 258611 THRU 258628,258630 THRU 258684, 258686 THRU 258734AND 258736 THRU 258749

"O"S.B.57-3810THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL WINGLETS ON THE TIP OF THE WING ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: :"MS20426AD5-8","MS20426AD5-7","MS20426AD5-6","MS20426AD4-5","MS20426AD3","MS20426AD4-13","MS20426AD4-12","MS20426AD4-10","MS20426AD4-8","MS20426AD4-7","MS20426AD5","MS20426AD3-6" & "MS20426AD3-5" RIVETS; "PR1425" & "PR1440" SEALER &"EA9309.3NA" ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +89 LB MOMENT: +38,890 LB-INEST. MAN/HRS: : 200 HRS.MEN : 2 (MEN)

140-1703-5WINGLET,800XP INSTL ATA :

800XP S/N: 258604 THRU 258609, 258611 THRU258628, 258630 THRU 258684, 258686 THRU258749 EXCEPT 258627, 258659, 258670,258684, 258717, 258724, 258729, 258742AND 258749. ALL U-125A ARE EXCLUDEDFROM THIS KIT.

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL WINGLETS ON THE TIP OF THE WING ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NOTE:"MS20426AD5""MS20426AD4-5""MS20426AD3-6""MS20426AD3-5""MS20426AD4-5""MS20426AD3""MS20426AD4-13""MS20426AD4-12""MS20426AD4-10""MS20426AD4-8""MS20426AD4-7""MS20426AD5-8""MS20426AD5-7""MS20426AD5-6" RIVETS,"PR1440""PR1425" SEALER, "EA9309-3NA""EA9309NA" ADHESIVE, "EA960" FILLER, AND"AMS-8802" SEALANT REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE FROM ANYCOMPANY AUTHORIZED OUTLET.

WT. CHANGE : +89 LB MOMENT: +622.45 LB-FTEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-3002-1LEAD ACID BATTERIES - INFORMATION ONLY ATA :800XP 258414 THRU 258423, EXCEPT 258421THIS KIT PROVIDES PARTS AND INFORMATION TO ACCOMMODATE INSTALLATION OF LEAD ACIDBATTERIES TO REPLACE NI-CAD BATTERIES ON INSERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

140-3003-1REPLACEMENT OF FIRE WARNING BELL ATA : 26AE 125 SERIES 1000A/1000BAE 125 SERIES 800A/800BBH/HS/BAE 125 SERIES 600A/600B, 252739 AND 252825BH/HS/BAE 125 SERIES 700A/700B WHICH ARE POST MODHAWKER 1000 AIRCRAFTHAWKER 800/800XPSB NO. 26-3323THIS KIT PROVIDES PARTS REQUIRED TO ACCOMMODATE INSTALLATION OF REPLACEMENT FIREWARNING BELL ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: A ND IS ELIGIBLE FOR AIRCRAFT S/N PRE MOD 25F566A PER PENDING "OPTIONAL"SERVICE BULLETIN NO. 26-3323.

NOTENOTENOTENOTE:::: "MIL-P-23377" EPOXY PRIMER,"EC2262" ADHESIVE,"EA9394" FILLER AND "SN60WRMAP3(QQ-S-571)" SOLDER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM RAPID OR YOUR LOCAL SUPPLIER.


140-3004-1KIT-REPLACEMENT OF FIRE WARNING BELL ATA : 26SB NO. 26-3378ORDER PIECE PARTS 8/3/2000TPWT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

140-3005-1KIT - ADDITION OF SUPPRESSION TO APU ATA : 31BAE. 125 SERIES 800A/BHAWKER 800/ 800XP***HAWKER 800XP & SERIEALS 258001 THROUGHT 258474,

EQUIPPED WITH GARRETT GTCP36-150(W)APU

HAWKER 800XP & HAWKER 800 EQUIPPED WITH GTC36-150W APUSB NO. 31-3385THIS KIT PROVIDES PARTS AND INSTRUCTIONS REQUIRED TO ACCOMODATE INSTALLATION OFREPLACEMENT APU RELAY TRANSIENT SUPPRESSION TO IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

140-3006-1REPLACEMENT OF CIRCUIT BREAKERS ATA : 24

ALL BAE 125 SERIES 800A/800B, HAWKER800/800XP

WHICH ARE PRE MOD 25E134A

SB NO. 24-3338THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF REPLACEMENT CIRCUITBREAKERS ON ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-P-23377" EPOXY PRIMER, "MIL-C-5541" ALODINE, & GREY PAINT ARE REQUIRED BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


140-3006-3REPLACEMENT OF CIRCUIT BREAKERS ATA : 24ALL BAE 125 SERIES 1000 & HAWKER 1000PER S.B.#24-3330 KIT NO. 1

PRE MOD 25F606B

SB # 24-3330 KIT NO. 2THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF REPLACEMENT CIRCUITBREAKERS FOR PANEL G-G ON ALL IN SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-P-23377: EPOXY PRIMER, "MIL-C-5541" ALODINE, & GREY PAINT ARE REQUIRED BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


140-3006-5REPLACEMENT OF CIRCUIT BREAKERS ATA : 24ALL BAE 125 SERIES 1000 WHICH ARE PRE MOD 25F606BHAWKER 1000 WHICH ARE PRE MOD 25F606BSB # 24-3330 KIT NO. 2THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF REPLACEMENT CIRCUITBREAKERS FOR PANEL G-K ON ALL IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-P-23377" EPOXY PRIMER, "MIL-C-5541" ALODINE, & GREY PAINT ARE REQUIRED BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 4 HRS.MEN : 1 (MAN)


KIT CATALOG

140-3009-1REPL OF PITOT PROBE ATA : 34800XP 258266 & 258277 THRU 258500SB NO. 34-3412KIT IS FOR MANDATORY HAWKER SB 34-3412. BULLETIN IS MANDATORY FOR ALL 800XP MODELS S/N:258266 & 258277 THRU 258500 = 224. ESTIMATED DEMAND IS 180 KITS OVER 24 MONTH COMPLIACEPERIOD.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 50MEN : N/A

140-3010-1TO DISABLE 'CW' MODE ON THE HF CONTROLLER ATA : 23BAE125 SERIES 800A (C-29A & U-125)THIS KIT PROVIDES INSTRUCTIONS AND PARTS REQUIRED TO DISABLE CW MODE ON THE HFCONTROLLER AND IDENTIFY THAT INOPERABILITY ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1MEN : 1 (MAN)

140-3014-1CONTROL DISPLAY UNIT REPLACEMENT ATA :HONEYWELL CONFIGURED HAWKER800XP AIRCRAFT

S/N: RG258366 THRU RG258507

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO CD-820 CDU'S IN PLACE OF THE CD-815CDU'S ON IN-SERVICE AIRCRAFT.WT. CHANGE : WT: -4.8 LBS, ARM: -224.0 INS, MOMENT: 1075.2 IN-LBS.EST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A

140-3014-3CONTROL DISPLAY UNIT REPLACEMENT ATA :HONEYWELL CONFIGURED HAWKER800XP AIRCRAFT

S/N: RG258297 THRU RG258365, RG258508,RG258510, AND RG258511.

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO CD-820 CDU'S IN PLACE OF THE CD-810CDU'S ON IN-SERVICE AIRCRAFT.WT. CHANGE : WT: -11.4 LBS, ARM: -224.0, MOMENT: 2553-6 IN-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-3014-5CONTROL DISPLAY UNIT REPLACEMENT ATA :HONEYWELL CONFIGURED 800XPAIRCRAFT

S/N: RG258297 THRU RG258508, RG258510AND RG258511

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TWO 5 AMP CIRCUIT BREAKERS IN PLACE OFTWO 2 AMP CIRCUIT BREAKERS NEEDED FOR TWO HONEYWELL CD-820 CONTROL DISPLAY UNITS ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

140-3015-1INTRO OF ALTERNATIVE TKS TIMER ATA : 30HAWKER SERIES PRE-MOD 25G005A OR 25E266A, IN-

SERVICESB NO. 30-3455THIS KIT PROVIDES PARTS REQUIRED TO INTRODUCE THE ALTERNATIVE TKS TIMER ON ALL HAWKERSERIES, PRE-MOD 25G005A OR 25E266A, IN-SERVICE AIRCRAFT PER "OPTIONAL" SB #30-3455.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2MEN : 1 (MAN)

140-3016-1DEEC OVERSPEED PROTECT SWITCH WIRING ATA : 76800XP POST MOD 25G103ASB #76-3480THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF AN ADDED JUMPER WIRE TOTHE NO. 1 & NO. 2 DEEC OVERSPEED PROTECTION SWITCH ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-3018-1ILLUMINATION OF PANEL 'PVA' ATA : 24PRE-MOD 25E188A HAWKER 800 (U125A) 258245, 258247, 258250, 258268, 258288,

258305, 258306, 258325, 258333 & 258341THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF ELECTRICAL WIRING TOENABLE THE ILLUMINATION OF THE 'PVA' PANEL ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-3025-0001FIRE EXTINGUISHER MARKER BANDS ATA : 26ALL BAE 125 SERIES 800A/800B(INCLUDING MAJOR VARIANTS C-29A ANDU-125A) AND HAWKER 800XP

THRU S/N: 258615

THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF ADDITIONAL MARKER BANDSFOR THE FIRE EXTINGUISHER SYSTEM ON ALL IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 1.5 HRS.MEN : 1 (MAN)


KIT CATALOG

140-3026-0001PROLINE 21 AIR BRAKE BAULK FOR CANADIAN CERTIFICATION ATA : 27800XP 258541, 258556, 258567 AND SUBSEQUENTTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO PREVENT MOVEMENT OF THE AIRBRAKE/LIFT DUMP SELECTOR LEVER FROM THE SHUT POSITION WHEN FLAPS ARE EXTENDED IN FLIGHT BY ANELECTRONICALLY SIGNALLED SOLENOID BAULK. A BAULK POSITION INDICATOR IS PROVIDED TO

NOTENOTENOTENOTE:::: "MS20995C32" SAFETY WIRE, "PR1431" SEALANT, "MPK" METHYL-PROPHYL-KETONEREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.


140-3027-0001REPLACEMENT, TIME DELAY RELAY ASSY ATA : 31ALL HAWKERS 125 SERIES 700 AIRCRAFTWITH MOD252328 INSTALLEDTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A 140-360044-0002 TIME DELAYRELAY ASSY AS A SPARES REPLACEMENT FOR EXISTING TDA310 OR TDA310A TIME DELAY UNIT ASSYON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: DH.125 SERIES 1A; HS.125 SERIES 1B; DH.125 SERIES 1A-522; HS.125 SERIES 1B-522;DH.125 SERIES 1A/R-522; HS.125 SERIES 1B/R-522; DH.125 SERIES 1A/S-522; HS.125SERIES 1B/S-522; DH.125 SERIES 3A; HS.125 SERIES 3B; DH.125 SERIES 3A/R; HS.125SERIES 3B/R; DH.125 SERIES 3A/RA; HS.125 SERIES 3B/RA; HS.125 SERIES 3B/RB; HS.125SERIES 3B/RC; HS.125 SERIES F3B; HS.125 SERIES F3B/RA; BH.125 SERIES 400A; DH.125SERIES 400A; HS.125 SERIES 400A; HS.125 SERIES 400B; HS.125 SERIES 400B/1; HS.125SERIES F400B; BH.125 SERIES 600A; HS.125 SERIES 600A; HS.125 SERIES 600B; HS.125SERIES 600B/1; HS.125 SERIES 600B/2; HS.125 SERIES 600B/3; HS.125 SERIES F600B;HS.125 SERIES 700A; HS.125 SERIES 700B; BAE.125 SERIES 800A; BAE.125 SERIES 800A(C-29A); BAE.125 SERIES 800A (U-125); BAE.125 SERIES 800B; HAWKER 800; HAWKER 800(U-125A); HAWKER 800XP AND HAWKER 850XP.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 3 HOURSMEN : 1 (MAN)

140-3028-0001REPLACEMENT, TDA310 TIME DELAY RELAY ASSY ATA : 31ALL HS/BH. 125 SERIES 600 AIRCRAFTWITH MODS252328 INSTALLED. REFMODEL 600A AND 600BTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A 140-360044-0002 OR140-360044-0015 TIME DELAY RELAY ASSY AS A SPARES REPLACEMENT FOR EXISTING TIME DELAYRELAY PART NUMBERS TDA310, TDA310A, TDA310MK2 OR TDA310MK3 TIME DELAY UNIT ASSY ON IN-SERVICE AIRCRAFT.




KIT CATALOG

140-3028-0003REPLACEMENT, TDA310 TIME DELAY RELAY ASSY ATA : 31ALL HS/BH. 125 SERIES 600 AIRCRAFTWITH MODS252328 INSTALLED. REFMODEL F600BTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A 140-360044-0002 OR140-360044-0015 TIME DELAY RELAY ASSY AS A SPARES REPLACEMENT FOR EXISTING TIME DELAYRELAY ASSY PART NUMBERS TDA310, TDA310A, TDA310MK2 OR TDA310MK3 TIME DELAY UNIT ASSY ONIN-SERVICE AIRCRAFT.



140-3028-0005REPLACEMENT, TDA310 TIME DELAY RELAY ASSY ATA : 31ALL HS/BH. 125 SERIES 600 AIRCRAFTWITH MODS252328 INSTALLED. REFMODEL 600A AND 600B LONG RANGE FUELTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A 140-360044-0002 OR140-360044-0015 TIME DELAY RELAY ASSY AS A SPARES REPLACEMENT FOR EXISTING TIME DELAYRELAY PART NUMBERS TDA310, TDA310A, TDA310MK2 OR TDA310MK3 TIME DELAY UNIT ASSY ON IN-SERVICE AIRCRAFT.




KIT CATALOG

140-3029-0001REPLACEMENT, TDA310 TIME DELAY RELAY ASSY ATA : 31ALL DH/HS. 125 SERIES 1A, 1B, 3A, 3B, 400A& 400B AIRCRAFT WITH MOD252328INSTALLED. PRE MOD 251721THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A 140-360044-0015 TIME DELAYASSY AS A SPARES REPLACEMENT FOR EXISTING TIME DELAY RELAY PART NUMBERS TDA310, TDA310A,TDA310MK2 OR TDA310MK3 TIME DELAY UNIT ASSY ON IN-SERVICE AIRCRAFT.



140-3029-0003REPLACEMENT, TDA310 TIME DELAY RELAY ASSY ATA : 31ALL DH/HS. 125 SERIES 1A, 1B, 3A, 3B, 400A& 400B AIRCRAFT WITH MOD252328INSTALLED. MOD 251721THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO INSTALL A 140-360044-0015 TIME DELAYRELAY ASSY AS A SPARES REPLACEMENT FOR EXISTING TIME DELAY RELAY PART NUMBERS TDA310,TDA310A, TDA310MK2 OR TDA310MK3 TIME DELAY UNIT ASSY ON IN-SERVICE AIRCRAFT.



140-3606-1CONVERTING MEGG MK1 TO MK2 INSTL ATA :800XP S/N: 8475 THRU 8511 AND 8513 THRU 8519THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A MEGGITT MK2 (ELECTRONICSTANDBY INSTRUMENT SYSTEM FOR HONEYWELL EQUIPPED IN-SERVICE AIRCRAFT) EQUIPPED WITHMEGGITT MK1, ELECTRONIC STANDBY INSTRUMENT SYSTEM.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION HAS BEEN INCORPORATED. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : 8.1 LBS. MOMENT: -50.8 LB-FT.EST. MAN/HRS: : CONTACT CUSTUMER SUPPORTMEN : N/A


KIT CATALOG

140-3607-0001ELECTRICAL WIRE PROTECTION INSTL ATA : 26HAWKER 800 AND HAWKER 800(U-125A) S/N: UP TO AND INCLUDING 258445HAWKER 800XP S/N: UP TO AND INCLUDING 258519"MANDATORY" SB NO. 26-3496THIS KIT PROVIDES PARTS AND INFORMATION NECSSARY TO INSTALL ELECTRICAL WIRE PROTECTIONFOR WIRES ROUTED THROUGH THE FIREWALLS TO THE MAIN ENGINES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS AND INFORMATION NECSSARY TO INSTALL ELECTRICAL WIREPROTECTION FOR WIRES ROUTED THROUGH THE FIREWALLS TO THE MAIN ENGINES ONIN-SERVICE AIRCRAFT.

WT. CHANGE : +1.5 LB; MOMENT: +9.87 LB-FTEST. MAN/HRS: : 10 HRS.MEN : 1 (MAN)

140-3607-0003ELECTRICAL WIRE PROTECTION INSTL ATA : 26BH.125 SERIES 400A,600A FITTED WITH TFE731-3H ENGINESDH.125 SERIES 1A,1A/S-522,3A,3A/R,3A/RA,400A

FITTED WITH TFE731-3H ENGINES

HS.125 SERIES 700A & B AIRCRAFT FITTED WITH TFE731-3H ENGINESHS.125 SERIES F3B,F3B/RA,F400B,F403B &F600B

FITTED WITH TFE731-3H ENGINES

"MANDATORY" SB NO. 26-3496THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL ELECTRICAL WIRE PROTECTIONFOR WIRES ROUTED THROUGH THE FIREWALLS TO THE MAIN ENGINES ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)

140-3608-1CONVERTING STBY AIRSPEED/ALT/ATTITUDE TO MEGGITT-MK2 INSTL ATA : 31800XP S/N: 8266 THRU 8475THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A MEGGITT MK2 (ELECTRONICSTANDBY INSTRUMENT SYSTEM FOR HONEYWELL)IN-SERVICE AIRCRAFT EQUIPPED WITH SMITH'SSTANDBY AIRSPEED/ALTIMETER/ATTITUDE INSTRUMENT SYSTEM.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL ORPILOT'S OPERATING HANDBOOK REVISION HAS BEEN INCORPORATED. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : CHANGE: 8.1 LB. MOMENT: -50.8 LB-FT.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

140-4001-1TO INTRODUCE MODIFIED GUTTER ARRANGEMENT ON FRAME ATA : 5300XP PRE-MOD 25F909A AIRCRAFT S/N: 258266 THRU 258519SB NO. 53-3310THIS KIT PROVIDES PARTS REQUIRED TO PREVENT WATER (MOISTURE) INGRESS INTO AVIONICS BAYAREA. KIT FURNISHS 1EA NEW GUTTER, AND REQUIRED RIVETS: "MS20470AD4-4-5" 34EA & "132269A402"2EA OR BEECH SPEC EQUILIVANT.

NOTENOTENOTENOTE:::: "PR1440" THIOKOL REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : PART I-6 HRS. PART II-1 HR.MEN : 1 (MAN)

140-4002-1REPLACEMENT OF FLAP SHROUD RUB STRIP ATA : 57125 SERIES PRE MOD 253419E"OPTIONAL" SB NO. 57-3364THIS KIT PROVIDES PARTS REQUIRED TO REPLACE EXISTING RUB STRIP WITH NEW "P-SEAL" ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 6MEN : 1 (MAN)

140-4003-0001VENTRAL TANK ACCESS PANEL ATA :ALL BAE 125-800 PRE-MOD 25G137AHAWKER 800 PRE-MOD 25G137AHAWKER 800XP PRE-MOD 25G137ATHIS KIT PROVIDES PARTS & INFORMATION REQUIRED FOR THE ADDITION OF ACCESS PANELS TO THEVENTRAL FUEL TANK OF IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: -0001 & -0002 INSTL ARE IDENTICAL BUT OPPOSITE.IF AIRCRAFT IS POST-MOD 253074A BUT PRE-MOD 25G137A, INSTALL -0002 ONLY.IF AIRCRAFT IS PRE-MOD 253074A, INSTALL -0001 & -0002.


140-4003-0002VENTRAL TANK ACCESS PANEL ATA : 53 HAWKER 800 PRE-MOD 25G137A HAWKER 800XP PRE-MOD 25G137AALL BAE 125-800 PRE-MOD 25G137ATHIS KIT PROVIDES PARTS & INFORMATION REQUIRED FOR THE ADDITION OF ACCESS PANELS TO THEVENTRAL FUEL TANK OF IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT CUSTOMER SUPPORTMEN : N/A


KIT CATALOG

140-4004-0001FRAME 12 & 14 REINFORCEMENT ATA : 53800XP S/N: 258541, 258556 AND 258567 THRU

258592"MANDATORY" SB NO. 53-3569THIS KIT PROVIDES PARTS FOR USE WITH SB #53-3569 FOR THE HAWKER 800XP AIRCRAFT ONLY.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 120MEN : 2 (MEN)

140-4005-1EMI SHIELDING INSTL ATA :MODEL 800XP (PRO LINE 21 FOR JAROPSEUROPEAN REGISTERED AIRCRAFT)

RG8567 & UP

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL EMI PROTECTION FOR ELECTRICAL ANDAVIONICS EQUIPMENT IN NOSE COMPARTMENT ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "980-2000-348" EMI BACKSHELL & NAPTHA OR MPK REQUIRED BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +5.0 LB MOMENT: -111.0 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-4005-5EMI SHIELDING INSTL ATA :MODEL 800XP (PROLINE 21, JAROPSEUROPEAN COMPLIANT AIRCRAFT)

RG8541, RG8556, RG8567 & UP, EXCEPTRG8618, RG8656, RG8663, RG8664, RG8673& RG8686

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL EMI PROTECTION FOR ELECTRICAL ANDAVIONICS EQUIPMENT IN NOSE COMPARTMENT ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR-148" PRIMER, "PR-2200""EC2084" SEALANT, NAPTHA OR MPK CLEANSER & "EA9309NA"ADHESIVE REQUIRED BUT NOT SUPPLIED WITH KIT. PROCURE SEPERATELY FROM ANYCOMPANY AUTHORIZED OUTLET.

WT. CHANGE : +5.0 LB MOMENT: -111.0 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-4005-7EMI SHIELDING INSTL ATA :800XP PROLINE 21, JAROPS EUROPEANCOMPLIANT A/C

RG8618, RG8656, RG8663, RG8664, RG8673& RG8686.

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE ACCESS DOOR TO EASE INSPECTION OFTHE EMERGENCY HYDRAULIC TANK FLUID LEVEL IN NOSE COMPARTMENT OF IN-SERVICE AIRCRAFT.WT. CHANGE : +5.O LB MOMENT: -111.0 LB-INEST. MAN/HRS: : EST. MAN/HRS: CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

140-4006-0001STATIC PLATE DOUBLER ATA : 53ALL MODEL BAE.125 SERIES 800ABAE.125 SERIES 800A(C-29A)BAE.125 SERIES 800A(U-125);BAE.125 SERIES 800BHAWKER 800HAWKER 800(U-125A)HAWKER 800XP 258001 THRU 258736 AND 258738 THRU

258746"O" S.B. 53-3797THIS KIT PROVIDES PARTS REQUIRED TO ACCOMODATE INSTALLATION OF STATIC PLATE DOUBLERS ONIN-SERVICE AIRCRAFT.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : FOR MODIFICATION, NOT INCLUDING FUNCTIONAL TEST (4 HRS)MEN : 2 (MEN)

140-5001-1INSTALLATION OF HYDRAULIC PIPING, WING OUTER SECTION ATA :800XP 258266, 258277 THRU 258287, 258289 THRU

258304, 258307 THRU 258324, 258327 THRU258330, 258332, 258335, 258337

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RESTRICTOR BYPASSING THE AIR BRAKEACTUATOR TO REDUCE OVERALL HYDRAULIC SYSTEM TEMPERATURE PROFILE FOR INSERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-5003-1HYDRAULIC PIPING BYPASS OF AIRBRAKE WITH RESTRICTOR ATA : 29800XP POST MOD 25F624ATHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RESTRICTOR BYPASSING THE AIR BRAKEACTUATOR TO REDUCE OVERALL HYDRAULIC SYSTEM TEMPERATURE PROFILE FOR IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

140-5003-3HYDRAULIC PIPING BYPASS OF AIRBRAKE WITH RESTRUCTOR ATA : 29BAE.125 SERIES 800A POST MOD. 259283C AND PRE MOD.

25F624A.BAE.125 SERIES 800B POST MOD. 259283C AND PRE MOD.

25F624A.HAWKER 800XP POST MOD. 259283C AND PRE MOD.

25F624A.THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A RESTRICTOR BYPASSING THE AIR BRAKEACTUATOR TO REDUCE OVERALL HYDRAULIC SYSTEM TEMPERATURE PROFILE FOR IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

140-5004-1EXTENDED OXYGEN SYSTEM, 3RD OXYGEN BOTTLE ATA :800XP 258412 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO ACCOMMODATE INSTALLATION OF A 3RDOXYGEN STORAGE BOTTLE ON INSERVICE AIRCRAFT.WT. CHANGE : AIRCRAFT MUST BE WEIGHED AFTER KIT INSTALLATION IS COMPLETE.EST. MAN/HRS: : CONTACT PRODUCT SUPPORT COMPLIANCE WITH CAR 4B.101 MUST BE MAINTAINED.MEN : N/A

140-5006-1AIR CONDITIONING CONNECTING SLEEVE ATA : 21

HAWKER 800XP S/N: U-125, U125A, C-29A PRE-MOD25F963A/B

SB NO. 21-3377 OR SUBSEQUENTTHIS KIT PROVIDES PARTS REQUIRED TO PREVENT DISCONNECTION OF THE CONNECTING SLEEVE.

NOTENOTENOTENOTE:::: BEDDING STRIPS ARE NO LONGER REQUIRED. THUS, BA7224 KIT IS NO LONGERREQUIRED. ACCEPTABLE TO USE BA7224 KIT TO PROVIDE THE BA7224-1 SLEEVE ANDBAS244-0560-2 CLAMPS.*** ALL AFFECTED A/C HAVE COMPLIED WITH THIS S/B


140-5008-1KIT - INTRODUCTION OF RUDDER BIAS RUDDER ATA : 27WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A


KIT CATALOG

140-5015-1INTRODUCTION OF MANUALLY OPERATED PRESSURE RELEASEVALVES

ATA : 29

800XPSB NO. 29-3225THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED TO ACCOMODATE INSTALLATION OFMANUALLY OPERATED PRESSURE RELEASE VALVES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "2014A/B" ADHESIVE, LOCKING WIRE, "PR1431" SEALANT, & HYDRAULIC FLUID REQUIREDBUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : +3.6 LBS. MOMENT: +33.8 LBS-FTEST. MAN/HRS: : MAN/HRS: 40 HRS.MEN : 1 (MAN)

140-5017-0001A/C LOUVER REPLACEMENT,COCKPIT SIDE CONSOLE (L/H LOUVERINSTALLATION)

ATA : 21

800 A/C EQUIPPED WITH ARKANSASAEROSPACE PANELS 800-8827-1/-2, -36/-37AND -40/-41.

800XP A/C EQUIPPED WITH ARKANSASAEROSPACE PANELS 800-8827-1/-2, -36/-37AND -40/-41.

THIS KIT PROVIDES PARTS & INSTRUCTIONS REQUIRED TO ACCOMODATE INSTALLATION OFREPLACEMENT AIR CONDITIONING LOUVER IN LOWER COCKPIT SIDE CONSOLE ON IN-SERVICEAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-5017-0002A/C LOUVER REPLACEMENT,COCKPIT SIDE CONSOLE (R/H LOUVERINSTALLATION)

ATA :

800 & 800XP A/C EQUIPPED WITH ARKANSASAEROSPACE PANELS 800-8827-1/-2, -36/-37AND -40/-41

THIS KIT PROVIDES PARTS & INSTRUCTIONS REQUIRED TO ACCOMODATE INSTALLATION OFREPLACEMENT AIR CONDITIONING LOUVER IN LOWER COCKPIT SIDE CONSOLE ON IN-SERVICEAIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-5018-0001AIR CONDITIONING OUTLET ATA :THESE KITS PROVIDE SPARES REPLACEMENT PARTS REQUIRED TO REPLACE COMPONENTS THAT ARENO LONGER AVAILABLE.

THE -0001 KIT PROVIDES OUTLETS THAT REPLACE THE 800-9402-26/27 AND 800-9402-11/12 LOUVERASSYS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

140-5018-0003AIR CONDITIONING OUTLET ATA :THESE KITS PROVIDE SPARES REPLACEMENT PARTS REQUIRED TO REPLACE COMPONENTS THAT ARENO LONGER AVAILABLE.

NOTENOTENOTENOTE:::: THE -0003 KIT PROVIDES OUTLETS THAT REPLACE THE 25-8VF445-1A/2A LOUVER ASSYS.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-7001-0001FLAP ASSEMBLY, INSTL OF COUNTERSUNK BOLT ATA : 27700-1000800XPC29AU125U125ACOMMUNIQUE 57-12THIS KIT PROVIDES PARTS REQUIRED TO INSTALL COUNTERSUNK BOLT IN LOWER SKIN OF FLAPS WITHPART NUMBERS: 25-8WF251-1A OR -2A, AND 25-9WF41-1A OR -2A.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS:EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

140-7001-0003FLAP ASSEMBLY, INSTL OF COUNTERSUNK BOLT ATA : 27700-1000800XPC29AU125U125ACOMMUNIQUE 57-12THIS KIT PROVIDES PARTS REQUIRED TO INSTALL COUNTERSUNK BOLT IN LOWER SKIN OF FLAPS WITHPART NUMBERS: 25-7WF3A/4A, 25-8WF3-1A,-2A,-169A,-170A,-383A OR -384A, AND 25-9WF3-1A OR -2A.

NOTENOTENOTENOTE:::: THIS KIT PROVIDES PARTS REQUIRED TO INSTALL COUNTERSUNK BOLT IN LOWER SKINOF FLAPS WITH PART NUMBERS: 25-7WF3A/4A, 25-8WF3-1A,-2A,-169A,-170A,-383A OR-384A, AND 25-9WF3-1A OR -2A.



KIT CATALOG

140-8003-1KIT - LANDING GEAR TORQUE LINK BUSHING ATA : 32H/HS/BAE 125 SERIES 800U-125) INCLUDING MAJOR VARIANTS C-29AHAWKER 800 INCLUDING MAJOR VARIANT U-125AHAWKER 800XP S/N 8266, 8277 THROUGH 8395 AS PER

"RECOMMENDED""RECOMMENDED" SB NO. 32-3135, REV. 2 OR SUBSEQUENTTHIS KIT PROVIDES PARTS REQUIRED TO IMPROVE DURABILITY OF TORQUE LINK BUSHES IN MAINLANDING GEAR ON ALL IN-SERVICE AIRCRAFT (POST-MOD 253257A).

NOTENOTENOTENOTE:::: LIGHT MINERAL OIL, MOTOR OIL, DRY ICE, LIQUID NITROGEN, GREASE,JOINTINGCOMPOUND AND SOLVENT REQUIRED BUT NOT FURNISHED WITH KIT. OBTAIN FROMRAPID OR YOUR LOCAL SUPPLIER.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 33 HRS.MEN : 1 (MAN)

140-8003-3LANDING GEAR-TORQUE LINK BUSHING ATA : 32BH/HS/BAE 125 SERIES 800 (INCLUDING MAJOR VARIANTS C-29A AND

U-125)HAWKER 800 (INCLUDING MAJOR VARIANT U-125A)HAWKER 800XP 8266, 8277 THROUGH 8395 AS PER

"RECOMMENDED" SERVICE BULLETIN NO.32-3135 REV 1, NOW REV 2 8/01

THIS KIT PROVIDES PARTS REQUIRED FOR MODIFICATION OF SPARES ON IN-SERVICE AIRCRAFT.NOTENOTENOTENOTE:::: LIGHT MINERAL OIL, MOTOR OIL, DRY ICE, LIQUID NITROGEN, GREASE, JOINTING

COMPOUND AND SOLVENT REQUIRED BUT NOT FURNISHED WITH KIT. OBTAIN LOCALLYFROM RAPID OR YOUR LOCAL SUPPLIER.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : MAN/HRS: 33 HRS.MEN : 1 (MAN)

140-8121-1NLG, TORQUE LINK BUSHINGS AND SPACERS ATA : 32ALL HS, DH, BH, BAE125 PRE MOD 25G025A & ECR12786HAWKER SERIES PRE MOD 25G025A & ECR12786SB NO. 32-3516THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW BUSHINGS AND SPACERS IN TORQUELINKS, AXLE AND TORQUE LINK PICK-UP SLEEVE FOR IN-SERVICE AIRCRAFT

NOTENOTENOTENOTE:::: SOLVENT, OIL, LIQUID NITROGEN & COMPOUND REQUIRED, BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

140-8124-0004MAIN GEAR FAIRING ASSY ATA :

BAE/HAWKER MODELS 800, 800XP, U-125AAND 1000

ALL

THIS KIT PROVIDES PARTS AND INFORMATION FOR SHIPPING OF THE MAIN LANDING GEAR FAIRINGASSY FOR SPARES ONLY, USED ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: IDENTICAL TO S25-8UM50009A AND S25-8UM50010A WITH LATER MODIFICATIONS TO THEMAIN LANDING GEAR FAIRING ASSY ADDED. THE ATTACHING PARTS ARE LISTED INSEPERATE KIT.


140-9001-1APU SYSTEM - INFORMATION ONLY ATA :800XP 258414 AND AFTER EXCEPT 258416 AND

258417THIS KIT PROVIDES INFORMATION REQUIRED TO ACCOMMODATE INSTALLATION OF THE AUXILIARYPOWER UNIT (PATS) ON INSERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUALAMENDMENT P3 TO HS.1.22 FROM HAWKER PUBLICATIONS.


149-3011-0001INDICATORS FOR FUEL TEMP & FILTER ATA :800XP RG8266 & SUBSEQUENTTHIS KIT PROVIDES PARTS & INFORMATION NECESSARY TO INSTALL WIRE AND ADDED MAINTENANCEPANEL FOR FUEL FILTER BLOCKED AND OVERHEAT ON IN-SERVICE A/C.

NOTENOTENOTENOTE:::: "47386" CRIMP TOOL REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.


149-3411-0001STRUCTURAL PROVISIONS FOR INSTL OF CDU UNITS W/WEATHERGRAPHICS (822-1485-102)

ATA :

800XP RG-8541, RG-8556, RG-8567 & AFTER UP TOEFFECTIVITY OF ECR13789

THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL THE STRUCTURAL PROVISIONSIN THE CENTER INSTRUMENT PANEL FOR THE INSTALLATION OF THE ROCKWELL COLLINS CDU UNITSWITH THE WEATHER GRAPHICS CARD, (PART NUMBER 822-1485-102) FOR IN-SERVICE AIRCRAFTWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

149-3412-0001KIT INSTALLATION-DA-A C B INSTL,LOCATOR ATA : 24800XP 8541, 8556, 8567 AND SUB TO 8608"MANDATORY" SB NO. 24-3555 REV 1THIS KIT PROVIDES PARTS & INFORMATION NECESSARY TO MODIFY THE WIRING AND BUSSING OFCIRCUIT BREAKER PANEL DA-A FOR HAWKER 800XP, COLLINS PROLINE 21 EQUIPPED IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: NOTE: INSERT 140-590032-005TC5, TEMPORARY CHANGE PAGE, TO AFM AT PAGE 17.CONTACT RAYTHEON AIRCRAFT COMPANY TECHNICAL PUBLICATIONS DEPARTMENTFOR INSERT.

NOTENOTENOTENOTE:::: THIS KIT REPLACES 149-3410-0001WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : PART 1: 18 HRS. (1 MAN) PART 2: 6 HRS. (1 MAN)MEN : 1 (MAN)

149-3413-0001KIT-BUSSING UPGRADE, FUEL STATUS DISPLAY ATA : 24800XP 258541,258556,258567 THROUGH 258669"OPTIONAL" SB NO. 24-3641THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE WIRING AND BUSSING OFCIRCUIT BREAKER PANEL DA-A AND DA-D FOR THE HAWKER 800XP, COLLINS PROLINE 21 EQUIPPEDAIRCRAFT. THIS WILL ENABLE THE DISPLAY OF FUEL QUANTITY ON THE LEFT CDU WHEN THE R

NOTENOTENOTENOTE:::: AA-52080-B-3","MIL-T-43435" TYPEII,SIZE3,FIN C & "MIL-T-43435" TYPE 1,SIZE3,FIN B NYLONTYING TAPE, "MS3367-4-9" & "MS3367-1-9" TIE DOWN STRAP & "47386" OR"M22520/5/01"&"M22520/5-100" DIE CRIMP TOOL.


149-3414-0001AUDIO PANEL UPDATE ATA :HAWKER 800XP FOR COLLINS PROLINE 21 CONFIGURED -

RG258541, RG258556 & RG258567 THRURG258669

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN UPDATED AUDIO SELECTOR PANEL (P/N803-006, ADF2 INSTALLED) AND TO REWIRE THE OBSERVERS PANEL TO ALLOW RECEPTION OF THECOPILOT'S AUDIO. THIS KIT REQUIRES THAT THE AUDIO PANEL BE RETURNED TO NAT (NORTHE

NOTENOTENOTENOTE:::: "SN60WRMAP3" SOLDER REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED PILOT'S OPERATING MANUAL(POM) REVISION HAS BEEN INCORPORATED. MANUAL REVISION MAY BE OBTAINEDFROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

149-3414-0003AUDIO PANEL UPDATE ATA :FOR COLLINS PROLINE 21 CONFIGUREDHAWKER 800XP

RG258541, RG258656, & RG258567 & AFTERUP TO THE EFFECTIVITY OF ECR 13790.

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN UPDATED AUDIO SELECTOR PANEL (P/N803-005, HF2 INSTALLED) AND TO REWIRE THE OBSERVERS PANEL TO ALLOW RECEPTION OF THECOPILOT'S AUDIO.






THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN UPDATED AUDIO SELECTOR PANEL (P/N803-006, ADF2 INSTALLED) AND TO REWIRE THE OBSERVERS PANEL TO ALLOW RECEPTION OF THECOPILOT'S AUDIO.






THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN UPDATED AUDIO SELECTOR PANEL (P/N803-007, HF2 & ADF2 INSTALLED) AND TO REWIRE THE OBSERVERS PANEL TO ALLOW RECEPTION OFTHE COPILOT'S AUDIO.





KIT CATALOG

149-3414-0009AUDIO PANEL UPDATE ATA :HAWKER 800XP FOR COLLINS PROLINE 21 CONFIGURED

RG258541, RG258556 & RG258567 THRURG258669

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN UPDATED AUDIO SELECTOR PANEL (P/N803-005, HF2 INSTALLED) AND TO REWIRE THE OBSERVERS PANEL TO ALLOW RECEPTION OF THECOPILOT'S AUDIO. THIS KIT REQUIRES THAT THE AUDIO PANEL BE RETURNED TO NAT (NORTHER





RG258541, RG258556 & RG258567 THRURG258669

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN UPDATED AUDIO SELECTOR PANEL (P/N803-006, ADF2 INSTALLED) AND TO REWIRE THE OBSERVERS PANEL TO ALLOW RECEPTION OF THECOPILOT'S AUDIO. THIS KIT REQUIRES THAT THE AUDIO PANEL BE RETURNED TO NAT (NORTHE




149-3417-0001COLLINS TDR-94D MODE S ENHANCED SURVEILLANCE UPGRADE ATA :

800XP RG-258541, 258556, 258567 THRU 258609,258611 THRU 258628, 258630 THRU 258684,258686 THRU 258716

"O"S.B.34-3717THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO MODIFY THE TDR-94D TRANSPONDERSAND THE IOC-3100 INPUT/OUTPUT CONCENTRATOR-IAPS CIRCUIT CARDS TO PROVIDE MODE STRANSPONDER ENHANCED SURVEILLANCE CAPABILITIES ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-T-43435" DACRON TYING TAPE, "MIL-T-43435""AA-52080-B-3" NYLON TYING TAPE,"MS3367-4-9" TIE DOWN STRAP (MINIATURE) "MS3367-1-9" TIE DOWN STRAP (STANDARD),"M83519/2-8" SHIELD TERMINATION, "M81714/17-D33" TERMINAL JUNCTION,"M39029/1-507""FC120N2""372-2514-110" CONTACT REQUIRED, BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT MAINTENANCEMANUAL AND CREW MANUAL HAVE BEEN INCORPORATED. MANUALS MAY BE OBTAINEDFROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

149-3418-0001ELEMENTARY SURVEILLANCE FLIGHT ID UPGRADE-INFO ONLY ATA : 34HONEYWELL CONFIGURED MODEL 800XP RG-258366 THRU RG-258540, RG-258542

THRU RG-258555, RG-258557 THRURG-258566

THIS KIT PROVIDES INFORMATION TO UPGRADE THE MODE S TRANSPONDERS FOR ELEMENTARYSURVEILLANCE (FLIGHT ID).

NOTENOTENOTENOTE:::: HAWKER 800XP AIRCRAFT WHICH HAD THE RCZ-833E (P/N 7510700-766) OR RCZ-851E (P/N 7510700-806) OR RCZ-833E (P/N 7510700-866) INTEGRATED COMM UNITS MODIFIED PERRAC SB 23-3263 AND HAVE A TCAS II WITH CHANGE 7 SYSTEM INSTALLED IN THEAIRCRAFT.


149-3419-0001COLLINS FMS-6000 FLIGHT MGMT SYS V.3.0.3 UPDATE-INFO ONLY ATA :800XP RG258541, RG258556, RG258567 THRU

RG258669, AND RG258670 THRU RG258716,RG258718 THRU RG258722

THIS KIT PROVIDES INFORMATION TO UPGRADE THE ROCKWELL COLLINS FLIGHT MANAGEMENTSYSTEM TO SOFTWARE VERSION 3.0.3. WHICH INCLUDES IMPROVEMENTS AND ISSUE CORRECTIONSIDENTIFIED SINCE DELIVERY OF FMS VERSION 2.2 SOFTWARE. THIS KIT IS PROVIDED FOR PROLINE 21CONFIGURED IN-SERVICE HAWKER 800XP, THAT HAVE S.B. 34-3642 INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

149-3419-0003COLLINS FMS-6000 FLIGHT MGMT SYS V.3.0.3 UPDATE-INFO ONLY ATA :800XP RG258541, RG258556, AND RG258567 THRU

RG258669THIS KIT PROVIDES INFORMATION TO UPGRADE THE ROCKWELL COLLINS FLIGHT MANAGEMENTSYSTEM TO SOFTWARE VERSION 3.0.3. WHICH INCLUDES IMPROVEMENTS AND ISSUE CORRECTIONSIDENTIFIED SINCE DELIVERY OF FMS VERSION 2.0.1 SOFTWARE. THIS KIT IS PROVIDED FOR PROLINE 21CONFIGURED IN-SERVICE HAWKER 800XP THAT DO NOT HAVE SERVICE BULLETIN 34-3642 INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

149-3421-0001RELOCATION OF ARTEX C406-2 E.L.T. ATA :

HAWKER 800XP/850XP WITH PROLINE 21 EQUIPPED AIRCRAFTTHIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE ARTEX C406-2 E.L.T. FROM AFT OF FRAME25 TO BETWEEN FRAMES 23 & 24 OF IN-SERVICE AIRCRAFT.



KIT CATALOG

149-3601-1AURAL WARN,FLAP AILERON & ELEVATOR INSTALLATION ATA : 31

HAWKER MODEL XP 258541, 258556, 258567 & AFTER EQUIPPEDWITH COLLINS PROLINE 21 AVIONICS.

"0" SB #31-3703 REV 1THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO WIRE THE FLAPS, AILERONS & ELEVATORINTO SHIPS AURAL WARN SYSTEM FOR TAKE OFF CONFIGURATION FOR COLLINS PRO LINE EQUIPPEDAIRCRAFT FOR REGISTRATION IN ISRAEL.

NOTENOTENOTENOTE:::: "M22759/16-22-9" WIRE REQUIRED BUT NOT FURNISHED WITH KIT.

PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : MAN/HRS: 12 HRS.MEN : 1 (MAN)

149-9100-1INSTL TURBINE VIBRATION IND SYS ATA :HAWKER 800XP COLLINS PROLINE 21 EQUIPPED AIRCRAFTTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL A TURBINE VIBRATIONINDICATOR SYSTEM FOR 800XP COLLINS PROLINE 21 EQUIPPED AIRCRAFT

NOTENOTENOTENOTE:::: "MS20995C32" SAFETY WIRE; "M22759/16-14-9" WIRE 14GA, "M22759/16-20-9" WIRE 20GA,&"M22759/16-22-9" WIRE 22GA REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURESEPERATLY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : 6.08 LBS. MOMENT: -1.2125 FT.EST. MAN/HRS: : 170 HRSMEN : 2 (MEN)

25-7-Y19 AB800 SRS TOOL KIT ATA : 12WT. CHANGE : N/AEST. MAN/HRS: : N/AMEN : N/A

401-3010-0001AUDIO/OXYGEN/LIGHTING ATA :HAWKER 4000 RC-12 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A OBSERVER SEAT AND ASSOCIATEDOXYGEN, LIGHTING, AUDIO AND ECS SYSTEMS.

NOTENOTENOTENOTE::::

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT TECH SUPPORTMEN : N/A


KIT CATALOG

401-3010-0003OBSERVER SEAT - SYSTEMS INSTALLATION ATA :HAWKER 4000 RC-12 AND AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A OBSERVER SEAT AND ASSOCIATEDOXYGEN, LIGHTING, AUDIO AND ECS SYSTEMS.


401-3011-0007KIT - AUDIO PANEL AND MUTE ATA : 23HAWKER 4000 RC-7 THROUGH RC-29THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE CABIN AUDIO MUTE SYSTEM AND NEWAUDIO PANEL ASSEMBLIES IN THE COCKPIT SIDE CONSOLES.


401-4000-0001GROSS WEIGHT INCREASE 39,500 LB ATA : 01HAWKER 4000 RC-7 THROUGH RC-28THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE HORIZONTAL STABILIZER, THE TORQUEKNEE FITTINGS, THE LOWER WIPER PLATES AND THE PIVOT PINS AND SLEEVES. PARTS ANDINFORMATION ARE PROVIDED TO REINFORCE THE FORWARD VERTICAL SPAR. THIS KIT ALSO PROVIDESREQUIRED SOFTWARE CHANGES AND REFERS TO MESSIER-DOWTY AND HBC SERVICE BULLETINS FORWORK REQUIRED ON THE MAIN LANDING GEARS. THIS IS TO ACHIEVE GROSS WEIGHT INCREASE TO39,500 POUNDS.

EST. MAN/HRS: : 132MEN : 2 (MEN)

401-4000-0003GROSS WEIGHT INCREASE 39,500 POUNDS ATA : 01HAWKER 4000 RC-7 THROUGH RC-28THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE HORIZONTAL STABILIZER, THE TORQUEKNEE FITTINGS, THE LOWER WIPER PLATES AND THE PIVOT PINS AND SLEEVES. PARTS ANDINFORMATION ARE PROVIDED TO REINFORCE THE FORWARD VERTICAL SPAR. THIS KIT ALSO PROVIDESREQUIRED SOFTWARE CHANGES AND REFERS TO MESSIER-DOWTY AND HBC SERVICE BULLETINS FORWORK REQUIRED ON THE MAIN LANDING GEARS. THIS IS TO ACHIEVE GROSS WEIGHT INCREASE TO39,500 POUNDS.EST. MAN/HRS: : 132MEN : 2 (MEN)


KIT CATALOG

401-4001-0001PROVISIONS INSTL CIRCUIT BREAKER ATA :HAWKER 4000 RC-7 THROUGH RC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL A NEW BRACKET MAKING CONNECTORS(J1206) AND (J1207) MORE ACCESSIBLE FOR IN-SERVICE MODEL 4000 SERIALS: RC-7 THROUGH RC-20


401-4002-0001SHROUD REWORK, WHEEL WELL, MLG ATA :HAWKER 4000 RC-4 THROUGH RC-27THIS KIT PROVIDES PARTS AND INFORMATION TO REWORK MAIN LANDING GEAR WHEEL WELL SHROUDSAND ADD GROMMETS. THIS KIT IS REQUIRED WHEN MESSIER DOWTY 32000-115/-116 (OR HIGHER DASHNUMBER) MAIN LANDING GEARS ARE INSTALLED.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT TECH SUPPORTMEN : N/A

401-5501-0001GASKET FABRICATION AND REPLACEMENT ATA :HAWKER 4000 RC-7 THROUGH RC-20THIS KIT PROVIDES INFORMATION REQUIRED TO FABRICATE AND MODIFY THE INSTALLATION OF PSUGASKETS IN THE CABIN.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT TECH SUPPORTMEN : N/A

401-9000-0001FUEL SYSTEM ICING INHIBITOR ELIMINATION ATA : 73HAWKER 4000 RC-5 THROUGH RC-22THIS KIT PROVIDES PARTS AND INFORMATION REQUIRED FOR ELIMINATION OF THE REQUIREMENT OFFUEL SYSTEM ICING INHIBITOR FOR IN SERVICE MODEL: 4000 SERIALS RC-5 THROUGH RC-22

WT. CHANGE : +3.5 LBS BALANCE +1,879.0 LBS - IN ACCORDANCE WITH SB 73-3903EST. MAN/HRS: : 40MEN : 2 (MEN)

401-9012-0001INSTALLATION - FUEL WIRING SEPARATION ATA :HAWKER 4000 RC7, RC9-RC11 AND RC-20THIS KIT PROVIDES PARTS AND INFORMATION TO SEPARATE FUEL WIRING HARNESSES AND INSTALLRED CONVOLUTED TUBING TO ENCOMPASS THE FUEL WIRING HARNESSES.



KIT CATALOG

401-9013-0001EME SUPPRESION INSTALLATION KIT ATA :HAWKER 4000 RC-7, RC-9, RC-10, RC-11, AND RC-20THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL EME SUPPRESION PROVISIONS TO THE WINGWIRING AND FUEL QUANTITY PROBES.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT TECH SUPPORTMEN : N/A



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberJACKPAD ATTACHMENT INSTALLATION, LH - (390-1100-0001) 1

JACKPAD ATTACHMENT INSTALLATION, RH - (390-1100-0002) 1

AILERON TRIM ACTUATOR - (390-1300-0001)

1

AILERON TRIM ACTUATOR - (390-1300-0002) 1

RVSM PLACARDS FOR LIMITATIONS - (390-3202-0) 1

RVSM PITOT SYSTEM INSTALLATION - (390-3203-0001) 2




VSM PITOT SYSTEM INSTALLATION - (390-3203-0013) 4

ESCUTCHEON ASSY INSTL, TERMINAL BLOCK - (390-3204-0001) 4

GROUP RVSM APPROVAL - (390-3205-0001) 4

ADC RELOCATION - (390-3208-0001) 5

STANDBY ALTIMETER INDICATOR REPL-INFO ONLY - (390-3211-0001) 5

PARKING BRAKE INSTL - (390-3220-0001) 5

DME #2 ANTENNA INSTL - (390-3400-0003) 5

"S" RELOCATION OF ADF NO. 1 CIRCUIT BREAKER - (390-3401-0001) 6

VHF COMM ANTENNA INSTL UPPER & LOWER - (390-3402-0001) 6

SPIGOT BEARING RETAINER INSTALLATION - (390-3404-0001) 6

FMS NO. 2 INSTALLATION - (390-3406-0001) 6

AHRS UPGRADE - INFORMATION ONLY - (390-3410-0001) 7

AUDIO AURAL WARNING TONE VOLUME CHANGE-INFO ONLY - (390-3411-0001)

7

ENHANCED FLIGHT ID UPGRADE-INFO ONLY - (390-3412-0001) 7

ENHANCED FLIGHT ID UPGRADE-INFO ONLY - (390-3412-0003) 7

ENHANCED FLIGHT ID UPGRADE-INFO ONLY - (390-3412-0005)

8

LIGHTING INSTL COCKPIT CONTROL OF CABIN - (390-3604-1) 8

LIFT DUMP ACTUATION - (390-3607-0001) 8

DC GENERATOR WIRING CHANGE-INFO ONLY - (390-3608-0001) 8

REMOTE ENTRY RELOCATION - (390-3612-0001) 9

REMOTE ENTRY RELOCATION - (390-3612-0005) 9

EL LIGHT WIRE SHIELDING-INFO ONLY - (390-3615-0001) 9

EL LIGHT WIRE SHIELDING-INFO ONLY - (390-3615-0003) 10

ELECTRICAL POWER- HYDRAULIC SHUTOFF VALVE WIRING IMPROVEMENT KIT

- (390-3622-0001)

10

ELECTRICAL POWER- HYDRAULIC SHUTOFF VALVE WIRING IMPROVEMENT KIT - (390-3622-0003)

10



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage Number"S" LIGHTNING DIVERTER STRIP INSTALLATION - (390-4100-0001) 11

DOOR ADJUSTMENT,FWD BAGGAGE - (390-4101-0001) 11

FWD PRESSURE BULKHEAD, REINFORCEMENT INSTL - (390-4102-0001) 11

WING ATTACH POTTING INSTL - (390-4300-0001) 12

LATCH RECIEVER, CABIN DOOR - (390-4301-0001) 12

CABIN WINDOW, INSTL. - (390-4302-0023) 12

ESCAPE HATCH WINDOW REPL INSTL - (390-4303-0001)

12

ESCAPE HATCH WINDOW REPL INSTL - (390-4303-0003) 13

SPIGOT BEARING RETAINER INSTALLATION - (390-4304-0001) 13

CABIN DOOR SWITCH BRACKET REPLACEMENT - (390-4305-0001)

13

CABIN DOOR SWITCH BRACKET REPLACEMENT - (390-4305-0003) 13

PYLON SKIN INSTALLATION - (390-4401-0001) 14

FAIRING INSTALL, FUSELAGE - (390-4402-0001) 14

AFT BAGGAGE/MAINTENANCE DOOR LATCH REPLACEMENT INSTL - (390-4403-0001) 14

SPOILER PANEL, FILLER REWORK INSTL - (390-4404-0001)

15

SPOILER PANEL, FILLER REWORK INSTL - (390-4404-0002)

15

SPOILER PANEL HINGE BRACKET FITTING INSTL - (390-4405-0001) 15

SPOILER PANEL HINGE BRACKET FITTING INSTL - (390-4405-0002) 16

"R" LEVER ASSEMBLY INSTALLATION - (390-5200-0001) 16

STIFFNER INSTL, TEE COLUMN ASSY, - (390-5201-0001) 16

ACCOUSTIC INSULATION - (390-5302-0007) 16

ACOUSTIC INSULATION - (390-5306-0001) 17

SIDEWALL INSULATION - (390-5309-0001) 17

SUPPLEMENTAL INTERIOR/EXTERIOR MARKINGS-UK - (390-5312-0001) 17

RAM AIR SYSTEMS INSTL. - (390-5540-0) 17

DRAIN INSTALLATION, RAM AIR SYSTEM - (390-5541-0001) 18

AFT FUSE FWD SEC,ECS PROV INSTL - (390-5550-0001) 18

GROUND SERVICE PRESSURE FILTRATION - (390-5800-0001) 18

GROUND SERVICE PRESSURE FILTRATION - (390-5800-0005) 18

OVERBOARD DRAIN WEEPAGE REDUCTION - (390-5802-0001) 19

HYDRAULIC CASE DRAIN CHECK VALVE INSTL - (390-5803-0001)

19

DAMPENER SUPPORT IMPROVEMENT - (390-5804-0001) 19

HYDRAULIC PUMP PRESSURE HOSE INSTALLATION - (390-5805-0001) 20

MASTER CYLINDER IMPROVEMENT - (390-5807-0001) 20

HYDRAULIC PULSE DAMPENER INSTL. - (390-9100-0) 20



Title - (Kit Number)Title - (Kit Number)Title - (Kit Number)Title - (Kit Number) Page NumberPage NumberPage NumberPage NumberTMA INSTALLATION, ENG MOUNT. - (390-9101-0) 20

TMA INSTALLATION - (390-9101-0001) 21

CLEARANCE DEFINITION, ENGINE BUILDUP - (390-9104-0003) 21

CLEARANCE DEFINITION, ENGINE BUILDUP - (390-9104-0005)

21

UNUSABLE FUEL REDUCTION - (390-9200-0001) 22




TEE ASSY. REPLACEMENT, SINGLE POINT - (390-9201-0001) 23

FUEL SENSOR TO ACCESS DOOR RELOCATION - (390-9202-0001) 23

DRAIN PROVISIONS FORWARD & AFT WHEEL WELL VAPOR BOX-INFO ONLY - (390-9203-0001) 23

FUEL TRANSFER SYSTEM - (390-9204-0001) 24

PNEUMATIC QUICK DRAIN INSTL - (390-9700-0001) 24


KIT CATALOG

390-1100-0001JACKPAD ATTACHMENT INSTALLATION, LH ATA : 07PREMIER 390 RB-1, RB-4 THROUGH RB-216, RB-218

THROUGH RB-225 & RB-227THIS KIT PROVIDES INFORMATION TO INSTALL THE JACK PAD ATTACHMENT ON THE LH WING, LOWERSKIN AND REAR SPAR AFT FLANGE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

390-1100-0002JACKPAD ATTACHMENT INSTALLATION, RH ATA : 07PREMIER 390 RB-1, RB-4 THROUGH RB-216, RB-218

THROUGH RB-225 & RB-227THIS KIT PROVIDES INFORMATION TO INSTALL THE JACK PAD ATTACHMENT ON THE RH WING, LOWERSKIN AND REAR SPAR AFT FLANGE.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8MEN : 1 (MAN)

390-1300-0001AILERON TRIM ACTUATOR ATA :

390 RB-1 AND RB-4 THRU RB-149THIS KIT PROVIDES PARTS AND INFORMATION TO PERFORM A ONE-TIME REPLACEMENT OF THE LEFT-HAND AILERON TRIM ACTUATOR P/N 390-381009-0005 OR -0007 WITH ACTUATOR P/N 390-381009-0009 ANDTO REPLACE THE ACTUATOR'S AIRCRAFT MATING CONNECTOR AND BACKSHELL WITH CONNECTORMS27473T10B35S AND BACKSHELL M85049/49-2S10W ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-1300-0002AILERON TRIM ACTUATOR ATA :390 RB-1 AND RB-4 THRU RB-149THIS KIT PROVIDES PARTS AND INFORMATION TO PERFORM A ONE-TIME REPLACEMENT OF THE RIGHT-HAND AILERON TRIM ACTUATOR P/N 390-381009-0006 OR -0008 WITH ACTUATOR P/N 390-381009-0010 ANDTO REPLACE THE ACTUATOR'S AIRCRAFT MATING CONNECTORS AND BACKSHELLS WITH CONNECTORMS27473T10B35S AND BACKSHELL M85049/49-2S10W ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3202-0RVSM PLACARDS FOR LIMITATIONS ATA : 34

RB-35 ONLYRB-24 ONLY



KIT CATALOG

390-3203-0001RVSM PITOT SYSTEM INSTALLATION ATA : 34PREMIER RB-19 THRU RB-42"R"SB #34-3581 REV 1THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO RELOCATE THE PITOT PROBES AND REWORK THEPITOT/STATIC SYSTEM TO IMPROVE THE ACCURACY OF THE ALTITUDE MEASURING SYSTEM FOR ALL IN-SERVICE AIRCRAFT WANTING RVSM CERTIFICATION.

NOTENOTENOTENOTE:::: PANEL IN KIT,390-530081-0005 IS GREY.

NOTENOTENOTENOTE:::: "822-1084-014" AFD, "822-1109-016" ADC, "390-3203-0009" SHIM,"EA9309NA""EA960""EA956""EA9394" ADHESIVE, "15350""PR1440" SEALER, &"ALODINE1200" CHEM FILM, "390-3203-0019" CORE & "390-3203-0021" OML REWORKLAMINATE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANYAUTHORIZED COMPANY OUTLET.


WT. CHANGE : +1.20 LBS; MOMENT: +144 LB-INEST. MAN/HRS: : .5 HR INSPECTION, 120 HRS.MEN : 2 (MEN)

390-3203-0003RVSM PITOT SYSTEM INSTALLATION ATA : 34390 RB-1 THRU RB-69"R"SB #34-3581 REV 1THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO RE-LOCATE THE PITOT PROBES AND REWORK THEPITOT/STATIC SYSTEM TO IMPROVE THE ACCURACY OF THE ALTITUDE MEASURING SYSTEM FOR ALL IN-SERVICE AIRCRAFT WANTING RVSM CERTIFICATION.



WT. CHANGE : +1.20 LBSMOMENT: +144 LB-INEST. MAN/HRS: : .5 HRS INSPECTION, 120 HRS.MEN : 2 (MEN)


KIT CATALOG

390-3203-0005RVSM PITOT SYSTEM INSTALLATION ATA : 34390 RB-1 THRU RB-69"R"SB #34-3581 REV 1THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO RE-LOCATE THE PITOT PROBES AND REWORK THEPITOT/STATIC SYSTEM TO IMPROVE THE ACCURACY OF THE ALTITUDE MEASURING SYSTEM FOR ALL IN-SERVICE AIRCRAFT WANTING RVSM CERTIFICATION.



WT. CHANGE : +1.20 LBS MOMENT: +144 LB-INEST. MAN/HRS: : .5 HR INSPECTION, 120 HRS.MEN : 2 (MEN)

390-3203-0007RVSM PITOT SYSTEM INSTALLATION ATA : 34390 RB-10, RB-29, RB-41 AND RB-48"R"S.B.#34-3581 REV 1THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO RE-LOCATE THE PITOT PROBES AND REWORK THEPITOT/STATIC SYSTEM TO IMPROVE THE ACCURACY OF THE ALTITUDE MEASURING SYSTEM FOR ALL IN-SERVICE AIRCRAFT WANTING RVSM CERTIFICATION.

NOTENOTENOTENOTE:::: PANEL, 390-530081-0007 CREAM.NOTENOTENOTENOTE:::: "822-1084-014" AFD, "822-1109-016" ADC, "390-3203-0009" SHIM,

"EA9309NA""EA960""EA956""EA9394" ADHESIVE, "15350""PR1440" SEALER, &"ALODINE1200" CHEM FILM, "390-3203-0019" CORE & "390-3203-0021" OML REWORKLAMINATE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANYAUTHORIZED COMPANY OUTLET.


WT. CHANGE : +1.20 LBS MOMENT: +144 LB-INEST. MAN/HRS: : .5 HR INSPECTION, 120 HRSMEN : 2 (MEN)


KIT CATALOG

390-3203-0013VSM PITOT SYSTEM INSTALLATION ATA : 34PREMIER 390 RB-1 THRU RB-69SB NO. 34-3581THIS KIT PROVIDES PARTS AND INSTRUCTIONS TO RE-LOCATE THE PITOT PROBES AND REWORK THEPITOT/STATIC SYSTEM TO IMPROVE THE ACCURACY OF THE ALTITUDE MEASURING SYSTEM FOR ALL IN-SERVICE AIRCRAFT WANTING RVSM CERTIFICATION.

NOTENOTENOTENOTE:::: "822-1084-014" AFD, "822-1109-016" ADC, "390-3203-0009" SHIM, "EA9309NA""EA960""EA956"ADHESIVE, "15350""PR1440" SEALER, & "ALODINE1200" CHEM FILM REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANY


WT. CHANGE : +1.20 LBSMOMENT: +144 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3204-0001ESCUTCHEON ASSY INSTL, TERMINAL BLOCK ATA :390 RB-4 THRU RB-41PREMIER COMMUNIQUE 3THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TERMINAL BLOCK ESCUTCHEON ASSYS FORIN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: CHEESE CLOTH & ALCOHOL OR ENVIRO CLEAN REQUIRED BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-3205-0001GROUP RVSM APPROVAL ATA : 34PREMIER RB-4 THRU RB-69SB NO. 34-3581THIS KIT PROVIDES THE OVERHEAD EL PANEL AND INSTRUCTIONS TO INSTALL IT, THAT INDICATE TOREFER TO AFM FOR RVSM LIMITATIONS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: 390-3203-0001, -0003, -0005, -0007 AND -0013 (OPTIONAL -1 EA REQUIRED). SEE KITDRAWING 390-3203 FOR APPROPRIATE KIT PART NUMBER.


WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : .5HR INSP/124 HRS COMPLMEN : N/A


KIT CATALOG

390-3208-0001ADC RELOCATION ATA : 34PREMIER 390 RB-1 & RB-4 THRU RB-69 (IF KIT

390-3203-0001,-0003,-0005,-0007, OR -0013HAS BEEN PREVIOUSLY INSTALLED) &RB-70 THRU RB-114.

SB NO. 34-3667

THIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE #2 ADC AND REWORK THE TUBINGSYSTEM TO ELIMINATE MOISTURE CONTAMINATION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "132370AD3" RIVET REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : MAN/HRS: 14 HRSMEN : 1 (MAN)

390-3211-0001STANDBY ALTIMETER INDICATOR REPL-INFO ONLY ATA :390 RB-4 & AFTERTHIS KIT PROVIDES INFORMATION TO REPLACE THE STANDARD STANDBY ALTIMETER INDICATOR WITH AMETRIC STANDBY ALTIMETER INDICATOR ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3220-0001PARKING BRAKE INSTL ATA : 32PREMIER RB-4 THRU RB-43"RECOMMENDED" SB NO. 32-3572THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE PARKING BRAKE LEVER IN THEPEDESTAL IN LIEU OF THE ORIGINAL PART.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 10MEN : 1 (MAN)

390-3400-0003DME #2 ANTENNA INSTL ATA :390 RB-4 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DME #2 (OPTION CODE 0020) FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "PR1428" SEALANT, "VV-P-236" PETROLEUM, & "EA9309NA" ADHESIVE REQUIRED, BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : WT: +8.4 LBS. MOMENT: +1068 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

390-3401-0001"S" RELOCATION OF ADF NO. 1 CIRCUIT BREAKER ATA : 34390 RB-2 THRU RB-31THIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE ADF NO. 1 CIRCUIT BREAKER FROMLMB TO ESSENTIAL BUS FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3402-0001VHF COMM ANTENNA INSTL UPPER & LOWER ATA : 34390 RB-2 THRU RB-61"RECOMMENDED" SB NO. 23-3583THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW VHF COMM ANTENNA ON BOTH UPPERAND LOWER AFT LOCATIONS. ALSO ADDS STATIC DISCHARGERS AND OTHER IMPROVEMENTS TOREDUCE OVER ALL P-STATIC BUILDUP ON AIRCRAFT. TO AGREE WITH FLEET CONFIGURATION FOR IN-

NOTENOTENOTENOTE:::: "16307" EPOXY, "EA9394" ADHESIVE, "ALODINE 1200; "VV-P-236" COATING,"PR-1428""PR-1440" SEALANT, "390-3402-0007""390-3402-0009" FILLER REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : +2.50 LBSMOMENT:+1109 LB-INEST. MAN/HRS: : 80MEN : 2 (MEN)

390-3404-0001SPIGOT BEARING RETAINER INSTALLATION ATA : 53390 RB-1, RB-4 THRU RB-139"M"S.B.53-3765THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE SPIGOT BEARING RETAINERS TOPROVIDE MECHANICAL BEARING RETENTION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "G-N312G" G-N METAL ASSEMBLY SPRAY LUBRICANT & "MIL-S-8802" SEALANT REQUIREDBUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 HRS FOR INSPECTION, 8 HRS TO INSTALL KITMEN : 1 (MAN)

390-3406-0001FMS NO. 2 INSTALLATION ATA : 34390 RB-2 & AFTERTHIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL AN OPTIONAL FLIGHT MANAGEMENTCOMPUTER TO AGREE WITH FLEET CONFIGURATION ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR-1422""PR1426" SEALANT, "VV-P-236" LUBRICANT, "EA9309" ADHESIVE, "1200 ALODINE"CHEM FILM, "CE1164" CONFORMAL COATING, "MEK" OR EQUIVALENT CLEANINGSOLVENT, "MS3367-5-9" TIE STRAPS, 180 GRIT SANDPAPER, 320 GRIT OR FINER GARNETPAPER, "822-0883-701" FMC-3000 LRU, & "822-1377-001" GPS RECEIVER REQUIRED, BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : 9/2 LBS MOMENT: 1324 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

390-3410-0001AHRS UPGRADE - INFORMATION ONLY ATA :390 RB-4, AND RB-6 THRU RB-9PR-CSL-1005 APRIL '05THIS KIT PROVIDES INFORMATION TO UPGRADE THE ATTITUDE HEADING REFERENCE SYSTEM ON IN-SERVICE AIRCRAFT. 1 PER AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 8 HRSMEN : 1 (MAN)

390-3411-0001AUDIO AURAL WARNING TONE VOLUME CHANGE-INFO ONLY ATA :

PREMIER 390 RB-4 THRU RB-134THIS KIT PROVIDES INFORMATION TO LOWER THE AUDIO AURAL WARNING TONE VOLUME LEVELS, ANDTO MATCH COCKPIT SPEAKER VOLUME TO HEADSET VOLUME ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3412-0001ENHANCED FLIGHT ID UPGRADE-INFO ONLY ATA : 34390 RB-4 THRU RB-101 & RB-103 THRU RB-134

THAT HAVE ELEMENTARY FLIGHT IDINSTALLED

"O"S.B.34-3730THIS KIT PROVIDES INFORMATION TO REPLACE AIRCRAFT AVIONICS HARDWARE FOR IN-SERVICEAIRCRAFTWT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

390-3412-0003ENHANCED FLIGHT ID UPGRADE-INFO ONLY ATA : 34390 RB-4 THRU RB-101 & RB-103 THRU RB-134

THAT DO NOT HAVE ELEMENTARY FLIGHTID INSTALLED

"O"S.B.34-3730THIS KIT PROVIDES INFORMATION TO REPLACE AIRCRAFT AVIONICS HARDWARE FOR IN-SERVICEAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)


KIT CATALOG

390-3412-0005ENHANCED FLIGHT ID UPGRADE-INFO ONLY ATA : 34

390 RB-135 & AFTER THAT DO NOT HAVEFLIGHT ID INSTALLED

"O"S.B.34-3730THIS KIT PROVIDES INFORMATION TO INSTALL AIRCRAFT AVIONICS HARDWARE FOR IN-SERVICEAIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : 8MEN : 1 (MAN)

390-3604-1LIGHTING INSTL COCKPIT CONTROL OF CABIN ATA : 33390 RB-2 - RB-50THIS KIT PROVIDES PARTS & INFORMATION TO INSTALL THE COCKPIT CONTROL OF CABIN LIGHTING TOAGREE WITH FLEET CONFIGURATION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "ALODINE 1200" CHEM FILM, "CE1164" CONFORMAL COATING, MEK OR EQUIVALENTCLEANING SOLVENT & GARNET PAPER 320 GRIT OR FINER REQURIED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


390-3607-0001LIFT DUMP ACTUATION ATA : 27390 RB-1 AND RB-4 THRU RB-99"MANDATORY" SB NO. 27-3606THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL LIFT DUMP ACTUATIONHARDWARE AND WIRING TO AGREE WITH FLEET CONFIGURATION ON IN-SERVICE AIRCRAFT.WT. CHANGE : 5.3 LBSMOMENT: 1126 IN-LBS.EST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3608-0001DC GENERATOR WIRING CHANGE-INFO ONLY ATA : 24390 S/N RB-75 & AFTERTHIS KIT PROVIDES INFORMATION TO MODIFY AIRCRAFT WIRING FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

390-3612-0001REMOTE ENTRY RELOCATION ATA : 33390 RB-4 THRU RB-40 MODIFIED BY 390-3601;

RB-41 THRU RB-83, RB-85 THRU RB-95 ANDRB-97 TO THE EFFECTIVITY OF EC89147.

THIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE COURTESY LIGHT CONTROLLER TOTHE RADOME BULKHEAD IN ORDER TO IMPROVE COURTESY LIGHT ACTIVATION DISTANCE WITH THEREMOTE TRANSMITTER FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-P-23377" PRIMER, ISOPROPYL ALCOHOL, "ALODINE 1200" REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

NOTENOTENOTENOTE:::: WITCH ASSEMBLIES: SEE TABLE VII FOR: POLISHED ALUMINUM, CHROME, 14K GOLD,SMOKED NICKEL, CHAMPAGNE GOLD, BRASS, COPPER, OR NICKEL FINISH, NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : +0.6 LB. MOMENT: 64 LB-IN.EST. MAN/HRS: : 40MEN : 1 (MAN)

390-3612-0005REMOTE ENTRY RELOCATION ATA : 33390 RB-4 THRU RB-119 & RB-121THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE COURTESY LIGHT CONTROLLER TOALLOW SYSTEM ACTIVATION WITH THE REMOTE TRANSMITTER ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "MIL-P-23377" PRIMER, ISOPROPYL ALCOHOL, "ALODINE 1200" PROTECTIVE COATINGREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: SWITCH ASSEMBLIES: SEE TABLE VII FOR: POLISHED ALUMINUM, CHROME, 14K GOLD,SMOKED NICKEL, CHAMPAGNE GOLD, BRASS, COPPER, OR NICKEL FINISH, NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.

WT. CHANGE : +1.2 LB MOMENT: +80 LB-INEST. MAN/HRS: : MAN/HRS: 30 HRSMEN : 1 (MAN)

390-3615-0001EL LIGHT WIRE SHIELDING-INFO ONLY ATA :390 RB-1 & RB-4 THRU RB-109. 107 A/CTHIS KIT PROVIDES INFORMATION TO REPLACE TWO WIRE SEGMENTS IN THE ELECTRO-LUMINESCENTLIGHTS DIMMING CIRCUIT WITH SHIELDED WIRES, IN ORDER TO REDUCE RF INTERFERENCE WITH THEEL LIGHT PANELS ON THE SUBPANEL, PEDESTAL & COCKPIT CB PANELS ON IN-SERVICE AIRCRWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

390-3615-0003EL LIGHT WIRE SHIELDING-INFO ONLY ATA :390 RB-110 THRU RB-134, SERIALS WHICH

PREVIOUSLY HAD SHIELDING TO THE DIMCONT WIPER, ONLY.

THIS KIT PROVIDES INFORMATION TO REPLACE TWO WIRE SEGMENTS IN THE ELECTRO-LUMINESCENTLIGHTS DIMMING CIRCUIT WITH SHIELDED WIRES, IN ORDER TO REDUCE RF INTERFERENCE WITH THEEL LIGHT PANELS ON THE SUBPANEL, PEDESTAL & COCKPIT CB PANELS ON IN-SERVICE AIRCRWT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-3622-0001ELECTRICAL POWER- HYDRAULIC SHUTOFF VALVE WIRINGIMPROVEMENT KIT

ATA : 24

MODEL 390 PREMIER 1 SERIALS RB-4 THROUGH RB-10, RB-12THROUGH RB-101, RB-103 THROUGHRB-134

REF SB 24-3868THIS KIT PROVIDES PARTS AND INFORMATION TO INCREASE THE HYDRAULIC VALVE MOTOR CIRCUITWIRE SIZE TO REDUCE VOLTAGE DROP IN THE CIRCUIT. THIS KIT ALSO MOVES EIGHT CIRCUITBREAKERS IN THE PILOT'S CIRCUIT BREAKER PANEL FROM THE STAND-BY TO THE ESSENTIAL BUS TORAISE CIRCUIT OPERATING VOLTAGES.NOT FURNISHED WITH THIS KIT PROCURE LOCALLY: TORQUE SEAL: F900 GREEN

MEN : N/A

390-3622-0003ELECTRICAL POWER- HYDRAULIC SHUTOFF VALVE WIRINGIMPROVEMENT KIT

ATA : 24

MODEL 390 PREMIER 1A SERIALS RB-102, RB-135 THROUGH RB-259REF SB 24-3868THIS KIT PROVIDES PARTS AND INFORMATION TO INCREASE THE HYDRAULIC VALVE MOTOR CIRCUITWIRE SIZE TO REDUCE VOLTAGE DROP IN THE CIRCUIT. THIS KIT ALSO MOVES EIGHT CIRCUITBREAKERS IN THE PILOT'S CIRCUIT BREAKER PANEL FROM THE STAND-BY TO THE ESSENTIAL BUS TORAISE CIRCUIT OPERATING VOLTAGES.NOT FURNISHED WITH THIS KIT PROCURE LOCALLY: TORQUE SEAL: F900 GREENMEN : N/A


KIT CATALOG

390-4100-0001"S" LIGHTNING DIVERTER STRIP INSTALLATION ATA : 53

RB-4 THRU RB-15RB-19 THRU RB-32

PREMIER 390 RB-34"MANDATORY" SB NO. 53-3526, JULY, 2002THIS KIT PROVIDES INSTRUCTIONS AND PARTS TO REPLACE LIGHTNING DIVERTER STRIPS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: URETHANE TOP COATING, "3M86" ADHESIVE PROMOTOR, "910-464" CATALYST, "528-306"ANTISTATIC PAINT, "EA9309NA" ADHESIVE & 181 GLASS CLOTH REQUIRED BUT NOTFURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZEDOUTLET.


390-4101-0001DOOR ADJUSTMENT,FWD BAGGAGE ATA : 52390 RB-10 THRU RB-36THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR DOOR ADJUSTMENT ON ALL IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: SCOTCH-BRITE SCOURING PAD, "EA9309" ADHESIVE, & "MS20995C32" SAFETY WIREREQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE FROM ANY AUTHORIZEDCOMPANY OUTLET.


390-4102-0001FWD PRESSURE BULKHEAD, REINFORCEMENT INSTL ATA : 53390 RB-64390 RB-17 THRU RB-58390 RB-4 THRU RB-15390 RB-1"MANDATORY" SB NO. 53-3620THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY FOR BULKHEAD REINFORCEMENT ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "5302" SCRIM CLOTH, "LOCTITE 7452" ACCELERATOR, "LOCTITE 609" RETAININGCOMPOUND, SCOTCH-BRITE SCOURING PAD, "PR-1440" SEALANT, "EA9309 NA"ADHESIVE,"MS20426AD5-2""MS20470AD3-3""MS20426AD3-3""MS20470AD6-6""MS20470AD6-3" RIVETSREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPARATELY FROM COMPANYAUTHORIZED OUTLET.

WT. CHANGE : WT. +6.0 LBS.MOMENT:+723 LB-IN.EST. MAN/HRS: : EST. MAN/HRS: 600 HRS.MEN : 2 (MEN)


KIT CATALOG

390-4300-0001WING ATTACH POTTING INSTL ATA : 53

RB-5 THRU RB-58"MANDATORY" SB NO. 53-3570THIS KIT PROVIDES TOOLS, PARTS & INFORMATION TO POT THE CORE AT THE WING ATTACH FITTINGFASTENERS.

NOTENOTENOTENOTE:::: "E300" RELEASE AGENT, "MIL-S-8802" ADHESIVE, & "EA9309" POTTING REQUIRED BUTNOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANYOUTLET.

WT. CHANGE : +2.2 LB. MOMENT: +610 LB.-IN.EST. MAN/HRS: : 50MEN : 2 (MEN)

390-4301-0001LATCH RECIEVER, CABIN DOOR ATA : 52390 RB-1 AND AFTER UP TO RB-58THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE AND REPLACE LATCH POSTS ANDECCENTRIC BUSHINGS IN THE CABIN DOOR LATCH, LATCH POSTS AND ECCENTRIC BUSHINGS IN THECABIN DOOR LATCH POSTS RECEIVERS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "NASM20995N32" SAFETY WIRE & "EA9359.3" ADHESIVE REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-4302-0023CABIN WINDOW, INSTL. ATA : 56390 RB-1, RB-4 THRU RB-79"RECOMMENDED" SB NO. 56-3584THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE AND REPLACE WINDOW CLAMPS FOR IN-SERVICE AIRCRAFT.WT. CHANGE : +11.6 LBSMOMENT: +3109 LBS-INEST. MAN/HRS: : 45MEN : 2 (MEN)

390-4303-0001ESCAPE HATCH WINDOW REPL INSTL ATA :

390 RB-1 THRU RB-15, RB-17 THRU RB-84THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EXISTING ESCAPE HATCH WINDOW WITHDRY-SEAL WINDOW FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "WL7400-.002" BAGGING FILM,"SCOTCH-BRITE" SCOURING PAD, "PR-1425" SEALANT,"LOCTITE 680" ADHESIVE, "LOCTITE PRIMER T" PRIMER, "CS213 1/8"X1/2"" BAG SEALANT,"EA9359.3" ADHESIVE, "AIRWEAVE N4" BREATHER PLY REQUIRED, BUT NOT FURNISHEDWITH KIT. PROCURE LOCALLY FROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

390-4303-0003ESCAPE HATCH WINDOW REPL INSTL ATA :390 RB-16, RB-85 THRU RB-114THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE EXISTING ESCAPE HATCH WINDOW WITHDRY-SEAL WINDOW FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "WL7400-.002" BAGGING FILM,"SCOTCH-BRITE" SCOURING PAD, "PR-1425" SEALANT,"CS213 1/8"X1/2"" BAG SEALANT, "EA9359.3" ADHESIVE, "AIRWEAVE N4" BREATHER PLYREQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE LOCALLY FROM ANY COMPANYAUTHORIZED OUTLET.


390-4304-0001SPIGOT BEARING RETAINER INSTALLATION ATA : 53390 RB-1, RB-4 THRU RB-139"M"S.B.53-3765THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL THE SPIGOT BEARING RETAINERS TOPROVIDE MECHANICAL BEARING RETENTION FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "G-N312G" G-N METAL ASSEMBLY SPRAY LUBRICANT & "MIL-S-8802" SEALANT REQUIREDBUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 2 HRS FOR INSPECTION, 14 HRS TO INSTALL KITMEN : 1 (MAN)

390-4305-0001CABIN DOOR SWITCH BRACKET REPLACEMENT ATA :

390 RB-1 THRU RB-165THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE SWITCH MOUNT BRACKET AND STRIKERPLATE.

NOTENOTENOTENOTE:::: NOTE: "MS20995C32" .032 SAFETY WIRE, "MIL-PRF-23827" LIGHT GREASE, "MIL-S-8802"SEALANT, & "EA956" ADHESIVE PASTE 2-PART EPOXY REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-4305-0003CABIN DOOR SWITCH BRACKET REPLACEMENT ATA :390 RB-166 THRU RB-174THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE SWITCH MOUNT BRACKET FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: NOTE: "MS20995C32" .032 SAFETY WIRE & "EA956" ADHESIVE PASTE 2-PART EPOXYREQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELY FROM ANYCOMPANY AUTHORIZED OUTLET.



KIT CATALOG

390-4401-0001PYLON SKIN INSTALLATION ATA : 25PREMIER RB-2 THRU RB-5PREMIER RB-7 THRU RB-53SB NO. 25-3582THIS KIT PROVIDES PARTS AND INFROMATION TO REMOVE AND REPLACE PYLON SKIN ASSEMBLIES ANDSEALS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "1500" ALODINE, "EA956" ADHESIVE, "DEVCON F" PRIMER, PAINT, "RTV106" AND "SILPAKA400" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPARATELYFROM ANY AUTHORIZED COMPANY OUTLET.

WT. CHANGE : +4.7 LB; MOMENT: +1899 LB-INEST. MAN/HRS: : 89 HRS COMPLMEN : N/A

390-4402-0001FAIRING INSTALL, FUSELAGE ATA :390 RB-4 THRU RB-134THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL DIELECTRIC RUBBER MAT ON THE LEFT,RIGHT AND CENTER FAIRINGS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "EC1300L""PR1440" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : WT: 22.84 LB - MOMENT: 5,955 LB-IN WITH SINGLE POINT:REFUELING, WT: 21.37 LB - MOMENT: 5,542 LB-INWITHOUT SINGLE POINT REFUELING


390-4403-0001AFT BAGGAGE/MAINTENANCE DOOR LATCH REPLACEMENT INSTL ATA : 52390 RB-4 THROUGH RB-10 AND RB-12

THROUGH RB-234REC SB 52-3864THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE CURRENT GOOSE NECK TYPE AFT BAGGAGEAND MAINTENANCE BAY LATCHES (4 EACH) WITH NEW ROTARY PIN STYLE LATCHES FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: THIS INSTALLATION IS NOT COMPLETE UNTIL THE NOTED AIRCRAFT FLIGHT MANUAL,PILOT OPERATING MANUAL OR PILOT CHECKLIST REVISION (OR SUPPLEMENT) HASBEEN INCORPORATED. MAY BE PROCURED SEPERATELY FROM ANY COMPANYAUTHORIZED OUTLET.

NOTENOTENOTENOTE:::: "52672" TAPE, GUIDELINE; "RTV-732" "AMS-S-8802" SEALANT; "1300L" "EA9309" ADHESIVE;"CA120 DESOCLEAN" PAINT PREP CLEANER; "Z97-01" ZO-MULTI PRIMER, WHITE; AND"20-54-1G" ZOLATONE COATING CAMILLE WHITE REQUIRED, BUT NOT FURNISHED WITHKIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +4.6 LBS. MOMENT: +1670 LB-INEST. MAN/HRS: : 40 HOURSMEN : 1 (MAN)


KIT CATALOG

390-4404-0001SPOILER PANEL, FILLER REWORK INSTL ATA : 27

390 RB-1, RB-4 THRU RB-101, RB-103 THRURB-119 & RB-121

"R"S.B.27-3783THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE SHORT FITTING ASSY OF THE COMPOSITESPOILER PANEL WITH THE LONG FITTING ASSY OF THE NEW METALLIC SPOILER PANEL FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.


390-4404-0002SPOILER PANEL, FILLER REWORK INSTL ATA : 27

390 RB-1, RB-4 THRU RB-101, RB-103 THRURB-119 & RB-121

"R"S.B.27-3783THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE SHORT FITTING ASSY OF THE COMPOSITESPOILER PANEL WITH THE LONG FITTING ASSY OF THE NEW METALLIC SPOILER PANEL FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: "EA9309" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.


390-4405-0001SPOILER PANEL HINGE BRACKET FITTING INSTL ATA :390 RB-1, RB-4 THRU RB-101, RB-103 THRU

RB-119 & RB-121THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE FITTING BRACKETS OF THE COMPOSITESPOILER PANEL WITH THE NEW FITTINGS FOR THE NEW METALLIC SPOILER PANELS FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: SHIM AND "EA9309NA" ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.



KIT CATALOG

390-4405-0002SPOILER PANEL HINGE BRACKET FITTING INSTL ATA :390 RB-1, RB-4 THRU RB-101, RB-103 THRU

RB-119 & RB-121THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE FITTING BRACKETS OF THE COMPOSITESPOILER PANEL WITH THE NEW FITTINGS FOR THE NEW METALLIC SPOILER PANELS FOR IN-SERVICEAIRCRAFT.

NOTENOTENOTENOTE:::: SHIM AND "EA9309NA" ADHESIVE REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-5200-0001"R" LEVER ASSEMBLY INSTALLATION ATA : 27

RB-19 THRU RB-27PREMIER RB-4 THRU RB-13"RECOMMENDED" SB 27-3515THIS KIT PROVIDES PARTS ANDINFORMATION NECESSARY TO INSTALL NEW LEVER ASSEMBLY ANDASSOCIATED HARDWARE FOR HORIZONTAL STABILIZER PITCH TRIM POSITION POTENTIOMETER FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-5201-0001STIFFNER INSTL, TEE COLUMN ASSY, ATA : 27

RB-4 THRU RB-57"RECOMMENDED" SB NO. 27-3571THIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO INSTALL STIFFENERS AND ASSOCIATEDHARDWARE FOR THE TEE COLUMN ASSY FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-5302-0007ACCOUSTIC INSULATION ATA : 21"RECOMMENDED" SB NO. 25-3582THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SOUND DAMPENING MATERIAL THROUGHOUTTHE AIRCRAFT CABIN AND AFT COMPARTMENT FOR IN-SERVICE AICRAFT.

NOTENOTENOTENOTE:::: "EC1761" ADHESIVE AND "5776" URALANE ADHESIVE REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANY OUTLET.

WT. CHANGE : 16.8 LBS MOMENT: 4628 IN LBSEST. MAN/HRS: : 24MEN : 2 (MEN)


KIT CATALOG

390-5306-0001ACOUSTIC INSULATION ATA : 25

RB-2 THRU RB-54"RECOMMENDED" SB NO. 25-3582THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL SOUND DAMPENING MATERIAL THROUGHOUTTHE AIRCRAFT CABIN AND AFT COMPARTMENT FOR IN-SERVICE AICRAFT.

NOTENOTENOTENOTE:::: "EC1761" ADHESIVE AND "5776" URALANE ADHESIVE REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY AUTHORIZED COMPANY OUTLET.

WT. CHANGE : 16.8 LBS MOMENT: 4628 IN LBSEST. MAN/HRS: : 24MEN : 1 (MAN)

390-5309-0001SIDEWALL INSULATION ATA : 25390 RB-4 THRU RB-111O SB 25-3720THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE THE UPPER SIDEWALL ASSEMBLIES, ANDPLACE SOUND DAMPENING INSULATION ASSEMBLIES FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "5776" URALANE ADHESIVE REQUIRED BUT NOT PROVIDED WITH KIT. PROCURESEPARATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : 4.00 LBMOMENT: 1129 IN-LBS.EST. MAN/HRS: : 40 HRS. (TO REMOVE/INSTALL INTERIOR PANELS), 10 HRS. (TO INSTALL KIT)MEN : 1 (MAN)

390-5312-0001SUPPLEMENTAL INTERIOR/EXTERIOR MARKINGS-UK ATA :390 RB-4 & AFTERTHIS KIT PROVIDES INSTALLATION INSTRUCTIONS & PARTS FOR SUPPLEMENTAL MARKINGS REQUIREDFOR FOREIGN CERTIFICATION-UK-FOR IN SERVICE AIRCRAFT. THE MARKINGS INSTALLED ON THISDRAWING ARE IN ADDITION TO THE ENGLISH LANGUAGE MARKINGS INSTALLED ON 390-530003 &390-530004.

NOTENOTENOTENOTE:::: "EC9309NA" ADHESIVE REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-5540-0RAM AIR SYSTEMS INSTL. ATA : 21390 RB-2 THRU RB-26"RECOMMENDED" SB NO. 21-3514PR-CSL-1002 (CUSTOMER SERVICE LETTERTHIS KIT PROVIDES PARTS AND INFORMATION NECESSARY TO ADD DRAIN TUBES AND TO INSTALL NEWLOUVER FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR1428""RTV732""EA9309NA"& "EA9394" ADHESIVE REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : -0.5 LB. MOMENT: -234 LB-IN.EST. MAN/HRS: : MAN/HRS: PART I: 1/2 HR. (1 MAN) PART II: 8 HRS. (1 MAN)MEN : N/A


KIT CATALOG

390-5541-0001DRAIN INSTALLATION, RAM AIR SYSTEM ATA : 24


PREMIER RB-19 THRU RB-32"MANDATORY" SB 24-3544; SC 209THIS KIT PROVIDES PARTS AND INFORMATION TO ADD DRAINAGLE PROVISIONS IN THE RAM AIR SYSTEMFOR IN-SERVICE AIRCRAFT

NOTENOTENOTENOTE:::: "RTV732" SEALANT & "CE1164" CONFORMAL COATING REQUIRED BUT NOT FURNISHEDWITH KIT. PROCURE SEPARATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-5550-0001AFT FUSE FWD SEC,ECS PROV INSTL ATA : 21PREMIER 390 RB-1 THRU RB-79THIS KIT PROVIDES A PART AND INFORMATION NECESSARY TO REPLACE THE PLACARD FOR THE AIRCONDITIONING SERVICE PANEL ON IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-5800-0001GROUND SERVICE PRESSURE FILTRATION ATA :390 RB-1 & RB-4 THRU RB-99THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GROUND SERVICE HYDRAULIC PRESSURETUBE ASSEMBLIES AND CHANGE THE EXTERNAL SOURCE PRESSURE INPUT TO BE UPSTREAM OF THEHYDRAULIC FILTRATION MODULE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "4PHS111-06" COUPLING REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.


390-5800-0005GROUND SERVICE PRESSURE FILTRATION ATA :390 RB-1 & RB-4 THRU RB-99THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE GROUND SERVICE HYDRAULIC PRESSURETUBE ASSEMBLIES AND CHANGE THE EXTERNAL SOURCE PRESSURE INPUT TO BE UPSTREAM OF THEHYDRAULIC FILTRATION MODULE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "4PHS111-06" COUPLING REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : NEGLIBIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

390-5802-0001OVERBOARD DRAIN WEEPAGE REDUCTION ATA :390 RB-4 THRU RB-174"O"S.B.29-3812THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE HYDRAULIC PACKAGE OVERBOARD DRAINTUBE ASSEMBLY AND RELIEF VALVE WITH REROUTED DRAIN AND NEW LOWER PRESSURE RELIEFVALVE FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "PR1440" SEALANT REQUIRED, BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY COMPANY AUTHORIZED OUTLET.


390-5803-0001HYDRAULIC CASE DRAIN CHECK VALVE INSTL ATA : 29

390 RB-4 THRU RB-224"M"S.B.29-3851

THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL CHECK VALVES IN THE HYDRAULIC PUMPCASE DRAIN LINES FOR IN-SERVICE AIRCRAFT.WT. CHANGE : WT: +1.7 LBS MOMENT: +672 LB-INEST. MAN/HRS: : 8MEN : 2 (MEN)

390-5804-0001DAMPENER SUPPORT IMPROVEMENT ATA :390 RB-50 AND AFTER AND PRIOR AIRCRAFT

WITH KIT 390-9100 INSTALLED. THIS KITTO BE INSTALLED PRIOR TO KIT 390-5805.

"M"S.B.29-3800THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL NEW PULSATION DAMPENER SUPPORTBRACKETS FOR IN-SERVICE AIRCRAFT.



KIT CATALOG

390-5805-0001HYDRAULIC PUMP PRESSURE HOSE INSTALLATION ATA :390 RB-4 THRU RB-49 EQUIPPED WITH FIELD

SERVICE KIT 390-9100 AND RB-50 ANDAFTER

"M"S.B.29-3800THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL HYDRAULIC PUMP PRESSURE HOSEASSEMBLIES IN PLACE OF THE TUBE ASSEMBLIES BETWEEN THE ENGINE DRIVEN PUMP AND THE PULSEDAMPENER ON BOTH LEFT AND RIGHT ENGINES.

NOTENOTENOTENOTE:::: NOTE: THIS KIT MUST BE INSTALLED WITH OR AFTER FIELD SERVICE KIT 390-5804 KIT,DAMPENER SUPPORT IMPROVEMENT, FOR IN-SERVICE AIRCRAFT MODEL 390 SERIALSRB-4 THRU RB-49 EQUIPPED WITH FIELD SERVICE KIT 390-9100 AND RB-50 AND AFTER.

WT. CHANGE : WT: +2.88 LBS. MOMENT: +1,115 LB-IN.EST. MAN/HRS: : 8 HRSMEN : 1 (MAN)

390-5807-0001MASTER CYLINDER IMPROVEMENT ATA : 32PREMIER MODEL 390 RB-4 THRU RB-10, RB-12 THRU RB-159

WITH 390-5801-0001 INSTALLED; ANDRB-160 THRU RB-202

THIS KIT PROVIDES PARTS AND INFORMATION TO REMOVE 4X 390-385800-0001 MASTER CYLINDERS.390-58205-0001 BRACKET. REWORK 390-584029 TUBE ASSY AND INSTALL 4X 390-385800-0003 MASTERCYLINDERS, 390-820504-0005 BRACKET, 390-584029-0009 TUBE ASSEMBLY FOR THE FOLLOWING INSERVICE AIRCRAFT: MODEL 390 SERIALS: RB-4 THRU RB-10, RB-12 THRU RB-159 WITH 390-5801-0001INSTALLED; AND RB-160 THRU RB-202. NOT FURNISHED WITH KIT: ADHESIVE, WEATHERBAN,ASHESIVE,SCOTCH SEAL AND SAFETY WIRE MS20995C32 OBTAIN LOCALLY. 390-385800-0003 NOTSUPPLIED WITH KIT; OBTAIN FROM RAPID

MEN : N/A

390-9100-0HYDRAULIC PULSE DAMPENER INSTL. ATA : 29PREMIER 390 RB-2 THRU RB-74"RECOMMENDED" SB NO. 25-3582THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROVISIONS FOR THE HYDRAULIC PULSEDAMPENER FOR IN-SERVICE AIRCRAFT.WT. CHANGE : +2.2 LBS MOMENT: +844 LB-INEST. MAN/HRS: : 16MEN : 2 (MEN)

390-9101-0TMA INSTALLATION, ENG MOUNT. ATA : 71PREMIER 390 RB-2 THRU RB-58THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TUNED MASS ABSORBERS TO AGREE WITHFLEET CONFIGURATION FOR IN-SERVICE AIRCRAFT.WT. CHANGE : BALANCE: +5.4 LBSMOMENT: +2079 LB-INEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


KIT CATALOG

390-9101-0001TMA INSTALLATION ATA : 25PREMIER RB-2 THRU RB-58SB NO. 25-3582THIS KIT PROVIDES PARTS AND INFORMATION TO INSTALL TUNED MASS ABSORBERS TO AGREE WITHFLEET CONFIGURATION FOR IN-SERVICE AIRCRAFT.WT. CHANGE : +5.4 LBS; MOMENT +2079 LB-INEST. MAN/HRS: : 8 HRS COMPLMEN : N/A

390-9104-0003CLEARANCE DEFINITION, ENGINE BUILDUP ATA : 71390 RB-1, RB-4 THRU RB-84, RB-87 THRU RB-90,

RB-92 THRU RB-96, RB-98 THRU RB-101, &RB-103 THRU RB-107

"M"SB #71-3685 REV 1THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROVISIONS FOR THE LH AND RH ENGINE BUILD-UP FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT IS BEING ISSUED FOR OWNER/OPERATORS WHO ATTEMPTED TO COMPLY WITH THEORIGINAL ISSUANCE OF THIS S.B., BUT COULD NOT MEET REQUIRED CLEARANCES.

WT. CHANGE : 1.22 LB MOMENT:478.19 LB-INEST. MAN/HRS: : 8 HRS PER ENGINEMEN : 1 (MAN)

390-9104-0005CLEARANCE DEFINITION, ENGINE BUILDUP ATA : 71

390 RB-1, RB-4 THRU RB-84, RB-87 THRU RB-90,RB-92 THRU RB-96, RB-98 THRU RB-101, &RB-103 THRU RB-107

"M"SB #71-3685 REV 1THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROVISIONS FOR THE LH AND RH ENGINE BUILD-UP FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: KIT IS BEING ISSUED FOR OWNER/OPERATORS WHO HAVE NOT COMPLIED WITH THEORIGINAL ISSUANCE OF S.B.

WT. CHANGE : 1.22 LB MOMENT:478.19 LB-INEST. MAN/HRS: : 8 HRS PER ENGINEMEN : 1 (MAN)


KIT CATALOG

390-9200-0001UNUSABLE FUEL REDUCTION ATA : 28


THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROVISIONS TO REDUCE UNUSABLE FUEL ON IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: "390-382032-0007" DISPLAY-FUEL QUANTITY, NOT FURNISHED WITH KIT. CONTACT RAPID1-888-727-4344 TO SCHEDULE EXCHANGE FOR REPLACEMENT COMPONENT PRIOR TOCOMPLETION OF THIS KIT.

NOTENOTENOTENOTE:::: "EA9309NA" ADHESIVE & "PR-1440" SEALANT REQUIRED BUT NOT FURNISHED WITH KIT.PROCURE SEPERATELY AT ANY COMPANY AUTHORIZED OUTLET.

WT. CHANGE : +3.1 LBS MOMENT: +862 IN-LBS, WT: +3.1 LBSMOMENT: +862 IN-LBSUNUSABLE FUEL WT: -59.8 LB. MOMENT: -16220 LB-IN.



RB-67 THRU RB-71THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROVISIONS TO REDUCE UNUSABLE FUEL ON IN-SERVICE AIRCRAFT.












KIT CATALOG







390-9201-0001TEE ASSY. REPLACEMENT, SINGLE POINT ATA : 28

RB-2 THRU RB-3THIS KIT PROVIDES PARTS AND INFORMATION TO REPLACE THE W952B40K24 TEE ASSY WITH THEW952B38K24 TEE ASSY TO AGREE WITH THE FLEET CONFIGURATION FOR IN-SERVICE AIRCRAFT.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A

390-9202-0001FUEL SENSOR TO ACCESS DOOR RELOCATION ATA : 28

RB-2 THRU RB-74"MANDATORY" SB NO. 28-3595THIS KIT PROVIDES PARTS AND INFORMATION TO RELOCATE THE LOW FUEL LEVEL SENSOR TOIMPROVE ACCURACY AND LEVEL AT WHICH SENSOR ACTIVATES FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PETROLEUM JELLY LUBRICANT REQUIRED BUT NOT FURNISHED WITH KIT. PROCURESEPERATELY FROM ANY AUTHORIZED COMPANY OUTLET.

NOTENOTENOTENOTE:::: THIS KIT TO BE INSTALLED IN CONJUNCTION WITH KIT 390-9204.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 2 (MEN)

390-9203-0001DRAIN PROVISIONS FORWARD & AFT WHEEL WELL VAPOR BOX-INFOONLY

ATA : 53

390 RB-4 THRU RB-101, RB-103 THRU RB-123"M"SB #53-3726THIS KIT PROVIDES INFORMATION ONLY TO ADD DRAIN PROVISIONS FOR THE FORWARD AND AFTWHEEL WELL VAPOR BOXES ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : INSPECTION 1 HR. MODIFICATION 8 HRSMEN : 1 (MAN)


KIT CATALOG

390-9204-0001FUEL TRANSFER SYSTEM ATA : 28


"M" SB #28-3594 ISSUED 11/03THIS KIT PROVIDES PARTS AND INFORMATION TO ADD PROVISIONS FOR TRANSFER SYSTEMMODIFICATIONS FOR IN-SERVICE AIRCRAFT.

NOTENOTENOTENOTE:::: PR1440" SEALANT REQUIRED BUT NOT FURNISHED WITH KIT. PROCURE SEPERATELYFROM ANY AUTHORIZED COMPANY OUTLET.

NOTENOTENOTENOTE:::: THIS KIT MUST BE WORKED IN CONJUNCTION WITH 390-9202.WT. CHANGE : NEGLIGIBLEEST. MAN/HRS: : 16MEN : 2 (MEN)

390-9700-0001PNEUMATIC QUICK DRAIN INSTL ATA :390 RB-4 THRU RB-139THIS KIT PROVIDES PARTS AND INFORMATION TO ADD DRAIN PROVISIONS FOR THE PNEUMATIC SYSTEMCOLLECTION TUBE IN AFT AVIONICS BAY ON IN-SERVICE AIRCRAFT.WT. CHANGE : N/AEST. MAN/HRS: : CONTACT PRODUCT SUPPORTMEN : N/A


Beech Kit Catalog April 2009

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Transcript of Beech Kit Catalog April 2009