Modification Control Report 13237 24. · PDF file737-11-1040 sb 00 recommended a/c alternate...

Document-Number Type Rev Compliance A|C Subject Status61163-28-08 SB 00 MANDATORY A/C *AD* ENG. FUEL SHUTOFF/SYSTEM XFEED VALVES - REPLACEMENT OF Closed 08.Dec.1995

1995-15-06 (ACTIVE)J.C. CARTER SB 61163-28-08SB 61163-28-08 (MOD-TASK)

ADSBTA

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.1995PerfRev.:'NOTE' / Reason: DELIVERYDOC.

Reason for this StatusDELIVERY DOC.

69-37313-31-03 SB 00 MANDATORY COMP *AD*P5-3 FLIGHT CONTROLS MODULE ASSEMBLY MODIFICATION Not Applicable by Serial Number2002-20-07 R12007-03-0769-37313-31-03737-27-1264

ADADSBSB

Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

737-11-1040 SB 00 RECOMMENDED A/C ALTERNATE FLAP EXTENSION LIMIT SPEED PLACARD REPLACEMENT Closed 06.Aug.1991This document is applicable to LN# 1001-1882.737-11-1040-R0 (ACTIVE)PRODUCTION LINE PRR34847

SBPRR


06.Aug.1991PerfRev.:'NOTE' / Reason: DELIVERYDOC, WO

Reason for this StatusDELIVERY DOC, WO

Document-Number Type Rev Compliance A|C Subject Status

For Aircraft `LN-KKM` (S/N: 24676, Act.TAH: 73322, Act.TAC: 44495)Selection: SERVICE BULLETIN Issued by `BOEING`

produced by www.swiss-as.comAMOS

Modification Control Report 13237 10:29

24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-11-1050 SB NO

TERECOMMENDED A/C INSTALLATION OF AN ACARS PLACARD IN THE FLIGHT COMPARTMENT Not Applicable

737-11-1050-R0 (ACTIVE) SB

737-11-1051 SB NOTE

RECOMMENDED A/C INSTALLATION OF A PLACARD ON THE P-8 ELECTRONICS PANEL Not Applicable by Serial Number

737-11-1051-R0 (ACTIVE) SB

737-11-1075 SB 00 RECOMMENDED A/C NACELLE AND POWER PLANT THRUST REVERSER MAINTENANCE WARNING Rejected by Operator737-11-1075-R0 SBReason for this StatusREJECTED BY PREVIOUS OPERATOR

737-11-1097 SB 00 RECOMMENDED A/C FWD/AFT CARGO COMPARTMENT/POTABLE WATER TANK WARNING MARKER Rejected by Operator2078-11-1 (EDO FIBER SCIENCE)737-11-1097-R0 (ACTIVE)737-SRP-38-0043 (REF)

SBSBSRP

Reason for this StatusCOMPLIANCE: NOT EMBODIED, NO ACTION

737-11-1105 SB NOTE

RECOMMENDED A/C MULTIPLE OPERATING WEIGHTS PLACARD INSTALLATION Not Applicable

737-11-1105-RO (ACTIVE)MASTER CHANGEMC0310MK3840

SB

CR


For Aircraft `LN-KKM` (S/N: 24676, Act.TAH: 73322, Act.TAC: 44495)Selection: SERVICE BULLETIN Issued by `BOEING` For Aircraft `LN-KKM` (S/N: 24676, Act.TAH: 73322, Act.TAC: 44495)Selection: SERVICE BULLETIN Issued by `BOEING`



24.Oct.2014/411


TERECOMMENDED A/C EXTERIOR PLACARDS AND MARKINGS/FORWARD AIRSTAIR DECAL INSTAL Rejected by Operator

737-11-1136-RO (ACTIVE)737-SRP-52-0074 (REF)PRODUCTION PRR35005-263RS

SBSRPPRR


737-11-1148 SB NOTE

OPTIONAL A/C REQUIRED PLACARDS - CHANGE CONTROL COLUMN CHECKLIST PLACARDS Rejected by Operator

SBB 737-11-1148 (MOD TASK)SBB 737-11-1148-R0 (REF)SBB 737-11-1148-R1 (ACTIVE)

TASBSB


737-1150-27-05 SB A MANDATORY COMP *AD* AUX RUDDER POWER CONTROL PACAGE - REPL OF INPUT LEVER Not Applicable by Serial NumberPN/SN in effectivity are units modified from -3 to -4 by NAS.-4 PN is modified and in compliance with SB.

-Either modified directly or maintained via CMM 27-20-02 which has SBincorperated at CMM rev.:16.2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)SMITHS 1150-27-05 (REF)SMITHS 1150-27-05A (ACTIVE)

ADADSBSB

Affected Rotables (Part No/Serial No/Position) Status1U1150-4 / 0962 Pos=#0 (KKM) Not Applicable





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Document-Number Type Rev Compliance A|C Subject Status737-20-1002 SB 01 RECOMMENDED A/C GROUNDING-FORWARD AND AFT ATTENDANT`S PANEL GROUND WIRE INST Closed 31.Mar.1993

737-20-1002-R1PRODUCTION LINE PRR34754

SBPRR


31.Mar.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC: WO:

Reason for this StatusDELIVERY DOC: WO:

737-20-1005 SB 00 RECOMMENDED A/C WIRE BUNDLE CHAFING IN THE P5 OVERHEAD PANE WIRE BUNDLE INSTALLATIONCHANGE

Open

24-099737-24-1083SRP-20-0009

SLSBSRP

000100

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document27.Jan.2016 Perform initially before(F) 28.Jan.2016

737-21-1085 SB 01 MANDATORY A/C *AD* TO ENSURE AIR DUCTS HAVE ADEQUATE FLAMMABILITY CHARACT. Not Applicable by Serial Number1986-19-06 (ACTIVE)737-21-1085 (ACTIVEPRODUCTION LINE PRR33656

ADSBPRR

737-21-1099 SB 01 RECOMMENDED A/C PASS. CABIN CONDITIONED AIR/FORW AND AFT ENTRY LIGHT SEALING Ex Factory737-21-1099-R1PRODUCTION LINE PRR34614

SBPRR

Reason for this StatusPRODUCTION PRR 34614





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Document-Number Type Rev Compliance A|C Subject Status737-21-1101 SB 01 RECOMMENDED A/C AIR CONDITIONING - EQUIPMENT COOLING SYSTEM/DUCT REPLACEMENT Ex Factory

737-21-1101-R1 (ACTIVE)PRODUCTION LINE PRR34784

SBPRR


737-21-1102 SB 01 RECOMMENDED A/C AIR CONDITIONING - RAM AIR SYSTEM WIRE MODIFICATION Closed 23.Mar.201020-10-11120-50-0520-50-1021-64-0121-64-0221-64-0324-22-0024-56-01737-21-1102737-21-1102-R1 (ACTIVE)PRODUCTION LINE PRR34756SBB 737-21-1102

AMMSOPMSOPMWDMWDMWDMAMMWDMSBSBPRRTA


23.Mar.2010 60868:00/H 35008/CPerfRev.:'NOTE' / Reason: 2-MOD 520108ITEM: 1

Reason for this Status2-MOD 520108 ITEM: 1





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Document-Number Type Rev Compliance A|C Subject Status737-21-1104 SB 01 RECOMMENDED A/C AFT ENTRY AREA OVERHEAD AIR DISTRIBUTION DUCT MODIFICATION Closed 01.Apr.1993


SBPRR


01.Apr.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC: WO:


737-21-1108 SB 00 RECOMMENDED A/C PRIMARY AND ALTERNATE EQUIPMENT COOLING SYSTEM CHANGES Not Applicable by Serial Number737-21-1108-RO (ACTIVE)PRODUCTION LINE PRR35051

SBPRR

737-21-1112 SB 00 RECOMMENDED A/C EQUIP. COOLING SYSTEM FANS, CHECK VALVES AND PLENUM DUCT REP Rejected by Operator737-21-1112-R0 (ACTIVE)PRODUCTION LINE PRR35162

SBPRR

737-21-1113 SB 00 RECOMMENDED A/C CABIN PRESSURE CONTROLLER - CONNECTOR REPLACEMENT Rejected by Operator20-10-0720-20-0020-50-1021-31-0021-31-2121-34-01737-21-1113-R0 (ACTIVE)PRODUCTION LINE PRR35005-59

AMMSWPMSOPMAMMAMMWDMSBPRR

Reason for this StatusCOMPLIANCE: N/A BY LINE NUMBER





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Document-Number Type Rev Compliance A|C Subject Status737-21-1118 SB 01 RECOMMENDED A/C WIRING CHANGE FOR THE STANDBY MODE OF THE CABIN PRESSURE SYS Closed 16.Mar.2009

Thid Modification is applicable to LN 1001-2717.737-21-1118-R1 (ACTIVE)PRODUCTION LINE PRR35005-111

SBPRR




737-21-1119 SB 01 RECOMMENDED A/C WIRING CHANGE FOR THE STANDBY MODE OF THE CABIN PRESSURE SYS Not Applicable by Serial Number21-66 (HAMILTON STANDARD)737-21-1119-R1 (ACTIVE)737-24-1110 (REF)PRODUCTION LINE PRR35322-R

SBSBSBPRR

737-21-1123 SB 02 RECOMMENDED A/C RAM AIR EXHAUST DUCT ASSEMBLY INSPECTION / MODIFICATION Rejected by Operator737-21-1123-R2 (ACTIVE)737-SRP-21-0097 (REF)

SBSRP






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Document-Number Type Rev Compliance A|C Subject Status737-21-1131 SB 02 MANDATORY A/C *AD* AIR CONDITION OVERHEAD DUCT LANYARD INSTALLATION Superseded (Closed 07.Feb.2008)

2005-03-02 (ACTIVE)737-21-1131 (REF)737-21-1131 IN 01737-21-1131-R1 (REF)737-21-1131-R2 (ACTIVE)PRODUCTION LINE PRR35426-RSBB 737-21-1131 (MOD-TASK)

ADSBSBSBSBPRRTA

4

This Document has been SUPERSEDED BY 737-21-1131/SB Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

07.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: KKM 151351ITEM: 1

Reason for this StatusKKM 151351 ITEM: 1

737-21-1131 SB 04 MANDATORY A/C *AD* AIR CONDITION OVERHEAD DUCT LANYARD INSTALLATION See prev. Docstatus / Special Text:This Aircraft is NA to this LN# dueto PRODUCTION LINEPRR35426-R

PRODUCTION LINE PRR35426-R PRR 00This Document SUPERSEDES 737-21-1131/SB Rev.02Reason for this StatusPERFORMED ON PREVIOUS REVISION

737-21-1141 SB 01 OPTIONAL A/C EQUIPMENT COOLING SYSTEM - REPLACE COOLING FLOW SENSOR Rejected by Operator737-21-1141MC2158MK3026

SBDOCR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21-1164 SB 00 RECOMMENDED A/C PRESSURIZATION INDICATION AND WARNING - REDUNDANT PRESSURE SWITCH

AND AURAL WARNING MODULE INSTALLATIONSuperseded (Cancelled)

BACKGROUNDThis service bulletin gives instructions to make changes to the CabinAltitude Warning System. These changes will install a second 10,000foot cabin altitude pressure switch and new Aural Warning Module(AWM). If the changes in this service bulletin are not done, thecabin altitude warning may not function if there is a failure ofthe cabin altitude 10,000 foot pressure switch. Boeing received areport from an operator that they had experienced a cabindepressurization. The flight crew were not aware of the cabindepressurization and that the oxygen masks had been deployed untilthey were informed by a member of the cabin crew. An investigationfound that the flight crew did not get an aural warningbecause of the failure of the cabin altitude 10,000 foot pressureswitch.

The installation of a second 10,000 foot pressure switch and a newdigital AWM with two fully independent channels will reduce theprobability of the flight crew being not aware of a depressurizationevent.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-SRP-21-0172AMM 24-22-00BAE CMM 31-26-20BAE SYSTEM SB 69-72814-31-03FTD 31-06003PRR 35005-282RSSRM CH 51SWPM 20-00-11,13SWPM 20-10-11,12,18,19SWPM 20-20-00,10SWPM 20-30-11,12,16,22SWPM 20-60-08,09SWPM 20-61-11,19WDM 21-33-01, 31-26-01WDM 32-31-01, 32-31-02

SRPAMMCMMSBFTDPRRSRMSWPMSWPMSWPMSWPMSWPMSWPMWDMWDM

000000000000000

This Document has been SUPERSEDED BY 737-21-1164/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21-1164 SB 01 MANDATORY A/C PRESSURIZATION INDICATION AND WARNING - REDUNDANT PRESSURE SWITCH

AND AURAL WARNING MODULE INSTALLATIONSuperseded (Cancelled)

BACKGROUNDThis service bulletin gives instructions to make changes to the CabinAltitude Warning System. These changes will install a second 10,000foot cabin altitude pressure switch and new Aural Warning Module(AWM).

Compliance:This SB ensures compliance with AD§ (c)(1).737-SRP-21-0172AMM 24-22-00BAE CMM 31-26-20BAE SYSTEM SB 69-72814-31-03FTD 31-06003PRR 35005-282RSSRM CH 51SWPM 20-00-11,13SWPM 20-10-11,12,18,19SWPM 20-20-00,10SWPM 20-30-11,12,16,22SWPM 20-60-08,09SWPM 20-61-11,19WDM 21-33-01, 31-26-01WDM 32-31-01, 32-31-02


000000000000000

This Document SUPERSEDES 737-21-1164/SB Rev.00This Document has been SUPERSEDED BY 737-21-1164/SB Rev.02Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21-1164 SB 02 MANDATORY A/C PRESSURIZATION INDICATION AND WARNING - REDUNDANT PRESSURE SWITCH

AND AURAL WARNING MODULE INSTALLATIONOpen / Special Text: SB group 6

BACKGROUNDThis service bulletin gives instructions to make changes to the CabinAltitude Warning System. These changes will install a second 10,000foot cabin altitude pressure switch and new Aural Warning Module(AWM).

Compliance:This SB ensures compliance with AD§ (c)(1).737-SRP-21-0172AMM 24-22-00BAE CMM 31-26-20BAE SYSTEM SB 69-72814-31-03FTD 31-06003PRR 35005-282RSSRM CH 51SWPM 20-00-11,13SWPM 20-10-11,12,18,19SWPM 20-20-00,10SWPM 20-30-11,12,16,22SWPM 20-60-08,09SWPM 20-61-11,19WDM 21-33-01, 31-26-01WDM 32-31-01, 32-31-02


000000000000000

This Document SUPERSEDES 737-21-1164/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document06.Nov.2018 Perform initially before(F) 07.Nov.2018





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21-1172 SB 00 RECOMMENDED A/C AIR CONDITIONING - DISTRIBUTION - CONTROL CABIN DUCT POLYURETHANE

FOAM INSULATION REPLACEMENTNot Applicable by Serial Number

737-SRP-21-0158 SRP 0

737-21-1173 SB 00 RECOMMENDED A/C AIR CONDITIONING - REPL. OF POLYRETHANE FOAM INSULATION Not Applicable by Serial Number20-30-03 (REF)20-50-10 (REF)20-50-12 (REF)25-21-45 (REF)737-21-1173-R0 (ACTIVE)737-SRP-21-0158 (REF)PRODUCTION 35005-289RS

SOPMSOPMSOPMAMMSBSRPPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21-1186 SB 00 MANDATORY A/C AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -

INSP OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSORClosed 08.Apr.2014 W/O:556884

This service bulletin gives instructions to do a General Visualinspection of the installation of metal clamps installed on the hosesof the Air Conditioning Temperature Sensor, Gasper Air Outlet and theDiffuser on the left side of the Control Cabin at STA 259.5. If themetal clamps are not the correct part number or not correctlypositioned on the hose, the adjacent wire bundles can become damaged.

All Norwegian AC are Group 1. AD will be released. NPRM2013-NM-125-AD issued.2013-NM-125-AD2014-04-05AMM 21-22-09, 25-11-21BOEING 737-21-1186IN01BOEING SRP 737-SRP-21-0186SAFO13006SWPM 20-10-11, 12, 13, 19

NPRMADAMMSBSRPSIBSWPM

000000IN01000000

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks25.Apr.2013 69256:00/H 41420/C 431232, N/A Was due at: 31.May.2013 PerfRev.:'00'

737-21-1186/SB* Rev.00 AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -INSP OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSOR

Closed 08.Apr.2014 W/O:556884

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks25.Apr.2013 69256:00/H 41420/C 431232, N/A Was due at: 31.May.2013 PerfRev.:'00'

> 737-21-1186-01/EO* Rev.00 AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -REMOVAL OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSOR

Closed 08.Apr.2014 W/O:556884

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Apr.2014 71829:00/H 43364/C 556884, Was due at: 01.Jun.2014 PerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21A1129 SB 00 MANDATORY A/C *AD* AIR CONDITIONING-DISTRIBUTION - DUCT INSULATION REPL. Not Applicable by Serial Number

This document is applicable to airplanes line numbers 2591,2601,2720, 2723, 2730, 2733, 2734, 2736 through 2850, 2852 through 3126,divided into four groups. All other LN# are Not Applicable per PRR35--05-231R.737-21A1129 IN 01 (REF)737-SRP-21-0125 (REF)PRODUCTION LINEPRR35005-231R

SB

SRP

PRR

00

00

00

737-21A1132 SB 03 MANDATORY A/C AIR CONDITIONING - DISTRIBUTION - REPLACEMENT OF BMS 8-39 DUCTINSULATION

Not Applicable by Serial Number

Effectivity:This document is applicable to LN# 3-1585.

Compliance:This SB ensures compliance with AD 2012-02-09 § (g).2011-NM-101-AD737-21A1132737-21A1132737-21A1132737-SRP-21-0130 (REF)PRODUCTION LINE PRR35005-235R

NPRMSBSBSBSRPPRR

0000010200

This Document SUPERSEDES 737-21A1132/SB Rev.02





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21A1132 SB 02 RECOMMENDED A/C AIR COND/DISTRIBUITON - DUCT INSULATION BMS 8-39 REPLACEMENT Superseded (Not Applicable by

Serial Number)737-SRP-21-0130 (REF)PRODUCTION LINE PRR35005-235RSBB 737-21A1132-R00 (REF)SBB 737-21A1132-R01 (REF)SBB 737-21A1132-R02 (ACTIVE)

SRP

PRR

SB

SB

SB

This Document has been SUPERSEDED BY 737-21A1132/SB Rev.03

737-21A1138 SB 02 RECOMMENDED A/C INSTALL. OF THE INSULATIONS AND TAPES OR THE OVERHEAD DUCT Not Applicable by Serial Number737-21A1138-R0 (REF)737-21A1138-R1 (REF)737-21A1138-R2 (ACTIVE)737-SRP-21-0140 (REF)PRODUCTION MRR3211-1453S

SBSBSBSRPPRR

737-21A1156 SB 03 MANDATORY A/C EQUIPMENT COOLING SYSTEM - ELECTRONIC FLIGHT INSTRUMENT SYSTEMCOOLING SUPPLY OFF LIGHT WIRING CHANGE

See prev. Docstatus

2009-12-05 (ACTIVE)737-21-1108 (REF737-21A1156-IN02737-21A1156-R0 (REF)737-21A1156-R1 (REF)737-21A1156-R2 (ACTIVE)

ADSBSBSBSBSB

100000

This Document SUPERSEDES 737-21A1156/SB Rev.02Reason for this StatusPERFORMED ON REV 2





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-21A1156 SB 02 MANDATORY A/C *AD* EFIS COOLING SUPPLY OFF LIGHT WIRING, MODIFICATION OF Superseded (Closed 27.Jun.2011

W/O:205151)2009-12-05 (ACTIVE)737-21-1108 (REF737-21A1156-IN02737-21A1156-R0 (REF)737-21A1156-R1 (REF)737-21A1156-R2 (ACTIVE)

ADSBSBSBSBSB

This Document has been SUPERSEDED BY 737-21A1156/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks27.Jun.2011 64534:00/H 37798/C 205151, N/A Was due at: 16.Jul.2011 PerfRev.:'02'

737-22-1101 SB NOTE

RECOMMENDED A/C AUTOFLIGHT - FLIGHT CONTROL COMPUTER FEATURES ACTIVATION Not Applicable by Serial Number

737-22-1101-R0 (ACTIVE)737-22-1102-R0 (REF)PRODUCTION LINEMC2210MK3054

SB

SB

PRR

737-22-1102 SB 00 RECOMMENDED A/C AUTO FLIGHT - AUTOPILOT - FLIGHT CONTROL COMPUTER REPLACEMENT Not Applicable by Serial Number

737-22-1104 SB NOTE

RECOMMENDED A/C INSPECTION/ INSTALLATION AILERON CONTROL WHEEL STEERING WIRE Not Applicable by Serial Number

737-22-1104-R0 (ACTIVE) SB





24.Oct.2014/411


TERECOMMENDED A/C EXAMINE AND MAINTAIN CHANNEL A AND B Closed 31.Mar.1993

737-22-1108 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Mar.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC: WO:


737-22-1109 SB 00 RECOMMENDED A/C REPLACEMENT OF THE AUTOTHROTTLE COMPUTER P/N 10-62017-21 Not Applicable737-22-1079 (REF)737-22-1082 (REF)737-22-1109-R0 (ACTIVE)755SUE-22-1211 (REF)P/N 10-62017-21 (REF)PRODUCTION PRR35011PRR35117-R

SBSBSBSBSBPRR

Reason for this StatusAFFECTED EQUIPMENT NOT INSTALL

737-22-1112 SB 00 RECOMMENDED A/C YAW DAMPER SYS WIRE CHANGE TO REDUCE KICKS CAUSED BY HIGH IN Closed 31.Mar.1991This document is applicable to LN# 1001-2108 with HF com systeminstalled.737-22-1112-R0 (ACTIVE)PRODUCTION MRR3221-845

SBPRR


31.Mar.1991PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:

Reason for this StatusDELIVERY DOC WO:





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-22-1120 SB 00 RECOMMENDED A/C INSP/INSTALLATION OF CLAMP TO PREVENT CHAFING OF WIRE BUNDLE Closed 10.Apr.1997

737-22-1120-R0 (ACTIVE)PRODUCTION MRR3225-1073

SBPRR


10.Apr.1997PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-22-1124 SB 00 MANDATORY A/C *AD* Y/D SYSTEM COUPLER & RUDDER POWER CONTROL WIRING CHANGE Superseded (Superseded)This document is effective for LN# 1-2907.1997-14-03 (ACTIVE)737-11-1124737-SRP-22-0009 (REF)PRODUCTION LINE PRR35005-134

ADSBSRPPRR

00010000

This Document has been SUPERSEDED BY 737-22-1124/SB Rev.01

737-22-1124 SB 01 MANDATORY A/C AUTOFLIGHT - AUTOPILOT - YAW DAMPER SYSTEM - YAW DAMPER COUPLER ANDRUDDER POWER CONTROL UNIT (PCU) WIRING CHANGE

Closed 11.Feb.1999

This document is effective for LN# 1-2907.1997-14-03 (ACTIVE)737-11-1124737-SRP-22-0009 (REF)PRODUCTION LINE PRR35005-134

ADSBSRPPRR

00010000

This Document SUPERSEDES 737-22-1124/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

11.Feb.1999PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:






24.Oct.2014/411


TEOPTIONAL A/C CHANGE THE PROGRAM PIN WIRING ON THE FLIGHT CONTROL COMPUTER Not Applicable by Serial Number

737-22-1189-R0 (REF)737-22-1189-R1 (ACTIVE)PRODUCTION LINEMC2210MK3355

SB

SB

PRR

737-22A1098 SB 00 MANDATORY A/C *AD* AUTOPILOT MODE CONTROL PANLE REPL. Performed by prev. OperatorThis document is applicable to LN# 1001-2008.1992-07-09A4051601-22-17A4051601-22-18

ADSBSB

000000


26.Oct.1993LHT EO007019

PerfRev.:'00'

Reason for this StatusPERFORMED BY LUFTHANSA





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-22A1130 SB 00 MANDATORY A/C AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THE

AUTOTHROTTLE COMPUTERPerformed by prev. Operator

1992-07-09A4051601-22-17A4051601-22-18

ADSBSB

000000

Perform WITHIN 540/D (effective from 08.Jan.2001)737-22A1130/SB Rev.00 AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THE

AUTOTHROTTLE COMPUTERPerformed by prev. Operator

> 737-22A1130-01/EO* Rev.00 AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THEAUTOTHROTTLE COMPUTER

Performed by prev. Operator


03.Mar.2000DELIVERYDOC

PerfRev.:'00'

> 737-22A1130-02/EO* Rev.00 AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THEAUTOTHROTTLE COMPUTER

Not Applicable

Affected Rotables (Part No/Serial No/Position) Status

755SUE2-4 / 6448 Pos=E&E (KKM)Not Applicable / Reason: AUTOASSIGNED

737-23-1056 SB 02 RECOMMENDED A/C COMMUNICATIONS - GENERAL - WIRE PROTECTION MODIFICATION Not Applicable by Serial Number737-23-1056-R2 (ACTIVE) SB

737-23-1056 SB 01 RECOMMENDED A/C COMMUNICATIONS - GENERAL - WIRE PROTECTION MODIFICATION Not Applicable by Serial Number





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-23-1059 SB 01 MANDATORY A/C *AD* COMMUNICATIONS - CREW CALL HORN CIRCUIT BREAKER INST. Closed 18.Sep.1991

This mod is applicable to LN# 1-1999. The following LN# are NotApplicab ref PRR34954.1991-09-05 (ACTIVE)737-23-1059-R0 (REF)737-23-1059-R1 (ACTIVE)PRODUCTION LINE PRR34954

ADSBSBPRR

00000100


18.Sep.1991PerfRev.:'NOTE' / Reason: DELIVERYDOC.


737-23-1060 SB 01 RECOMMENDED A/C PASSENGER ADDRESS AND ENTERTAINMENT SYSTEM CHANGE Rejected by Operator737-23-1060-R1 (ACTIVE) SBReason for this StatusNOT EMBODIED, NO ACTION

737-23-1068 SB 04 RECOMMENDED A/C HF COMM SYSTEM DISCONNECT BRACKET CHANGE Closed 05.Apr.1996737-22-1112 (REF)737-23-1068-R4 (ACTIVE)

SBSB








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-23-1094 SB 00 RECOMMENDED A/C EMERGENCY LOCATOR TRANSMITTER CIRCUIT BREAKER REMOVAL Not Applicable

737-23-1094-RO (ACTIVE) SBReason for this StatusCOMPLIANCE: N/A BY SB EFFECTIVITY

737-23-1158 SB 00 RECOMMENDED A/C WHF COMMUNICATION SYSTEM-KEYLINE INHIBI WIRING-INSTALLATION Not Applicable737-23-1158-R0 (ACTIVE) SBReason for this StatusCOMPLIANCE: N/A BY SB AFFECTIVITY

737-23-1168 SB 01 RECOMMENDED A/C LATCHING INTERPHONE SWITCH/REMOTE ELECTRONIC UNIT MODIFICATI Rejected by Operator737-23-1168-R1 (ACTIVE)737-SRP-23-0062 (REF)PRODUCTION LINE PRR38060-34

SBSRPPRR

Reason for this StatusN/A BY SB AFFECTIVITY

737-23-1301 SB 00 OPTIONAL A/C CONTROL WHEEL PUSH-TO-TALK SWITCH REPLACEMENT Closed 20.Nov.2010 W/O:117980737-23-1301-R0 (ACTIVE)MC2351MK3334 (REF)

SBDOCR

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks20.Nov.2010 62913:00/H 36543/C 117980, N/A Was due at: 30.Nov.2010 PerfRev.:'00'

737-23-1302 SB 00 MANDATORY A/C COMMUNICATIONS - PASSENGER ENTERTAINMENT SYSTEM - AUDIOENTERTAINMENT MULTIPLEXER POWER RELAY WIRING CHANGE






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1077 SB 04 MANDATORY A/C *AD* ELEC. LOAD DISTRIBUTION - WIRE BUNDLE INSP & PANEL MOD. Closed 19.Sep.1992

1992-07-10 (ACTIVE)737-24-1077-R0 (REF)737-24-1077-R1 (REF)737-24-1077-R2 (REF)737-24-1077-R3 (REF)737-24-1077-R4 (ACTIVE)SBB 737-24-1077 (MOD TASK)

ADSBSBSBSBSBTA




737-24-1081 SB 01 RECOMMENDED A/C ELECTRIAL POWER-GENERATOR FEEDER CABLE CONNECTOR CHANGE Rejected by Operator737-24-1081-R1 (ACTIVE)PRODUCTION LINE PRR33890-80

SBPRR

737-24-1082 SB 00 RECOMMENDED A/C INSPECTION AND INSTALLATION SYSTEM - STATIC CONVERTER Not Applicable737-24-1082-R0 (ACTIVE) SB

737-24-1083 SB 01 RECOMMENDED A/C P5 OVERHEAD INSTRUMENT PANEL-WIRE BUNDLE INSTALLATION CHANGE Closed 25.Feb.1992737-24-1083-R1 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1084 SB 01 MANDATORY A/C *AD* ELEC. LOAD DISTRIBUTION - BATTERY BUS WIRE REPLACEMENT Closed 18.Sep.1992

1992-07-10 (ACTIVE)737-24-1084-R0 (REF)737-24-1084-R1 (ACTIVE)SBB 737-24-1084 (MOD-TASK)

ADSBSBTA




737-24-1087 SB 00 RECOMMENDED A/C ELECTRIC POWER.GENERAL Closed 03.Oct.1994737-24-1087 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

03.Oct.1994PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-24-1088 SB 00 RECOMMENDED A/C STANDBY POWER SYSTEM MOD. Closed 21.Feb.1998737-24-1088 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1089 SB 04 RECOMMENDED A/C STANDBY POWER SYSTEM SMALL BATTERY SYSTEM MODIFICATION Closed 21.Feb.1998

737-24-1089-R4 (ACTIVE)CSB 69-37321-31-01 (REF)PRODUCTION LINE PRR 33890-93

SBSBPRR




737-24-1091 SB 02 RECOMMENDED A/C ELECTRIAL POWER-GROUND STUD INSPECTION Closed 08.Dec.1995737-24-1091-R2 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.1995PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-24-1092 SB 00 RECOMMENDED A/C ELECTRICAL POWER - GENERAL - WIRE BUNDLE ROUTING CHANGE Open737-24-1092-R0 (ACTIVE) SBDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT

737-24-1093 SB 01 RECOMMENDED A/C WIRE SUPPORT TRAY ROUTING MODIFICATION Rejected by Operator737-24-1093-R1 (ACTIVE) SB

737-24-1101 SB 01 RECOMMENDED A/C ELECTRICAL POWER - CIRCUIT BREAKER GUARD INSTALLATION Rejected by Operator737-24-1101PRODUCTION LINE PRR35186-R

SBPRR

01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1102 SB 01 RECOMMENDED A/C ELECTRICAL POWER - GENERATOR DRIVE AND STANDBY POWER MODULE Rejected by Operator

69-37315-31-02 (REF)737-24-1079 (REF)737-24-1102-R1 (ACTIVE)PRODUCTION LINE PRR35005-30

CSBBSBSBPRR

737-24-1106 SB 03 RECOMMENDED A/C BATTERY CHARGER TRANSFER RELAY REPLACEMENT AND RELOCATION Not Applicable737-24-1106-R3 (ACTIVE) SB

737-24-1108 SB 01 RECOMMENDED A/C STANDBY POWER SYSTEM - STATIC INVERTER CHANGE Not Applicable737-24-1108-R1 (ACTIVE)PRODUCTION LINE PRR35166-R

SBPRR

737-24-1110 SB 03 RECOMMENDED A/C NORMAL TRANSFER BUS CIRCUIT BREAKERS REPLACEMENT Rejected by Operator737-24-1110-R3 (ACTIVE)PRODUCTION LINE PRR35005-82

SBPRR

This Document SUPERSEDES 737-24-1110/SB Rev.02

737-24-1110 SB 01 RECOMMENDED A/C NORMAL TRANSFER BUS CIRCUIT BREAKERS REPLACEMENT Superseded (Superseded / SpecialText: This Aircraft is NotApplicable due to PRR35005-82)

737-24-1110-R3 (ACTIVE)PRODUCTION LINE PRR35005-82

SBPRR

This Document SUPERSEDES 737-24-1110/SB Rev.00This Document has been SUPERSEDED BY 737-24-1110/SB Rev.02





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1110 SB 02 RECOMMENDED A/C NORMAL TRANSFER BUS CIRCUIT BREAKERS REPLACEMENT Superseded (Superseded / Special

Text: This Aircraft is NotApplicable due to PRR35005-82)


SBPRR


737-24-1110 SB 00 RECOMMENDED A/C NORMAL TRANSFER BUS CIRCUIT BREAKERS REPLACEMENT Superseded (Superseded / SpecialText: This Aircraft is NotApplicable due to PRR35005-82)

PRODUCTION LINE PRR35005-82 PRRThis Document has been SUPERSEDED BY 737-24-1110/SB Rev.01

737-24-1115 SB 02 OPTIONAL A/C MAIN POWER CIRCUIT BREAKER AUXILIARY CONTACT WIRING CHANGE Not Applicable737-24-1115-R2 (ACTIVE)737-SRP-24-0035 (REF)PRODUCTION LINE PRR35005-165

SBSRPPRR

Reason for this StatusVSCF NOT INSTALLED

737-24-1123 SB 01 RECOMMENDED A/C ENG GENERATOR CIRCUIT BRK AUXILIARY CONTACT WIRING CHANGE Rejected by Operator737-24-1115 (REF)737-24-1123-1 (ACTIVE)737-24-1124 (REF)737-SRP-24-0001 (REF)

SBSBSBSRP





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1124 SB 00 RECOMMENDED A/C MAIN POWER CIRCUIT BREAKER AUXILIARY CONTACT WIRING CHANGE Superseded (Superseded)

737-24-1111 (REF)737-24-1115 (REF)737-24-1123 (REF)737-24-1124-R0 (ACTIVE)

SBSBSBSB


737-24-1124 SB 01 RECOMMENDED A/C MAIN POWER CIRCUIT BREAKER AUXILIARY CONTACT WIRING CHANGE Rejected by Operator737-24-1111 (REF)737-24-1115 (REF)737-24-1123 (REF)737-24-1124-R0 (ACTIVE)

SBSBSBSB


737-24-1145 SB 00 MANDATORY A/C AD* INST. OF IN-FLIGHT. ENT SYSTEM CB, RELAY AND WIRING Not Applicable by Serial NumberThe AC that are Not Applicable have this Status due to PRR35428-R.737-SRP-24-0093 (REF)PRR35428-R

SRPPRR

0000

737-24-1163 SB 02 RECOMMENDED A/C COOLING BLOWER INSPECT REPAIR AND PROTECTION OF WIRE BUNDLE Closed 27.Jun.2011 W/O:205149737-24-1163-R2 (ACTIVE)737-24A1164 (REF)

SBSB

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks27.Jun.2011 64534:00/H 37798/C 205149, N/A Was due at: 22.Jun.2011 PerfRev.:'02'

737-24-1174 SB 00 RECOMMENDED A/C DC GENERATION - DC GENERATION SYSTEM - REPLACEMENT OF THE 40 AMP-HOURBATTERY WITH 48 AMP-HOUR LOW MAINTENANCE BATTERY

Superseded (Not Applicable bySerial Number)

RejectedThere have not been any problem with existing battery.This Document has been SUPERSEDED BY 737-24-1174/SB Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24-1174 SB 01 RECOMMENDED A/C DC GENERATION - DC GENERATION SYSTEM - REPLACEMENT OF THE 40 AMP-HOUR

BATTERY WITH 48 AMP-HOUR LOW MAINTENANCE BATTERYNot Applicable by Serial Number


737-24-1189 SB 01 RECOMMENDED A/C ELECTRICAL POWER - ELECTRICAL POWER - INSTALL SPLIT SLEEVE ON WIREBUNDLES ON THE INBOARD LEADING EDGE OF THE LEFT AND RIGHT WINGS

Rejected by Operator

Rejected.SLB 737-SL-24-96 has been performed.Reason for this Status.

737-24A1009 SB 01 MANDATORY A/C *AD* REPLACE NAS 1068 NUTPLATES IN CIRCUIT BOARD IN COCKPIT Not Applicable1968-25-01 (ACTIVE)737-24A1009 (ACTIVE)

ADSB

737-24A1118 SB 00 RECOMMENDED A/C P6 CIRCUIT BREAKER DOOR FASTENER REPLACEMENT Closed 08.Feb.2000737-24A1118-R0 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24A1136 SB 02 RECOMMENDED COMP *AD* GENERATOR CONTROL UNIT REPLACEMENT Rejected by Operator

It has been decided to test the GCU every 600 hour as per AD1999-24-08 instead of replacing the GCU`s.1999-18-17 (SUPERSEDED)1999-24-08 (ACTIVE)37-AD-1999-24-08 (REPET-TASK)737-24A1136 (REF)737-24A1136-R1 (REF)737-24A1136-R2 (ACTIVE)737-SRP-24-0001 (REF)HAMILTON SUNDSTR.AVZ122-24-3HAMILTON SUNDSTR. AVZ22-24-1

ADADTASBSBSBSRPSBSB


948F458-3 / WG491 Pos=LH (KKM)Rejected by Operator / Reason: AUTOASSIGNED

948F458-5 / ZI1747 Pos=RH (KKM) Not Applicable / Reason: 89476948F458-5 / TT7773 Pos=AFT (KKM) Not Applicable / Reason: 275620

737-24A1164 SB 01 RECOMMENDED A/C INSTALL OF THE FIRE PROTECTION BLANKET AROUND THE RACEWAY WB Superseded (Cancelled)737-24A1164 IN 02 (REF)737-24A1164-R0737-24A1164-R1 (ACTIVE)PRODUCTION LINE PRR35005-26

SBSBSBPRR

This Document SUPERSEDES 737-24A1164/SB Rev.00This Document has been SUPERSEDED BY 737-24A1164/SB Rev.02Reason for this StatusManually deassigned after Document Cancelled/Superseeded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24A1164 SB 00 RECOMMENDED A/C INSTALL OF THE FIRE PROTECTION BLANKET AROUND THE RACEWAY WB Superseded (Cancelled)

737-24A1164 IN 02 (REF)737-24A1164-R0737-24A1164-R1 (ACTIVE)PRODUCTION LINE PRR35005-26

SBSBSBPRR

This Document has been SUPERSEDED BY 737-24A1164/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded

737-24A1164 SB 03 RECOMMENDED A/C ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTIONS - INSTALLATION THE FIREPROTECTION BLANKET AROUND THE RACEWAY WIRE BUNDLES

See prev. Docstatus

COMPLIANCE INFORMATION RELATED TO THIS REVISION (R03)No more work is necessary on airplanes changed in accordance withRevision 2 of this service bulletin.This Document SUPERSEDES 737-24A1164/SB Rev.02

737-24A1164 SB 02 RECOMMENDED A/C ELECTRICAL POWER - ELECTRICAL LOAD DISTRIBUTIONS - INSTALLATION THE FIREPROTECTION BLANKET AROUND THE RACEWAY WIRE BUNDLES

Superseded (Closed 28.Jun.2011W/O:205197)

This Document SUPERSEDES 737-24A1164/SB Rev.01This Document has been SUPERSEDED BY 737-24A1164/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Jun.2011 64534:00/H 37798/C 205197, N/A Was due at: 05.Jul.2012 PerfRev.:'02'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-24A1166 SB 04 MANDATORY A/C *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL AND

REPLACEMENT OF THE STATIC INVERTER MODULENot Applicable

This document is applicable to:737CL: All LN#.PRR35005-265RS PRR 00This Document SUPERSEDES 737-24A1166/SB Rev.03Perform BEFORE 31.Jul.2013

737-24A1166/SB Rev.04 *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL ANDREPLACEMENT OF THE STATIC INVERTER MODULE

Not Applicable

This Document SUPERSEDES 737-24A1166/SB Rev.03> 737-24A1166-01/EO* Rev.00 *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL AND

REPLACEMENT OF THE STATIC INVERTER MODULENot Applicable


39B168-1-C / 3427 Pos=E&E (KKM)Not Applicable / Reason: AUTOASSIGNED

> 737-24A1166-02/EO* Rev.00 *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL ANDREPLACEMENT OF THE STATIC INVERTER MODULE

Not Applicable / Special Text: Notapplicable due to SB effectivity.

Reason for this StatusNOT APPLIC DUE TO PART NOT INST.

737-24A1166 SB 03 MANDATORY A/C *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL ANDREPLACEMENT OF THE STATIC INVERTER MODULE

Superseded (Not Applicable)

PRR35005-265RS PRR 00This Document has been SUPERSEDED BY 737-24A1166/SB Rev.04Reason for this StatusNOT APPLIC DUE TO PART NOT INST.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1231 SB 01 MANDATORY A/C *AD* LAVATORIES - AFT LAVATORY PARTITION BEAM, SAW CUT INSP. Not Applicable by Serial Number

1989-12-02 (ACTIVE)737-25-1231 (REF)737-25-1231-R1 (ACTIVE)SBB 737-25-1231 (INSP-TASK)

ADSBSBTA


737-25-1231 SB 00 MANDATORY A/C *AD* LAVATORIES - AFT LAVATORY PARTITION BEAM, SAW CUT INSP. Superseded (Not Applicable bySerial Number)

1989-12-02 (ACTIVE)737-25-1231 (REF)737-25-1231-R1 (ACTIVE)SBB 737-25-1231 (INSP-TASK)

ADSBSBTA


737-25-1248 SB 02 RECOMMENDED A/C E-2 AND E-3 ELECTRICAL/ELECTRONIC RACK MOISTURE SHROUD REPL Rejected by Operator737-25-1248-R1 (ACTIVE) SBThis Document SUPERSEDES 737-25-1248/SB Rev.01

737-25-1248 SB 01 RECOMMENDED A/C E-2 AND E-3 ELECTRICAL/ELECTRONIC RACK MOISTURE SHROUD REPL Superseded (Superseded)737-25-1248-R1 (ACTIVE) SBThis Document SUPERSEDES 737-25-1248/SB Rev.00This Document has been SUPERSEDED BY 737-25-1248/SB Rev.02

737-25-1248 SB 00 RECOMMENDED A/C E-2 AND E-3 ELECTRICAL/ELECTRONIC RACK MOISTURE SHROUD REPL Superseded (Superseded)737-25-1248-R1 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-25-1248/SB Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1254 SB 00 RECOMMENDED A/C FORWARD AND AFT COMPARTMENT DOOR INSULATION FLAME RESISTANCE Superseded (Superseded)

737-25-1254-R3 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-25-1254/SB Rev.01Reason for this StatusREJECTED BY PREVIOUS OPERATOR

737-25-1254 SB 03 RECOMMENDED A/C FORWARD AND AFT COMPARTMENT DOOR INSULATION FLAME RESISTANCE See prev. Docstatus737-25-1254-R3 (ACTIVE) SBThis Document SUPERSEDES 737-25-1254/SB Rev.02Reason for this StatusDATUM AIRCRAFT MODIFIED BY SB 737-25-1254 REV.:02

737-25-1254 SB 01 RECOMMENDED A/C FORWARD AND AFT COMPARTMENT DOOR INSULATION FLAME RESISTANCE Superseded (Superseded)737-25-1254-R3 (ACTIVE) SBThis Document SUPERSEDES 737-25-1254/SB Rev.00This Document has been SUPERSEDED BY 737-25-1254/SB Rev.02Reason for this StatusREJECTED BY PREVIOUS OPERATOR

737-25-1254 SB 02 RECOMMENDED A/C FORWARD AND AFT COMPARTMENT DOOR INSULATION FLAME RESISTANCE Superseded (Closed 25.Feb.1992)737-25-1254-R3 (ACTIVE) SBThis Document SUPERSEDES 737-25-1254/SB Rev.01This Document has been SUPERSEDED BY 737-25-1254/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

25.Feb.1992REF MALEVSB LIST

Reason: REF MALEV SB LIST

Reason for this StatusREF MALEV SB LIST





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1259 SB 00 RECOMMENDED A/C OVERHEAD STOWAGE COMPARTMENT - FITTING Not Applicable by Serial Number

This document is applicable to LN# 1001-1750, the following LN# areNot Applicable per PRR 34838.737-25-1259-R0 (ACTIVE)PRODUCTION LINE PRR34838

SBPRR

737-25-1260 SB 00 RECOMMENDED A/C FORWARD SERVICE AND ENTRY DOOR ESCAPE SLIDES - INFL VALVE Not Applicable by Serial Number102-25-17 (REF-AIR CRUISERS)737-25-1260-R0 (ACTIVE)

SBSB

737-25-1266 SB 00 MANDATORY A/C *AD* EQUIPMENT FURNISHING - MAG. STBY COMPASS LINER, REPLACE Not Applicable by Serial Number1991-07-14 (ACTIVE)737-25-1266-R0 (ACTIVE)SBB 737-25-1266 (MOD TASK)

ADSBTA

737-25-1274 SB 04 MANDATORY A/C *AD* INSPECTION & REWORK OF FORWAD LOWERED CEILING PANEL Closed 03.May.1994Mod appl.: LN# 1001-2089 The following LN# are Not Applicable refPRR34963.1990-25-14 (ACTIVE)737-25-1274-R0 (REF)737-25-1274-R1 (REF)737-25-1274-R2 (REF)737-25-1274-R3 (REF)737-25-1274-R4 (ACTIVE)PRODUCTION LINE PRR34963

ADSBSBSBSBSBPRR


03.May.1994PerfRev.:'NOTE' / Reason: DELIVERYDOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1292 SB 00 RECOMMENDED A/C EQUIPMENT/FURNISHINGS - EMERGENCY - ESCAPE SLIDE ASSEMBLY - FORWARD

DOOR ESCAPE SLIDE MODIFICATIONRejected by Operator

Perform within an unlimited threshold.737-25-1292/SB Rev.00 EQUIPMENT/FURNISHINGS - EMERGENCY - ESCAPE SLIDE ASSEMBLY - FORWARD

DOOR ESCAPE SLIDE MODIFICATIONRejected by Operator

> 737-25-1292-01/EO* Rev.00 EQUIPMENT/FURNISHINGS - EMERGENCY - ESCAPE SLIDE ASSEMBLY - FORWARDDOOR ESCAPE SLIDE MODIFICATION


Reason for this StatusREJECTED BY PREVIOUS OPERATOR

737-25-1294 SB 00 MANDATORY A/C *AD* CHANGE OF FORTY-FIVE INCH OVERHEAD STOWAGE COMPARTMENT Not Applicable by Serial Number1992-19-16 (ACTIVE)737-25-1294-R0 (ACTIVE)PRODUCTION LINE PRR35041-2RSBB 737-25A1283-R2 (REF)

ADSBPRRSB

737-25-1298 SB 00 RECOMMENDED A/C INST. OF WALL MOUNTED ATTENDANT SEAT HEADREST INDEXING BRACK Closed 20.Jan.1993Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

20.Jan.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-25-1310 SB 00 RECOMMENDED A/C PASSENGER CABIN - SCULPTURED CEILING PANELS GAP IMPROVEMENT Rejected by Operator737-25-1310-R0 (ACTIVE) SBReason for this StatusCOMPLIANCE: NOT EMBODIED, NO ACTION





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1317 SB 00 RECOMMENDED A/C MOISTURE SHROUD INSTALLATION ON THE E1 AND E3-5 RACKS Superseded (Superseded)

THIS SB HAS BEEN REPLACED BY SB 737-25-1364.737-25-1317-R1 (ACTIVE)PRODUCTION LINE PRR35005-75

SBPRR


737-25-1317 SB 01 RECOMMENDED A/C MOISTURE SHROUD INSTALLATION ON THE E1 AND E3-5 RACKS Cancelled (Cancelled)THIS SB HAS BEEN REPLACED BY SB 737-25-1364.737-25-1317-R1 (ACTIVE)PRODUCTION LINE PRR35005-75

SBPRR

This Document SUPERSEDES 737-25-1317/SB Rev.00This Document has been CANCELLED BY 737-25A1364/SB Rev.00

737-25-1318 SB 00 RECOMMENDED A/C INSPECTION/REPLACEMENT OF DIAGONAL SUPPORT ASSEMBLIES Closed 08.Dec.1995737-25-1318-R0 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1322 SB 02 MANDATORY A/C *AD* DOOR HANDLE MOUNTING HUB ASSEMBLY REPLACEMENT. Closed 08.Dec.1995

This mod is applicable to LN# 1-2650. The following LN# are NotApplicable due to PRR35260.2000-14-13 (ACTIVE)737-25-1322-R0 (REF)737-25-1322-R1 (REF)737-25-1322-R2 (ACTIVE)PRODUCTION LINE PRR35260SBB 737-25-1322 (MOD TASK)

ADSBSBSBPRRTA




737-25-1324 SB 00 OPTIONAL A/C EQUIPMENT/FURNISHINGS - EMERGENCY - ESCAPE EQUIPMENT - ADDITION OFVELCRO TAPES TO SLIDE INSTALLATION ON FORWARD ENTRY AND SERVICE DOORS

Not Applicable

This SB has been issued to decrease wear damage to the girt of theforward evacuation slides.Reason for this StatusNOT APPLICABLE DUE TO THE INSTALLED SLIDES

737-25-1329 SB 00 RECOMMENDED A/C ATTACHMENT OF SIDEWALL INSULATION BLANKETS Not Applicable737-25-1329-R0 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1330 SB 00 RECOMMENDED A/C OVERHEAD STOWAGE BIN WEIGHT LIMIT IN 60 INCH Superseded (Closed 16.Feb.1996)

737-25-1330-R0 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-25-1330/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-25-1330 SB 01 RECOMMENDED A/C OVERHEAD STOWAGE BIN WEIGHT LIMIT IN 60 INCH See prev. Docstatus737-25-1330-R0 (ACTIVE) SBThis Document SUPERSEDES 737-25-1330/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks16.Feb.1996 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC WO:

737-25-1331 SB 00 RECOMMENDED A/C REPLACEMENT OF THE WINDOW SHADE IN THE OVERWING EXIT HATCH Not Applicable737-25-1331-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1334 SB 00 MANDATORY A/C *AD* FLIGHT COM. EQUIPMENT - EXAMINE SEAT TRACK ALIGNMENT Closed 24.Jul.1997

1998-03-10 (ACTIVE)737-25-1334-R1 (ACTIVE)737-25-1334-RO (REF)737-SRP-25-0092 (REF)PRODUCTION LINEPRR35005-158R

AD

SB

SB

SRP

PRR


24.Jul.1997PerfRev.:'NOTE' / Reason: DELIVERYDOC.


737-25-1334 SB 01 MANDATORY A/C FLIGHT COMPARTMENT EQUIPMENT - EXAMINE SEAT TRACK ALIGNMENT Closed 24.Jul.19971997-15-06 (SUPERSEDED)1998-03-10 (ACTIVE)737-25A1334-R1 (ACTIVE)PRODUCTION LINEPRR35005-158R

AD

AD

SB

PRR 00

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks24.Jul.1997 PerfRev.:'NOTE' / Reason: DEL DOCSReason for this StatusDEL DOCS

737-25-1365 SB 00 RECOMMENDED A/C ELECTRONIC COMPARTMENT-E/E BAY - INSTALL DRIP LOOP Rejected by Operator737-25-1365-R0 (ACTIVE)PRODUCTION LINE PRR35402-2

SBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1371 SB 03 MANDATORY A/C PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Not Applicable by Serial Number

2001-11-11737-25-1371-R0 (REF)737-25-1371-R1 (REF)737-25-1371-R2 (REF)737-25-1371-R3 (ACTIVE)AVIO INT 180/A184-01 (REF)AVIO INT 184/E23-01-R1 (REF)

ADSBSBSBSBSBSB

00


737-25-1371 SB 02 MANDATORY A/C PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Superseded (Not Applicable bySerial Number)


ADSBSBSBSBSBSB

00






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1371 SB 01 MANDATORY A/C PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Superseded (Not Applicable by

Serial Number)2001-11-11737-25-1371-R0 (REF)737-25-1371-R1 (REF)737-25-1371-R2 (REF)737-25-1371-R3 (ACTIVE)AVIO INT 180/A184-01 (REF)AVIO INT 184/E23-01-R1 (REF)

ADSBSBSBSBSBSB

00


737-25-1371 SB 00 MANDATORY A/C PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Superseded (Not Applicable bySerial Number)


ADSBSBSBSBSBSB

00


737-25-1394 SB 02 RECOMMENDED A/C EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - REPLACEMENT OFTHE OXYGEN GENERATOR ACTUATOR CAM HOUSINGS

Cancelled (Not Applicable by SerialNumber)

This SB is only revised to inform that it is replaced by SB737-25-1548.This Document SUPERSEDES 737-25-1394/SB Rev.01This Document has been CANCELLED BY 737-25-1548/SB Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1394 SB 01 RECOMMENDED A/C REPL. OF THE OXYGEN GENERATOR ACTUATOR CAM HOUSINGS Superseded (Not Applicable by

Serial Number)This mod is entered only because it is performed when SBB 737-25-1548is parformed. SBB 737-25-1548 will accomplish this modification.737-25-1394 IN 02 (REF) SBThis Document SUPERSEDES 737-25-1394/SB Rev.00This Document has been SUPERSEDED BY 737-25-1394/SB Rev.02

737-25-1394 SB 00 RECOMMENDED A/C REPL. OF THE OXYGEN GENERATOR ACTUATOR CAM HOUSINGS Superseded (Not Applicable bySerial Number)

737-25-1394 IN 02 (REF)737-25-1394-R0 (REF)737-25-1394-R1 (ACTIVE)SBB 737-25-1394 (MOD-TASK)

SBSBSBTA


737-25-1405 SB 01 MANDATORY A/C *AD* ESCAPE SLIDE (DOOR-MOUNTED) LATCH ASSEMBLY MODIFICATION Closed 28.Aug.20042001-15-01 (ACTIVE)737-25-1405-R1 (REF)737-25-1405-R2 (ACTIVE)737-25-1405-RO (REF)737-SRP-25-0150 (REF)SBB 737-25-1405 (MOD-TASK)

ADSBSBSBSRPTA


28.Aug.2004 44948:00/H 22546/CPerfRev.:'NOTE' / Reason: KKM 150238ITEM: 1






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1412 SB 03 MANDATORY A/C **AD* OBSERVER/ATTENDANT SHOULDER RESTRAINT SYSTEM ATTACHMEN Not Applicable by Serial Number

This mod is applicable to LN# 596-3110 with excemptions. Thefollowing LN# are Not Applicable per MRR3259-1295.2006-26-13 (ACTIVE)737-25-1412-R0 (REF)737-25-1412-R1 (REF)737-25-1412-R2 (REF)737-25-1412-R3 (ACTIVE)PRODUCTION MRR3259-1295.

ADSBSBSBSBPRR 00

737-25-1430 SB 00 MANDATORY A/C EQUIPMENT AND FURNISHINGS - EMERGENCY - FORWARD ENTRY AND SERVICEDOOR REPLACEMENT OF THE ESCAPE SLIDE COMPARTMENT HINGE

Superseded (Superseded)

2004-02-08737-25-1430PRODUCTION LINE PRR35431-R

ADSBPRR

000100


737-25-1430 SB 01 MANDATORY A/C ESCAPE SLIDE COMPARTMENT HINGE ASSEMBLY REPLACEMENT Closed 08.Mar.20052004-02-08737-25-1430PRODUCTION LINE PRR35431-R

ADSBPRR

000100


08.Mar.2005 46130:00/H 23575/CPerfRev.:'NOTE' / Reason: KKM 150401ITEM: 1






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1434 SB 00 MANDATORY A/C *AD* ESCAPE SLIDE AFT LATCH CABLE ASSY MOUNTING FASTENERS Closed 08.Mar.2005

2004-03-34 (SUPERSEDED)2004-03-34-R1 (ACTIVE)

ADAD




737-25-1438 SB 02 MANDATORY A/C *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Superseded (Not Applicable)2006-12-06 (ACTIVE)25-442 REV. F (DRIESSEN)37-25-046 (REF)737-25-1438-R0 (REF)737-25-1438-R1 (REF)737-25-1438-R2 (REF)737-25-1438-R3 (REF)737-25-1438-R4 (ACTIVE)SBB 737-25-1438 (MOD-TASK)

ADSBEODSBSBSBSBSBTA

This Document SUPERSEDES 737-25-1438/SB Rev.01This Document has been SUPERSEDED BY 737-25-1438/SB Rev.03Reason for this StatusAFFECTED EQIPMENT NOT INSTALL





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1438 SB 00 MANDATORY A/C *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Superseded (Superseded)

2006-12-06 (ACTIVE)25-442 REV. F (DRIESSEN)37-25-046 (REF)737-25-1438-R0 (REF)737-25-1438-R1 (REF)737-25-1438-R2 (REF)737-25-1438-R3 (REF)737-25-1438-R4 (ACTIVE)SBB 737-25-1438 (MOD-TASK)

ADSBEODSBSBSBSBSBTA



ADSBEODSBSBSBSBSBTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1438 SB 04 MANDATORY A/C *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not Applicable

737-300/400/500 airplanes with Driessen or Showa galleys installed.Ref TO 37-25-046 for galley type installed.2006-12-06 (ACTIVE)25-442 REV. F (DRIESSEN)37-25-046 (REF)737-25-1438-R0 (REF)737-25-1438-R1 (REF)737-25-1438-R2 (REF)737-25-1438-R3 (REF)737-25-1438-R4 (ACTIVE)

ADSBEODSBSBSBSBSB

This Document SUPERSEDES 737-25-1438/SB Rev.03Reason for this StatusAFFECTED EQIPMENT NOT INSTALL


ADSBEODSBSBSBSBSBTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1455 SB 00 OPTIONAL A/C EMERGENCY EQUIPMENT - SMOKE HOOD INSPECTION/ REPLACEMENT Not Applicable / Special Text: NAS

does not install B/E PBE, NASinstalls Draeger PBE.

119003-35-3 (REF)737-25-1455 (ACTIVE)737-SRP-25-0190 (REF)PRODUCTION LINEPRR35005-247RS

SB

SB

SRP

PRR

737-25-1507 SB 01 OPTIONAL A/C FLIGHT COMPARTMENT DOOR REPLACEMENT (COLLECTOR-SB) Not Applicable by Serial Number737-25-1507-R1 (COLECTOR-SB)PRODUCTION LINEMC2518MK3019ST01335LA (ACTIVE)

SB

PRR

STC

737-25-1512 SB 00 RECOMMENDED A/C FLIGHT COMPARTMENT DOOR REPLACEMENT.(REINFORCED DOOR) Not Applicable by Serial Number2003-66 (REF)737-25-1512-R0 (ACTIVE)ADVISORY CIRCULARS AC25.795-1ADVISORY CIRCULARS AC25.795-2SBB 737-25-1512 (MOD TASK)ST01335LA (ACTIVE)

LDP

SB

DOCR

DOCR

TA

STC





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1529 SB 02 MANDATORY A/C FLIGHT COMPARTMENT DOOR REPLACEMENT (REINFORCED DOOR) Not Applicable by Serial Number

737-25-1529-R2 (ACTIVE)ADVISORY CIRCULARS AC25.795-1ADVISORY CIRCULARS AC25.795-2PRODUCTION MC2518MK3019ST01335LA

SB

DOCR

DOCR

PRR

STC 00

737-25-1548 SB 01 MANDATORY A/C EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - MODIFICATION OFTHE OXYGEN ACTIVATION MECHANISM


SB 737-25-1548 superceeds/replaces SB 737-25-1239 Rev:00 and Rev:01.

Compliance:This SB ensures compliance with AD 2007-07-02 § (f)2007-07-02 (ACTIVE)737-25-1548 IN 01 (REF)737-25-1548 IN 02 (REF)737-25-1548 IN 03 (ACTIVE)737-25-1548-R0 (ACTIVE)MRR3254-1596 OTH000

ADSBSBSBSBPRR

This Document CANCELS 737-25-1394/SB Rev.02This Document SUPERSEDES 737-25-1548/SB Rev.00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1548 SB 00 MANDATORY A/C MOD OF THE PSU OXYGEN ACTIVATION MECHANISM Superseded (Not Applicable by

Serial Number)Compliance:This SB ensures compliance with AD 2007-07-02 § (f)2007-07-02 (ACTIVE)737-25-1548 IN 01 (REF)737-25-1548 IN 02 (REF)737-25-1548 IN 03 (ACTIVE)737-25-1548-R0 (ACTIVE)MRR3254-1596 OTH000

ADSBSBSBSBPRR


737-25-1567 SB 01 MANDATORY A/C SLIDE COMPARTMENT MODIFICATION, FWD SERVICE DOOR Closed 02.Nov.2012 W/O:273620This document is applicable to all 737CL.

Compliance:This SB ensures compliance with AD 2008-03-20 § (f)2008-03-20737-FTD-25-02007

ADFTD

0000

This Document SUPERSEDES 737-25-1567/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks02.Nov.2012 68139:00/H 40570/C 273620, N/A Was due at: 15.Mar.2013 PerfRev.:'01'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25-1567 SB 00 MANDATORY A/C SLIDE COMPARTMENT MODIFICATION, FWD SERVICE DOOR Superseded (Cancelled)

2008-03-20 (ACTIVE)737-25-1567 R0 (REF)737-25-1567 R1 (ACTIVE)SBB 737-25-1567 (MAINT TASK)

ADSBSBTA

This Document has been SUPERSEDED BY 737-25-1567/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded

737-25-1572 SB 00 MANDATORY A/C *AD* EQUIPMENT/FURNISHINGS - INSULATION BLANKETS, REPL OF Not ApplicableOnly MSN: 24256 in NAS fleet is applicable.All other AC are Not Applicable by LN# per Boeing SB.737-SRP-25-0237 (REF)PRODUCTION PRR35005-267RS

SRPPRR

Reason for this StatusNOT APPLICABLE BY VARIABLE NUMBER. AFFECTED INSULATION TYPE NOT INST.

737-25-1599 SB 00 OPTIONAL A/C EQUIPMENT/FURNISHINGS - PASSENGER SEAT - MOVE THE PASSENGER Not ApplicableThis SB is only applicable to certain B737-700 aircraft. Thereforethe SB is not applicable to NAS aircraft.2010-NM-058-AD2012-09-06737-25-1598737-53-1286

NPRMADSBSB

00000001

737-25-1643 SB 00 MANDATORY A/C EQUIPMENT/FURNISHINGS - ESCAPE SLIDES, STRAPS AND LANYARDS - CARGO DOOR,PERSONNEL SAFETY NET REPLACEMENT

Not Applicable

Applicable for 737-700C only. NAS does not operate the aircraft type.Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1182 SB 00 MANDATORY A/C *AD* EVACUATION SLIDE COMPARTMENT LATCH ASSEMBLY REPLACEMENT Not Applicable by Serial Number

1985-19-04 (SUPERSEDED)1985-25-04 (ACTIVE)1986-05-04 (ACTIVE)737-25A1182-R4 (ACTIVE)

ADADADSB

737-25A1221 SB 01 MANDATORY A/C *AD* FWD SERVICE/ENTRY DOOR ESCAPE SLIDE GIRT RETENTION MOD Not Applicable103-25-19-R8 (REF)1988-07-07 (SUPERSDED)1991-24-04 (SUPERSEDED)1996-18-04 (ACTIVE)737-25A1221-R0 (REF)737-25A1221-R1 (ACTIVE)PRODUCTION PRR34388SBB 737-25A1221 (MOD-TASK)

SBADADADSBSBPRRTA

Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1248 SB 02 RECOMMENDED A/C ELECT COMP E2 & E3 ELECT RACK MOISTURE SHROUD REPLACEMENT Closed 18.Feb.2014 W/O:489229

Document effectivity is LN# 1-2151.All NAS AC are Group 2 AC and performed through EO 737-25A1248-01.737-25-1248737-25-1248737-25A1248737-25A1248-01737-SRP-25-0276 (REF)PRODUCTION PRR34692

SBSBSBEOSRPPRR

000102000000

This Document SUPERSEDES 737-25A1248/SB Rev.01Perform WITHIN 1825/D (effective from 20.May.2009)

737-25A1248/SB Rev.02 ELECT COMP E2 & E3 ELECT RACK MOISTURE SHROUD REPLACEMENT Closed 18.Feb.2014 W/O:489229This Document SUPERSEDES 737-25A1248/SB Rev.01

> 737-25A1248-01/EO* Rev.00 ELECT COMP E2 & E3 ELECT RACK MOISTURE SHROUD REPLACEMENT GROUP 2 AC Closed 18.Feb.2014 W/O:489229Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks18.Feb.2014 71572:00/H 43151/C 489229, N/A Was due at: 19.May.2014 PerfRev.:'00'

737-25A1248 SB 01 RECOMMENDED A/C ELECT COMP E2 & E3 ELECT RACK MOISTURE SHROUD REPLACEMENT Superseded (Cancelled)737-25-1248737-25-1248737-25A1248737-SRP-25-0276 (REF)

SBSBSBSRP

000102

This Document has been SUPERSEDED BY 737-25A1248/SB Rev.02Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1270 SB 02 RECOMMENDED A/C FWD DOORS ESCAPE SLIDE LATCH CABLE ASSY REPLACEMENT Closed 28.Aug.2004

This SB is only related to AD 1990-12-11. This SB calls out a singleinspection, while the AD requires a repetitive inspection.1990-12-11737-25A1270737-25A1270PRODUCTION LINE PRR33890-78

ADSBSBPRR

00000100




737-25A1283 SB 02 MANDATORY A/C *AD* MODIFICATION OF OVERHEAD STOWAGE COMPARTMENT Closed 31.Mar.1993This mod is applicable to LN# 991-2095. The following LN# are NotApplicable per PRR35041-2R.1992-19-16 (ACTIVE)737-25-1291 (REF)737-25-1294 (REF)PRODUCTION LINE PRR35041-2RSBB 737-25A1283-R2 (ACTIVE)

ADSBSBPRRSB


31.Mar.1993PerfRev.:'NOTE' / Reason: DELIVERYDOCS

Reason for this StatusDELIVERY DOCS





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1299 SB 00 MANDATORY A/C *AD* COCKPIT WIRE BUNDLES DOOR HEADER SUPPORT BRACKET ASSEM Closed 31.Mar.1993

This document is applicable to LN# 1001-2256.1992-04-07 (ACTIVE)37-AD-1992-04-07 (REPETITIVE)737-25A1299 NSC 2 (REF)737-25A1299-R0 (REF)737-25A1299-R1 (ACTIVE)SBB 737-25A1299 (MOD-TASK)

ADTASBSBSBTA

Perform within an unlimited threshold.737-25A1299/SB Rev.00 *AD* COCKPIT WIRE BUNDLES DOOR HEADER SUPPORT BRACKET ASSEM Closed 31.Mar.1993> 737-25A1299-01/EO* Rev.00 *AD* COCKPIT WIRE BUNDLES DOOR HEADER SUPPORT BRACKET ASSEM Closed 31.Mar.1993


31.Mar.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC.


> AD-1992-04-07/EO* Rev.00 *AD* *AD*WIREBUNDLE INSTALLATION ABOVE COCKPIT-TO-CABIN DOO Not Applicable by Serial Number

737-25A1333 SB 00 RECOMMENDED A/C CHANGE SHARP CORNERS OF LINING SUPPORT PAN ON AFT DOORS Closed 24.Jan.1997737-25-1180 (REF)737-25A1333-R0 (ACTIVE)SBB 737-25A1333 (INSP-TASK)

SBSBTA








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1344 SB 00 RECOMMENDED A/C EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT - FLIGHT COMPARTM Superseded (Not Applicable by

Serial Number)Rejected due to NAS installing IPECO buckle and restraints.737-25A1344 (SUPERSEEDED)737-25A1344 R01 (ACTIVE)SBB 737-25A1344 (MAINT TASK)

SBSBTA


737-25A1344 SB 01 RECOMMENDED A/C EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT - FLIGHT COMPARTM Not Applicable by Serial NumberRejected due to NAS installing IPECO buckle and restraints.737-25A1344 (SUPERSEEDED)737-25A1344 R01 (ACTIVE)SBB 737-25A1344 (MAINT TASK)

SBSBTA


737-25A1363 SB 01 MANDATORY A/C *AD* CREW SEATS, REAR TRACK LOCK BRACKET BOLTS INSPECTION Superseded (Closed 12.Jun.2004)2004-04-03 (ACTIVE)737-25A1263-R0 (REF)737-25A1363-R1 (REF)737-25A1363-R2 (ACTIVE)IPECO A001-25-47 (REF)

ADSBSBSBSB

This Document SUPERSEDES 737-25A1363/SB Rev.00This Document has been SUPERSEDED BY 737-25A1363/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

12.Jun.2004 44399:00/H 22146/CPerfRev.:'NOTE' / Reason: KKM 150228ITEM: 1






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1363 SB 02 MANDATORY A/C *AD* CREW SEATS, REAR TRACK LOCK BRACKET BOLTS INSPECTION Superseded (See prev. Docstatus)

2004-04-03 (ACTIVE)737-25A1263-R0 (REF)737-25A1363-R1 (REF)737-25A1363-R2 (ACTIVE)IPECO A001-25-47 (REF)

ADSBSBSBSB

This Document SUPERSEDES 737-25A1363/SB Rev.01This Document has been SUPERSEDED BY 737-25A1363/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks12.Jun.2004 44399:00/H 22146/C PerfRev.:'NOTE'Reason for this StatusKKM 150228 ITEM: 1

737-25A1363 SB 00 MANDATORY A/C *AD* CREW SEATS, REAR TRACK LOCK BRACKET BOLTS INSPECTION Superseded (Superseded)2004-04-03 (ACTIVE)737-25A1263-R0 (REF)737-25A1363-R1 (REF)737-25A1363-R2 (ACTIVE)IPECO A001-25-47 (REF)

ADSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1363 SB 03 MANDATORY A/C EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT - CAPTAIN AND FIRST See prev. Docstatus

Compliance:No more work required by rev.:03 of SB. All NAS AC modified byprevious revisions of SB.2004-04-03737-25A1263737-25A1363737-25A1363IPECO A001-25-47 (REF)

ADSBSBSBSB

0000010200

This Document SUPERSEDES 737-25A1363/SB Rev.02Reason for this StatusTHE AIRCRAFT HAS BEEN MODIFIED BY PREVIOUS REVISION OF THE SB

737-25A1364 SB 00 RECOMMENDED A/C E/E BAY LIQUID CONTAMINATION PROTECTION IMPROVEMENTS - E1 SH Superseded (Cancelled)737-25-1317 (REPLACED)737-SRP-25-0276 (REF)PRODUCTION PRR35402-R

SBSRPPRR

This Document CANCELS 737-25-1317/SB Rev.01This Document has been SUPERSEDED BY 737-25A1364/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-25A1364 SB 01 RECOMMENDED A/C EQUIPMENT/FURNISHINGS - CARGO AND ACCESSORY COMPARTMENTS -

ELECTRONIC COMPARTMENT - E/E BAY LIQUID CONTAMINATION PROTECTIONIMPROVEMENTS

Closed 18.Feb.2014 W/O:489230

737-25-1317 (REPLACED)737-25-1364737-25-1364 IN-01737-25-1364 IN-02737-SRP-25-0276 (REF)PRODUCTION PRR35402-R

SBSBSBSBSRPPRR

000000000000

This Document SUPERSEDES 737-25A1364/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks18.Feb.2014 71572:00/H 43151/C 489230, N/A Was due at: 20.May.2014 PerfRev.:'01'

737-26-1055 SB 02 MANDATORY A/C *AD* FIRE PROTECTION - ENGINE FIRE DETECTOR REPLACEMENT Not Applicable by Serial NumberMod appl is LN# 1037 - 1717.The following LN# are Not Applicable per PRR33890-48.1990-15-14 (ACTIVE)737-26-1055-R0 (REF)737-26-1055-R1 (REF)737-26-1055-R2 (ACTIVE)PRODUCTION PRR33890-48SBB 737-26-1055 (MOD-TASK)

ADSBSBSBPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-26-1055 SB 00 MANDATORY A/C *AD* FIRE PROTECTION - ENGINE FIRE DETECTOR REPLACEMENT Superseded (Not Applicable by

Serial Number)Mod appl is LN# 1037 - 1717.The following LN# are Not Applicable per PRR33890-48.1990-15-14 (ACTIVE)737-26-1055-R0 (REF)737-26-1055-R1 (REF)737-26-1055-R2 (ACTIVE)PRODUCTION PRR33890-48SBB 737-26-1055 (MOD-TASK)

ADSBSBSBPRRTA


737-26-1055 SB 01 MANDATORY A/C *AD* FIRE PROTECTION - ENGINE FIRE DETECTOR REPLACEMENT Superseded (Not Applicable bySerial Number)

Mod appl is LN# 1037 - 1717.The following LN# are Not Applicable per PRR33890-48.1990-15-14 (ACTIVE)737-26-1055-R0 (REF)737-26-1055-R1 (REF)737-26-1055-R2 (ACTIVE)PRODUCTION PRR33890-48SBB 737-26-1055 (MOD-TASK)

ADSBSBSBPRRTA


737-26-1061 SB 00 RECOMMENDED A/C ENGINE FIRE EXTINGUISHING ELECTRIAL CONNECTOR IDENTIFICATION Not Applicable by Serial Number737-26-1061-RO (ACTIVE) SB

737-26-1063 SB 00 MANDATORY A/C *AD* ENG AND APU FIRE DETECTION ACCESSORY UNIT REPLACEMENT Not Applicable by Serial NumberPRODUCTION PRR34741 PRR 00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-26-1066 SB 00 RECOMMENDED A/C ENGINE FIRE EXT. HOSE AND TUBE REPLACEMENT Ex Factory


SBPRR

Reason for this StatusPRODUCTION PRR34716

737-26-1067 SB 01 MANDATORY A/C *AD* MODIFICATION OF ENGINE FIRE EXTINGUISHING SYSTEM WIRING Closed 27.Feb.1992This document is applicable to LN# 1001-1889. THe following LN# areNot Applicable per PRR34774.1991-09-12 (ACTIVE)PRODUCTION LINE PRR34774SBB 737-26-1067-R1 (ACTIVE)

ADPRRSB


27.Feb.1992PerfRev.:'NOTE' / Reason: DELIVERYDOC

Reason for this StatusDELIVERY DOC

737-26-1067 SB 00 MANDATORY A/C *AD* MODIFICATION OF ENGINE FIRE EXTINGUISHING SYSTEM WIRING Superseded (Superseded)1991-09-12 (ACTIVE)PRODUCTION LINE PRR34774SBB 737-26-1067-R1 (ACTIVE)

ADPRRSB


737-26-1070 SB 00 RECOMMENDED A/C FIRE PROTECTION - ENGINE AND APU FIRE CONTROL MODULE REPLACEMENT OF OpenNo safety or economic benefit. NAS will not implement this SB.Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-26-1072 SB 00 OPTIONAL A/C ENGINE FIRE DETECTION-CHANGES TO THE QUICK ENGINE CHANGE KIT Rejected by Operator

Rejected by previous operator.737-26-1072-R0PRODUCTION PRR35008-R

SBPRR


737-26-1079 SB 00 RECOMMENDED A/C ENG FIRE DET-WIRE CHANGE TO THE ENGINE DETECTOR WIRE BUNDLE Rejected by OperatorPRODUCTION LINE PRR35005-47 PRR 00

737-26-1114 SB 01 RECOMMENDED A/C FIRE DETECTION, FENWAL CONNECTORS IN MAIN WHEEL WELL Closed 07.Sep.2003737-26-1114-R0 (REF)737-26-1114-R1 (ACTIVE)737-SRP-26-0056S (REF)SBB 737-26-1114 (MOD-TASK)

SBSBSRPTA


07.Sep.2003 42719:00/H 20513/CPerfRev.:'NOTE' / Reason: KKM 150041ITEM: 1


737-26A1029 SB 03 MANDATORY A/C *AD* HTL FIRE EXTINGUISHER DISCHARGE OUTLETS Not Applicable by Serial NumberApplies to AC in range LN# 1-1062 with HTL firing extinguishersinstalled.1986-19-03 (ACTIVE)737-26A1029 (ACTIVE)

ADSB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-26A1082 SB 03 RECOMMENDED A/C FIRE DETECTION-CARGO COMPARTMENT SMOKE DETECTION INSTALL Closed 24.Mar.2000

737-26A1082-R3 (ACTIVE)PRODUCTION LINE PRR38060-15SBB 737-26A1082

SBPRRTA




737-26A1108 SB 01 MANDATORY A/C *AD* ENGINE & CARGO COMPT FIRE EXT BOTTLE HOSES INSPECTION Closed 10.Aug.2004 / Special Text:GROUP 4 OR 5 AIRPLANE

2003-23-05 (ACTIVE)737-26A1082 (REF)737-26A1108-R0 (REF)737-26A1108-R1 (ACTIVE)737-SRP-73-0028 (REF)SBB 737-26A1108 (MOD-TASK)

ADSBSBSBSRPTA




737-27-1154 SB 00 MANDATORY A/C *AD* FLIGHT CTRLS - AILERON CTRL CABLE PULLLEY BRACKET INSP. Not Applicable by Serial NumberThis document is applicable to LN# 1-1388. The following LN# are NotApplicable per Boeing SB.1997-03-14 (ACTIVE)737-27-1154-RO (ACTIVE)

ADSB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1155 SB 00 MANDATORY A/C *AD AILERON - CENTERING SPRING AND TRIM MECHANISM MOD. Not Applicable by Serial Number

This mod is applicable to LN# 1-1742. The following LN# are NotApplicable due to PRR34533737-27-1155 NSC-01737-27-1155 NSC-02737-27-1155 NSC-03PRODUCTION LINE PRR34533

SBSBSBPRR

00000000

737-27-1158 SB 00 RECOMMENDED A/C HORIZONTAL STAB TRIM CONTROL SYSTEM SWICH GUARD REPLACEMENT Closed 17.Sep.1991737-27-1158-R0 (ACTIVE)PRODUCTION LINE PRR34640

SBPRR


17.Sep.1991PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-27-1161 SB 02 MANDATORY A/C *AD* HORIZONTAL STAB. TRIM CONTROL SYSTEM-AUX. BRAKE REPLACE Closed 26.Feb.19921991-20-04 (ACTIVE)737-27-1161-R0 (REF)737-27-1161-R1 (REF)737-27-1161-R2 (ACTIVE)

ADSBSBSB


26.Feb.1992PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.

Reason for this StatusPREVIOUS OPERATOR DOC.

737-27-1163 SB 00 RECOMMENDED A/C ELEVATOR AND TAB CONTROL SYSTEM. BRACKET MODIFICATION Not Applicable by Serial Number737-27-1163-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1165 SB 00 RECOMMENDED A/C RUDDER TRIM KNOB & GUARD REPLACEMENT Superseded (Superseded)


SBPRR


737-27-1165 SB 01 RECOMMENDED A/C RUDDER TRIM KNOB & GUARD REPLACEMENT Closed 19.Apr.1991This document is applicable to LN# 1001-1865. The following LN# areNot Applicable per PRR33890-71.737-27-1165-R1 (ACTIVE)PRODUCTION LINE PRR33890-71

SBPRR




737-27-1171 SB 02 RECOMMENDED A/C BOLT REPLACEMENT ON THE ELEVATOR BYSS ASSY See prev. DocstatusDocument effectivity LN# 1436-1911.737-27-1171-R2 (ACTIVE) SBThis Document SUPERSEDES 737-27-1171/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks22.Mar.1995 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC WO:





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1171 SB 01 RECOMMENDED A/C BOLT REPLACEMENT ON THE ELEVATOR BYSS ASSY Superseded (See prev. Docstatus)

Document effectivity LN# 1436-1911.737-27-1171-R2 (ACTIVE) SBThis Document SUPERSEDES 737-27-1171/SB Rev.00This Document has been SUPERSEDED BY 737-27-1171/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-27-1171 SB 00 RECOMMENDED A/C BOLT REPLACEMENT ON THE ELEVATOR BYSS ASSY Superseded (Closed 22.Mar.1995)Document effectivity LN# 1436-1911.737-27-1171-R2 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-27-1171/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-27-1172 SB 00 RECOMMENDED A/C FLIGHT CONTROLS - CONTROL CABLES - FILLER BLOCK INSTALLATION Not ApplicableB737-500 Aircraft only.737-27-1072-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1174 SB 02 OPTIONAL A/C L/E FLAPS AND SLAT POSITION INDICATING SYSTEM - SWITCH REPL. Closed 18.Dec.2001

737-27-1174737-27-1174737-27-1174PRODUCTION LINE PRR33890-88

SBSBSBPRR

00010200




737-27-1175 SB 00 RECOMMENDED A/C LEADING EDGE FLAP CHANGES TO MAKE THE SYSTEM RELIABLE Rejected by Operator737-27-1175-R0 (ACTIVE)PRODUCTION LINE PRR33890-88

SBPRR

737-27-1182 SB 00 RECOMMENDED A/C FLIGHT CONTROLS - HOR. STAB. TRIM CONTR. SYS. - MAIN STAB TRIM ANDAUTOPILOT ACTUATOR, REPLACEMENT OF. INST OF ONE SINGLE ACTUATOR


This SB has been rejected by all previous operators.Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1185 SB 00 MANDATORY A/C RUDDER POWER CONTROL UNIT-SERVO VALVE REPLACEMENT Superseded (Not Applicable /

Special Text: This Aircraft is NotApplicable due to PRODUCTIONLINE PRR35153)

This modification is applicable for LN# 1-2453. The following LN# areNot Applicable ref PRR35153.

This modification is mandated by AD 1997-14-04 §b.1994-01-071997-14-04737-27-1185PRODUCTION LINE PRR35153

ADADSBPRR

00000100

This Document has been SUPERSEDED BY 737-27-1185/SB Rev.01Reason for this StatusSBB 737-27A1202

737-27-1185 SB 01 MANDATORY A/C RUDDER POWER CONTROL UNIT-SERVO VALVE REPLACEMENT Not ApplicableThis modification is applicable for LN# 1-2453. The following LN# areNot Applicable ref PRR35153.

This modification is mandated by AD 1997-14-04 §b.1994-01-071997-14-04737-27-1185PRODUCTION LINE PRR35153

ADADSBPRR

00000100

This Document SUPERSEDES 737-27-1185/SB Rev.00Reason for this StatusSBB 737-27A1202





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1186 SB 00 RECOMMENDED A/C SUPPORT BRACKETS FOR THE PROXIMITY SENSORS AT SLATS 3 AND 4 Not Applicable by Serial Number

Document effectivity is LN# 2380 - 2457.737-27-1186-R0PRODUCTION LINE PRR33890-88

SBPRR

737-27-1190 SB 00 RECOMMENDED A/C FLIGHT CONTROLS - FLIGHT CONTROLS MULTIPLE USE SYSTEM/UNITS -REPLACEMENT OF A CONTROL CABLE GUARD

Closed 08.Dec.1995

Document effectivity is LN# 1556 - 2641.737-27-1190-R0 (ACTIVE)PRODUCTION LINE PRR35005-102

SBPRR




737-27-1193 SB 00 RECOMMENDED A/C FLIGHT CONTROLS - FLIGHT CONTROLS MULTIPLE USE SYSTEM/UNITS -REPLACEMENT OF A CONTROL CABLE GUARD

Closed 18.Mar.2009

Document effectivity is LN# 1001 - 2763.737-27-1193 NSC 01 (REF)PRODUCTION LINE PRR35005-102

SBPRR

0000








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1197 SB 00 RECOMMENDED A/C REPL OF THE UPPER COVER ON THE ELEVATOR FEEL AND CENTERING Closed 02.Apr.2001

Document effectivity LN# 1001 - 2764.737-27-1197-R0 (ACTIVE)PRODUCTION LINE PRR35335

SBPRR




737-27-1200 SB 00 OPTIONAL A/C FLIGHT CONTROLS - TORQUE TUBE SAFETY AWARENESS, WHEEL WELL. Closed 15.Nov.2007Document effectivity LN# 1-2825.PRODUCTION PRR35005-162 PRR 00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

15.Nov.2007 54273:00/H 30097/CPerfRev.:'NOTE' / Reason: VERIFIED,NAS W/O #151137

Reason for this StatusVERIFIED, NAS W/O #151137

737-27-1203 SB 00 OPTIONAL A/C REPL OF THE SPRINGS IS THE ELEVATOR FEEL AND CENTERING UNIT Superseded (Superseded / SpecialText: This Aircraft is NotApplicable due to PRR 38060-3(PRODUCTION))

Document effectivity LN# 1001 - 3063.737-27-1197 (REF)737-27-1203-R2 (ACTIVE)737-27A1194 (REF)737-SL-27-127 (REF)PRR 38060-3 (PRODUCTION)

SBSBSBSLPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1203 SB 02 OPTIONAL A/C REPL OF THE SPRINGS IS THE ELEVATOR FEEL AND CENTERING UNIT Rejected by Operator

Document effectivity LN# 1001 - 3063.737-27-1197 (REF)737-27-1203-R2 (ACTIVE)737-27A1194 (REF)737-SL-27-127 (REF)PRR 38060-3 (PRODUCTION)

SBSBSBSLPRR


737-27-1203 SB 01 OPTIONAL A/C REPL OF THE SPRINGS IS THE ELEVATOR FEEL AND CENTERING UNIT Superseded (Superseded)Document effectivity LN# 1001 - 3063.737-27-1197 (REF)737-27-1203-R2 (ACTIVE)737-27A1194 (REF)737-SL-27-127 (REF)PRR 38060-3 (PRODUCTION)

SBSBSBSLPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1204 SB 02 OPTIONAL A/C HORIZONTAL STAB. TRIM CTRL SYST, REPL OF SHAFT & BEARARINGS Closed 29.Mar.2001

737-27-1204 IN 01 TO SBB R2737-27-1204 R2 (ACTIVE)737-27-1204-R0 (REF)737-27-1204-R1 (REF)PRODUCTION LINE PRR35375SBB 737-27-1204 (MOD-TASK)

SBSBSBSBPRRTA




737-27-1209 SB 00 RECOMMENDED A/C CONTROL WHEEL INTERFERENCE INSPECTION AND MODIFICATION Superseded (Superseded)Document effectivity LN# 1001 - 3035.737-27-1209-R2 (ACTIVE)PRODUCTION LINE MRR3277-1148

SBPRR

This Document has been SUPERSEDED BY 737-27-1209/SB Rev.01Reason for this StatusREJECTED BY PREVIOUS OPERATOR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1209 SB 01 RECOMMENDED A/C CONTROL WHEEL INTERFERENCE INSPECTION AND MODIFICATION Superseded (Closed 17.Nov.1999)

Document effectivity LN# 1001 - 3035.737-27-1209-R2 (ACTIVE)PRODUCTION LINE MRR3277-1148

SBPRR

This Document SUPERSEDES 737-27-1209/SB Rev.00This Document has been SUPERSEDED BY 737-27-1209/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

17.Nov.1999PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-27-1209 SB 02 RECOMMENDED A/C CONTROL WHEEL INTERFERENCE INSPECTION AND MODIFICATION See prev. DocstatusDocument effectivity LN# 1001 - 3035.737-27-1209-R2 (ACTIVE) SBThis Document SUPERSEDES 737-27-1209/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Nov.1999 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC WO:





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1211 SB 00 MANDATORY A/C *AD* REPL OF THE ROD ENDS FOR THE LEADING EDGE SLAT ACTUATOR Superseded (Closed 08.Dec.2001)

2000-02-03 (ACTIVE)737-27-1211-R3 (ACTIVE)PRODUCTION LINE PRR35005-175

ADSBPRR

This Document has been SUPERSEDED BY 737-27A1211/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.2001PerfRev.:'NOTE' / Reason: REPLACED BY737-27A1243

Reason for this StatusREPLACED BY 737-27A1243

737-27-1223 SB 00 MANDATORY A/C *AD* INSP. & REPL. OF AILERON TAB CONTROL ROD Not Applicable2002-10-12 (ACTIVE)37-SBB-27-1223 (MOD-TASK)737-27-1223 IN01 (REF)737-27-1223-RO (ACTIVE)

ADTASBSB

737-27-1223/SB Rev.00 *AD* INSP. & REPL. OF AILERON TAB CONTROL ROD Not Applicable> 737-27-1223/EO* Rev.00 *AD* *AD* 2002-10-12 REPL. OF AILERON TAB CONTROL ROD Not Applicable by Serial Number

This Document is terminated with implementation of 737-27-1223-01/EO Rev.00> 737-27-1223-01/EO* Rev.00 *AD* INSP. & REPL. OF AILERON TAB CONTROL ROD Closed 03.Apr.2001

This Document terminates 737-27-1223/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

03.Apr.2001PerfRev.:'NOTE' / Reason: DELEVIERYDOCS

Reason for this StatusDELEVIERY DOCS





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1231 SB 01 RECOMMENDED A/C FLAP AND HZT STABILIZER TRIM SYSTEMS - S245 FLAP LIMIT SWTH Rejected by Operator

737-27-1231 IN 02 (ACTIVE)737-27-1231-R1 (ACTIVE)737-SRP-27-0117 (REF)

SBSBSRP

737-27-1246 SB 01 MANDATORY A/C *AD* RUDDER & RUDDER TRIM CONTROL SYSTEM, WIRE PROVISIONS Closed 14.Mar.20052002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1246-R0 (REF)737-27-1246-R1 (ACTIVE)PRODUCTION LINE PRR35435-RSBB 737-27-1246 (MOD TASK)

ADADSBSBPRRTA








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1255 SB 03 MANDATORY A/C *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. Superseded (See prev. Docstatus)

2002-20-072002-20-072007-03-07737-27-1255737-27-1255737-27-1255737-27-1255737-27-1255 IN-03737-27-1255 IN-04

ADADADSBSBSBSBSBSB

000100010203040000

This Document SUPERSEDES 737-27-1255/SB Rev.02This Document has been SUPERSEDED BY 737-27-1255/SB Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150404 ITEM: 1





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1255 SB 02 MANDATORY A/C *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. Superseded (Closed 17.Mar.2005)

2002-20-07 (SUPERSEDED)2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1255 IN 03 (REF)737-27-1255 IN 04 (REF)737-27-1255-R0 (REF)737-27-1255-R1 (REF)737-27-1255-R2 (REF)737-27-1255-R3 (REF)

ADADADSBSBSBSBSBSB




737-27-1255 SB 00 MANDATORY A/C *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. Superseded (Superseded)2002-20-07 (SUPERSEDED)2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1255 IN 03 (REF)737-27-1255 IN 04 (REF)737-27-1255-R0 (REF)737-27-1255-R1 (REF)737-27-1255-R2 (REF)737-27-1255-R3 (REF)

ADADADSBSBSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1255 SB 04 MANDATORY A/C *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. See prev. Docstatus

2002-20-072002-20-072007-03-07737-27-1255737-27-1255737-27-1255737-27-1255737-27-1255 IN-03737-27-1255 IN-04

ADADADSBSBSBSBSBSB

000100010203040000

This Document SUPERSEDES 737-27-1255/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150404 ITEM: 1

737-27-1255 SB 01 MANDATORY A/C *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. Superseded (Superseded)2002-20-07 (SUPERSEDED)2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1255 IN 03 (REF)737-27-1255 IN 04 (REF)737-27-1255-R0 (REF)737-27-1255-R1 (REF)737-27-1255-R2 (REF)737-27-1255-R3 (REF)

ADADADSBSBSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1255P2 SB 03 MANDATORY A/C *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW. Closed 21.Feb.2008

Applicable to all 737-100 to 500 LN 0001-3132 with SB 27-1255 Rev 1or 2 installed, that have not performed Rev 3.2002-20-07 (SUPERSEDED)2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1255 IN 03 (REF)737-27-1255 IN 04 (REF)737-27-1255-R0 (REF)737-27-1255-R1 (REF)737-27-1255-R2 (REF)737-27-1255-R3 (ACTIVE)SBB 737-27-1255P2 (MOD TASK)

ADADADSBSBSBSBSBSBTA




737-27-1261 SB 00 MANDATORY A/C FLIGHT CONTROLS - HYDRAULICAL MODULAR PACKAGE - AUTHORITY FOR PARTINSTALLATION

Information Only

This SB only gives intstructions on which PN/SN are allowd to beinstalled on AC.For PN: 65-44891-7 only SN: 8937 and higher can be installed.737-27A1260 SB 00Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1264 SB 02 MANDATORY A/C *AD* RUDDER & RUD. TRIM CTRL SYST. REPLACEMENT OF P5-3 PANEL Closed 17.Mar.2005

2002-20-07 (SUPERSEDED)2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1264-R0 (REF)737-27-1264-R1 (REF)737-27-1264-R2 (ACTIVE)PRODUCTION LINE PRR35436-RSBB 737-27-1264 (MOD-TASK)

ADADADSBSBSBPRRTA




737-27-1265 SB 01 RECOMMENDED A/C T/E FLAP TRANSMISSION - UNIVERSAL JOINT BOLT ASSY REPL. Rejected by OperatorThis SB has been rejected by NAS, no safety or economic benefit.737-27-1265 IN 01 (REF)737-27-1265 IN 02 (REF)737-27-1265-R0 (REF)737-27-1265-R1 (ACTIVE)737-SL-27-194 (RELATED)737-SRP-27-0155 (REF)PRODUCTION LINEPRR35005-251RSSBB 737-27-1265 (MOD TASK)

SBSBSBSBSLSRPPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1265 SB 00 RECOMMENDED A/C T/E FLAP TRANSMISSION - UNIVERSAL JOINT BOLT ASSY REPL. Superseded (Superseded)

This SB has been rejected by NAS, no safety or economic benefit.737-27-1265 IN 01 (REF)737-27-1265 IN 02 (REF)737-27-1265-R0 (REF)737-27-1265-R1 (ACTIVE)737-SL-27-194 (RELATED)737-SRP-27-0155 (REF)PRODUCTION LINEPRR35005-251RSSBB 737-27-1265 (MOD TASK)

SBSBSBSBSLSRPPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1267 SB 01 RECOMMENDED A/C OUTB. T/E FLAP DRIVE TORQUE TUBE COUPLING INSPECTION/REPLACEMENT Repetitive

737-27-1267737-27-1267-01737-27-1267-02PRODUCTION PRR35005-251RS

SBEOEOPRR

000000

Thereafter perform in an interval of 12000/C737-27-1267/SB Rev.01 OUTB. T/E FLAP DRIVE TORQUE TUBE COUPLING INSPECTION/REPLACEMENT Repetitive> 737-27-1267-01/EO* Rev.00 OUTB. T/E FLAP DRIVE TORQUE TUBE COUPLING INSPECTION L/H Repetitive

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

49798/CPerform initially before(F) 0/C /Interval(F):12000/C

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks27.Jun.2011 64534:00/H 37798/C 205168, N/A Was due at: 39176/C PerfRev.:'00'

> 737-27-1267-02/EO* Rev.00 OUTB. T/E FLAP DRIVE TORQUE TUBE COUPLING INSPECTION R/H RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



737-27-1269 SB 00 RECOMMENDED A/C RUDDER FEEL & CENERING UNIT, FLANGE CLEARANCE INSP & REWORK Closed 10.Mar.2005737-27-1269-R0 (ACTIVE)PRODUCTION MRR3273-1556SBB 737-27-1269 (MOD-TASK)

SBPRRTA








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1272 SB 00 MANDATORY A/C *AD * AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION Repetitive

2006-21-01 (ACTIVE)37-SBB-27-1272P1 (REPETITIVE)37-SBB-27-1272P2 (REPETITIVE)737-27-1272-R0 (ACTIVE)737-SRP-27-0166 (REF)

ADTATASBSRP

Perform within an unlimited threshold.737-27-1272/SB Rev.00 *AD * AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION Repetitive> 737-27-1272P1/EO* Rev.00 *AD* AILERON BALANCE TAB FREEPLAY CHECK Repetitive


07.Feb.2016 79572:00/HPerform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D or0/H / Interval(F):730/D or 8000/H


07.Feb.2014 71572:00/H 43151/C 489495, N/AWas due at: 30.Oct.2014 and 4568340/HPerfRev.:'00'

> 737-27-1272P2/EO* Rev.00 *AD* AILERON BALANCE TAB BEARING LUBRICATION *** MANDATORY REPETITIVELUBRICATION ***

Repetitive


24.Feb.2015 75572:00/H

Perform initially before(F) 0/H Performinitially within (effective from ManufacturerDate 13.Mar.1990) (F) 0/D /Interval(F):4000/H or 365/D


24.Feb.2014 71572:00/H 43151/C 489223, N/AWas due at: 12.Apr.2014 and 4388100/HPerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27-1294 SB 00 RECOMMENDED A/C FLIGHT CONTROLS - TRAILING EDGE FLAP SYSTEM - MACH TRIM FLAP, FLAPS UP

AND FLAP LANDING WARNING LIMIT SWITCH REPLACEMENTSuperseded (Superseded)

This SB is part of a validation program between Boeing and NSB. TheSB will be trial performed on LN-KKE, LN 2608. All other AC arerejected for this modification. NSB does not currently have areliability issue with the affected switches.737-27-1294 IN-01 SB 00This Document has been SUPERSEDED BY 737-27-1294/SB Rev.01Reason for this StatusNON MANDATORY SB REJECTED DUE TO NO RELIABILITY ISSUES

737-27-1294 SB 01 RECOMMENDED A/C FLIGHT CONTROLS - TRAILING EDGE FLAP SYSTEM - MACH TRIM FLAP, FLAPS UPAND FLAP LANDING WARNING LIMIT SWITCH REPLACEMENT


This SB is part of a validation program between Boeing and NSB. TheSB will be trial performed on LN-KKE, LN 2608. All other AC arerejected for this modification. NSB does not currently have areliability issue with the affected switches.737-27-1294 IN-01 SB 00This Document SUPERSEDES 737-27-1294/SB Rev.00Reason for this StatusAUTO ASSIGNED

737-27A1126 SB 01 MANDATORY A/C *AD* TO PREVENT HAZARDS ASSOCIATED WITH MALFUNC. AOA SENSOR Not ApplicableThis SB is Not Applicable to NAS. This SB concerns 737-100/200.1985-19-01 (ACTIVE)737-27A1126-R1 (ACTIVE)SBB 737-27A1126 (MOD-TASK)

ADSBTA





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1164 SB 01 MANDATORY A/C FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Superseded (Superseded)

1993-01-27 (ACTIVE)737-27A1164-R1 (REF)737-27A1164-R2 (ACTIVE)737-27A1164-RO (REF)PTODUCTION LINE PRR33890-67SBB 737-27A1164 (MOD-TASK)

ADSBSBSBPRRTA

This Document SUPERSEDES 737-27A1164/SB Rev.00This Document has been SUPERSEDED BY 737-27A1164/SB Rev.02

737-27A1164 SB 00 MANDATORY A/C FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Superseded (Superseded)1993-01-27 (ACTIVE)737-27A1164-R1 (REF)737-27A1164-R2 (ACTIVE)737-27A1164-RO (REF)PTODUCTION LINE PRR33890-67SBB 737-27A1164 (MOD-TASK)

ADSBSBSBPRRTA


737-27A1164 SB 02 MANDATORY A/C FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Closed 08.Dec.19951993-01-27 (ACTIVE)737-27A1164-R1 (REF)737-27A1164-R2 (ACTIVE)737-27A1164-RO (REF)PTODUCTION LINE PRR33890-67SBB 737-27A1164 (MOD-TASK)

ADSBSBSBPRRTA

This Document SUPERSEDES 737-27A1164/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.1995LHT EO006425





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1191 SB 00 MANDATORY A/C *AD* HORIZONTAL STAB. - REPL. OF THE STAB. TRIM ELEC. ACT. Superseded (Superseded)

1995-10-05 (ACTIVE)737-27A1191-R0 (REF)737-27A1191-R1 (ACTIVE)PRODUCTION LINE PRR35005-103SBB 737-27A1191 (MOD-TASK)

ADSBSBPRRTA


737-27A1191 SB 01 MANDATORY A/C *AD* HORIZONTAL STABILIZER - REPL. OF THE HORIZONTAL STABILIZER ELECTRICTRIM ACTUATOR

Performed by prev. Operator


25.Nov.1994DELIVERYDOC

PerfRev.:'01'

737-27A1194 SB 02 MANDATORY A/C *AD* FLIGHT CONTROLS - INSP/MOD OF THE FEEL & CENTERING UNIT Closed 19.Nov.19961996-25-17 (ACTIVE)737-27A1194-R0 (REF)737-27A1194-R1 (REF)737-27A1194-R2 (ACTIVE)PRODUCTION LINE PRR35335SBB 737-27A1194 (MOD-TASK)

ADSBSBSBPRRTA


19.Nov.1996PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1198 SB 00 MANDATORY A/C *AD* AILERON/RUDDER TRIM CONTROL MODULE REPLACEMENT Closed 13.Jun.1997

This document is applicable to LN# 1001-2311,2316,2349. All other LN#are Not Applicable per Boeing SB.1997-06-09 (ACTIVE)737-27A1198-R0 (ACTIVE)

ADSB


13.Jun.1997PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.


737-27A1199 SB 00 MANDATORY A/C *AD* FLAPS - MOD. OF FLAP CTRL. CABLE FAILURE DETECTION SYS. Closed 08.Apr.1997This Document is applicable to LN# 1001-2765.1997-02-16 (ACTIVE)737-27A1199-RO (ACTIVE)737-SRP-27-0070 (REF)PRODUCTION LINE PRR35005-155SBB 737-27A1199 (MOD TASK)

ADSBSRPPRRTA


08.Apr.1997PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1202 SB 02 MANDATORY A/C *AD* RUDDER PCU DUAL SERVO VALVE AND DUAL LOADPATH BOLT REPL Closed 21.Feb.1998

This modification is applicable to LN# 1-2914. The following LN# areNot Applicable per PRR35365 and PRR38060-6.

This modification is mandated by AD 1997-14-04 §c.1994-01-07 (SUPERSEDED)1996-23-51 (SUPERSEDED)1997-14-04 (ACTIVE)737-27A1202-R0 (REF)737-27A1202-R1 (REF)737-27A1202-R2 (REF)737-27A1202-R3 (ACTIVE)PRODUCTION LINE PRR 35365PRODUCTION LINE PRR38060-6SBB 737-27A1202 (MAINT TASK)

ADADADSBSBSBSBPRRPRRTA


21.Feb.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1205 SB 00 MANDATORY A/C ELEVATOR TAB ROD ATTACHMENT NUT INSPECTION Closed 09.Feb.1999

This mod is applicable to LN# 1-2939. The following LN# are NotApplicable due to MRR 3277-1146.1999-05-15 (SUPERSEDED)2000-19-05 (ACTIVE)2000-19-05 XA (REF)737-27A1205-R0 (ACTIVE)737-SL-27-118/A/B/C/D (REF)PRODUCTION LINE MRR3277-1146

ADADADSBSLPRR




737-27A1206 SB 03 MANDATORY A/C *AD* RUDDER PRESSURE REDUCER AND YAW DAMPER COUPLER INST. Closed 26.Jul.2000This Document is effective for LN# 1-3075.1997-14-03 (SUPERSEDED)1998-02-01 (SUPERSEDED)2007-03-07 (ACTIVE)737-27A1206-R0 (REF)737-27A1206-R1 (REF)737-27A1206-R2 (REF)737-27A1206-R3 (ACTIVE)PRODUCTION LINE PRR35360

ADADADSBSBSBSBPRR


26.Jul.2000PerfRev.:'NOTE' / Reason: DELIVERYDOCS.

Reason for this StatusDELIVERY DOCS.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1207 SB 03 RECOMMENDED A/C REPLACEMENT OF DUAL-LOADPATH BOLTS FOR THE ELEVATOR FEEL UN Rejected by Operator

737-27A1207-R3 (ACTIVE)PRODUCTION LINE PRR38060-12

SBPRR


737-27A1207 SB 01 RECOMMENDED A/C REPLACEMENT OF DUAL-LOADPATH BOLTS FOR THE ELEVATOR FEEL UN Superseded (Superseded)737-27A1207-R3 (ACTIVE)PRODUCTION LINE PRR38060-12

SBPRR



SBPRR



SBPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1211 SB 01 MANDATORY A/C *AD* REPLACEMENT OF ROD ENDS FOR LEADING EDGE SLAT ACTUATORS Superseded (Superseded)

2000-02-03 (SUPERSEDED)2003-03-05 (ACTIVE)737-27A1211 IN 04 (REF)737-27A1211-R0 (REF)737-27A1211-R1 (REF)737-27A1211-R2 (REF)737-27A1211-R3 (ACTIVE)737-SL-27-095 (REF)FAA LETTER 130S-00-0313PRODUCTION LINE PRR 35005-175SBB 737-27A1211 (MOD TASK)

ADADSBSBSBSBSBSLAMOCPRRTA

This Document SUPERSEDES 737-27-1211/SB Rev.00This Document has been SUPERSEDED BY 737-27A1211/SB Rev.02





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1211 SB 03 MANDATORY A/C FLIGHT CONTROLS - LIFT AUGMENTATION - LEADING EDGE FLAPS AND SLATS

REPLACEMENT OF THE ROD ENDS FOR THE LEADING EDGE SLAT ACTUATORSSee prev. Docstatus / Special Text:This aircraft is Not Applicable dueto PRODUCTION LINE PRR35005-175



This Document SUPERSEDES 737-27A1211/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks18.Dec.2001 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1211 SB 02 MANDATORY A/C *AD* REPLACEMENT OF ROD ENDS FOR LEADING EDGE SLAT ACTUATORS Superseded (Closed 18.Dec.2001)










24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1212 SB 01 MANDATORY A/C *AD* RUDDER PEDAL PUSHROD FASTENES, INSP FOR CORRECT INSTALL Closed 14.Jul.1998

1998-13-12 (SUPERSEDED)1998-13-12-R1 (ACTIVE)737-27A1212-R0 (REF)737-27A1212-R1 (ACTIVE)737-SL-27-121 (REF)737-SRP-27-0103 (REF)SBB 737-27A1212 (MOD TASK)

ADADSBSBSLSRPTA




737-27A1213 SB 01 MANDATORY A/C *AD* INSPECTION OF THE SPOILER MIXER FOR CORRECT INSTALL. Closed 10.Oct.1998This modification is applicable to LN 1-2681.1999-25-02 (ACTIVE)737-27A1213-R0 (REF)737-27A1213-R1 (ACTIVE)737-SRP-27-0104 (REF)

ADSBSBSRP


10.Oct.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1214 SB 01 MANDATORY A/C *AD* RUDDER & TAB-RUDDER PEDAL PUSHROD FASTENER REPLACEMENT Closed 23.Oct.2002

This mod is applicable for LN# 1-3101. The following LN# are NotApplicable per PRR35404.2001-22-13 (ACTIVE)737-27A1214-R0 (REF)737-27A1214-R1 (ACTIVE)PRODUCTION LINE PRR35404

ADSBSBPRR


23.Oct.2002PerfRev.:'NOTE' / Reason: DELIVERYDOC

Reason for this StatusDELIVERY DOC

737-27A1221 SB 01 MANDATORY A/C *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Closed 17.Mar.20051999-11-05 (ACTIVE)37-SBB-27A1221 (REPETITIVE)737-27A1221-R0 (REF)737-27A1221-R1 (ACTIVE)737-SL-27-129 (REF)PRODUCTION LINEPRR35005-224-R

ADTASBSBSLPRR

Perform within an unlimited threshold.737-27A1221/SB Rev.01 *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Closed 17.Mar.2005> 737-27A1221/EO* Rev.00 *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Not Applicable by Serial Number> 737-27A1221-01/EO* Rev.00 *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Closed 17.Mar.2005

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 PerfRev.:'NOTE' / Reason: KKM 150404Reason for this StatusKKM 150404





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1227 SB 02 MANDATORY A/C *AD* FLIGHT CONTROLS - FLAP LIMIT SWITCH INSP. & RELAY INST Superseded (Not Applicable by

Serial Number)Compliance:This SB ensures compliance with AD 1999-10-13 § (a).

This document is applicable to LN# 2997-3027.1999-10-13 (ACTIVE)737-27A1227-R3 (ACTIVE)737-SRP-27-0114 (REF)PRODUCTION LINE PRR38060-31

ADSBSRPPRR


737-27A1227 SB 03 MANDATORY A/C *AD* FLIGHT CONTROLS - FLAP LIMIT SWITCH INSP. & RELAY INST Not Applicable by Serial NumberCompliance:This SB ensures compliance with AD 1999-10-13 § (a).

This document is applicable to LN# 2997-3027.1999-10-13 (ACTIVE)737-27A1227-R3 (ACTIVE)737-SRP-27-0114 (REF)PRODUCTION LINE PRR38060-31

ADSBSRPPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1238 SB 00 MANDATORY A/C *AD* LATERAL TRANSFER MECH, LOWER BEARING SUPPORT INSP/MOD Closed 30.Mar.2001

2002-18-02 (ACTIVE)737-27A1238-R0 (ACTIVE)PRODUCTION LINE MRR3270-1357

AD

SB

PRR




737-27A1243 SB 03 MANDATORY A/C *AD* LEADING EDGE SLATS-INSPECT. FOR VIBRO-ENGRAVED ROD ENDS Closed 06.Dec.20012003-03-05 (ACTIVE)737-27A1243-R0 (ACTIVE)SBB 737-27A1243 (MOD-TASK)

ADSBTA








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1266 SB 01 MANDATORY A/C *AD* INSP. OF ELEVATOR CONTROL TAB RODS AND CTR ROD JAM NUTS Repetitive

2007-16-05 (ACTIVE)37-SBB-27A1266 (REPETITIVE)737-27A1266 IN 01 (ACTIVE)737-27A1266-R0 (REF)737-27A1266-R1 (ACTIVE)

ADTASBSBSB

Thereafter perform in an interval of 4500/CThereafter perform in an interval of 6000/H

737-27A1266/SB Rev.01 *AD* INSP. OF ELEVATOR CONTROL TAB RODS AND CTR ROD JAM NUTS Repetitive> 737-27A1266/EO* Rev.00 *AD* INSP. OF ELEVATOR CTR. TAB RODS AND CTR. ROD JAM NUTS *** REPETITIVE

INSPECTIONS***Repetitive


77572:00/H 47651/CPerform initially before(F) 0/H or 0/C /Interval(F):6000/H or 4500/C


04.Feb.2014 71572:00/H 43151/C 502761, N/AWas due at: 45070/C and 4448340/HPerfRev.:'00'

737-27A1274 SB 00 MANDATORY A/C FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR INPUT TORQUE TUBEMODIFICATION

Superseded (Closed 18.Feb.2008)

AMOC issued for extension, not required for NAS. All AC modified ontime.130S-11-15A737-SRP-27-0163

AMOCSRP

0000


18.Feb.2008 54542:00/H 30315/CKKM 151344ITEM: 1

PerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1274 SB 01 MANDATORY A/C FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR INPUT TORQUE TUBE

MODIFICATIONSee prev. Docstatus

AMOC issued for extension, not required for NAS. All AC modified ontime.

This document is applicable to LN# 1-3132.130S-11-15A737-SRP-27-0163

AMOCSRP

0000

This Document SUPERSEDES 737-27A1274/SB Rev.00Reason for this StatusAIRCRAFT MODIFIED VIA SB 737-27A1274 REV.:00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1278 SB 01 RECOMMENDED A/C FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -

BALLSCREW AND BALL NUT INSPECTION AND LUBRICATIONOpen

FLIGHT CONTROLS - Horizontal Stabilizer Trim Control System -Ballscrew and Ball Nut Inspection , Lubrication, and Repair/Overhaul

SB/EO is applicable to:LN# 1-3132All NAS AC are Group 1 AC

SB is divided into 5 Work packages (WP):WP 1 is applicable to group 1 ACWP 2 is NOT applicable to group 1 AC.WP 3 is NOT applicable to group 1 AC.WP 4 is applicable to group 1 ACWP 5 is applicable to group 1 AC

Compliance:

This SB is divided into 4 EO and they are:

EO 737-27A1278-01 covers detailed inspection.EO 737-27A1278-02 covers lubricationEO 737-27A1278-03 covers restoration/OHEO 737-27A1278-04 covers impementation of MFG SB on Group 1 AC.37-NAS-2741-001 (REPETITIVE)37-NAS-2741-002 (REPETITIVE)737-27A1278-R0 (SUPERSEEDED)737-27A1278-R1 (ACTIVE)PRODUCTION LINE PRR35005-261R

TA

TA

SB

SB

PRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusPerform within an unlimited threshold.

737-27A1278/SB Rev.01 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -BALLSCREW AND BALL NUT INSPECTION AND LUBRICATION

Open

This Document SUPERSEDES 737-27A1278/SB Rev.00> 737-27A1278-01/EO* Rev.00 DETAILED INSP. OF BALLSCREW;HORIZONTAL STABILIZER TRIM CONTROL SYSTEM Repetitive


04.Aug.2015 75572:00/HPerform initially before(F) 4000/H /Interval(F):4000/H or 547/D


03.Feb.2014 71572:00/H 43151/C 436901, N/AWas due at: 07.May.2014 and 4328340/HPerfRev.:'00'

> 737-27A1278-02/EO* Rev.00 LUBRICATION OF BALLSCREW;HORIZONTAL STABILIZER TRIM CONTROL SYSTEM RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

05.Oct.2015 75319:36/HPerform initially before(F) 2000/H /Interval(F):360/D or 2000/H


10.Oct.2014 73319:36/H 44494/C 544213,Was due at: 07.Feb.2015 and 4414320/HPerfRev.:'00'

> 737-27A1278-03/EO* Rev.00 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -BALLSCREW AND NUT INSPECTION, LUBRICATION, AND REPAIR/OVERHAUL

Part-Requirem.Contr.

> 737-27A1278-04/EO* Rev.00 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -BALLSCREW AND NUT INSPECTION, LUBRICATION, AND REPAIR/OVERHAUL

Open (Next Shop Visit)

Affected Rotables (Part No/Serial No/Position) Status65-49970-25 / KE01031 Pos=AFT (KKM) Open / NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1278 SB 00 RECOMMENDED A/C STABLIZER BALLSCREW AND BALL NUT INSPECTION AND LUBRICATION Superseded (Superseded)

37-NAS-2741-001 (REPETITIVE)37-NAS-2741-002 (REPETITIVE)737-27A1278-R0 (SUPERSEEDED)737-27A1278-R1 (ACTIVE)PRODUCTION LINE PRR35005-261R

TA

TA

SB

SB

PRR


25.May.2009 58477:00/H 33256/CPerfRev.:'NOTE' / Reason: TASK37-NAS-2741-001/002

Reason for this StatusTASK 37-NAS-2741-001/002

737-27A1281 SB 00 MANDATORY A/C *AD* STBY RUD SHUTOFF VALVE TEST & FORCE FIGHT MONITOR TEST Cancelled2007-03-07 (ACTIVE)37-SBB-27A1281-1 (REPETITIVE)37-SBB-27A1281-2 (REPETITIVE)737-27A1281 IN 01 (REF)737-27A1281-R0 (ACTIVE)PRODUCTION LINEPRR35005-272RS

ADTATASBSBPRR

Perform within an unlimited threshold.737-27A1281/SB Rev.00 *AD* STBY RUD SHUTOFF VALVE TEST & FORCE FIGHT MONITOR TEST Cancelled> 737-27A1281-1/EO* Rev.00 *AD* *AD* STANDBY RUDDER ACTUATOR SHUTOFF VALVE TEST Cancelled

Reason for this StatusCANCELLED BY SB 737-27-1255 REV 3 PART 2

> 737-27A1281-2/EO* Rev.00 *AD* *AD* RUDDER MAIN PCU FORCE FIGHT MONITOR TEST CancelledReason for this StatusCACELLED BY SB 737-27-1255 REV3 PART 2





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-27A1286 SB 00 RECOMMENDED A/C FLIGHT CONTROLS - RSEP FAIRING ASSEMBLY INSPEC & REPLACEMENT Closed 28.Jun.2011 W/O:205194

This SB inspects whether the correct RSEP rudder fairings arecorrect.Applicability LN: 1018-3132. All NAS AC are Group 2 AC.737-27-1252 (REF)737-27-1255 (REF)737-27A1286-R0 (ACTIVE)737-SRP-27-0198 (REF)SBB 737-27A1286 (MOD TASK)

SBSBSBSRPTA

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Jun.2011 64534:00/H 37798/C 205194, N/A Was due at: 09.May.2012 PerfRev.:'00'

737-28-1059 SB 02 OPTIONAL COMP ENGINE FUEL FEED SYSTEM - FUEL BOOST PUMP REPLACEMENT OF Not Applicable by Line Number /Special Text: Not appicable due toMSN/ Line no.

No economic or safety benefit. NAS will not implement this SB.fuel pumps will be replaced with an improved pump on attrition basis.

References:/A/: PRR33890-64Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

737-28-1067 SB 02 RECOMMENDED A/C FUEL COMPENSATOR REPLACEMENT Rejected by Operator737-28-1067-R2 (ACTIVE)PRODUCTION PRR34935PRR35330-R

SB

PRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1084 SB 03 MANDATORY A/C *AD* FUEL FEED TUBE ASSEMBLY MOD. Not Applicable by Serial Number

The SB is applicable for LN: 1001-17171990-15-03 (ACTIVE)737-28-1055-R0 (REF)737-28-1055-R1 (REF)737-28-1084-R0 (REF)737-28-1084-R1 (REF)737-28-1084-R2 (REF)737-28-1084-R3 (ACTIVE)

ADSBSBSBSBSBSB

737-28-1086 SB 00 RECOMMENDED A/C FUEL INDICATING SYSTEM ELECTRICAL WIRE BUNDLE RELOCATION Not Applicable by Serial Number737-28-1086-R0 (ACTIVE) SB

737-28-1087 SB 02 RECOMMENDED A/C INSTALLATION OF FOUR CIRCUIT BREAKES FUEL QUANTITY IND SYS Rejected by Operator737-28-1087-R2 (ACTIVE)PRODUCTION LINE PRR34845

SBPRR

737-28-1088 SB 00 MANDATORY A/C *AD* FUEL - AUX. FUEL TANK & SUPPORT STRUCTURE, INSP. OF Not Applicable1991-16-08 (ACTIVE)737-28-1088-R0 (ACTIVE)737-28A1034-R2 (REF)SBB 737-28-1088 (INSP-TASK)

ADSBSBTA

Reason for this StatusNOT EQUIPPED WITH A BOEING AFT CARGO BAY AUXILIARY

737-28-1100 SB 00 RECOMMENDED A/C DELETION OF FUEL FEED CHECK VALVES Rejected by Operator737-28-1100-R0 (ACTIVE)PRODUCTION LINE PRR35205

SBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1115 SB 01 MANDATORY A/C *AD* REFUEL VALVE ACTUATOR SUPPRESSION DIODES REPLACEMENT. Closed 19.Nov.2000

1999-23-20 (ACTIVE)737-28-1115 IN 01 (REF)737-28-1115-R0 (REF)737-28-1115-R1 (ACTIVE)PEODUCTION LINE PRR38060-19SBB 737-28-1115 (MAINT TASK)

ADSBSBSBPRRTA


19.Nov.2000PerfRev.:'NOTE' / Reason: DELIVERYDOC.


737-28-1117 SB 01 RECOMMENDED A/C FUEL - STORAGE CENTER WING FUEL TANK INSPECTION Closed 11.Feb.1999737-28-1117-R1 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1131 SB 03 MANDATORY A/C *AD* REPL OF THE FUEL VENT DOOR TO ADD A FLAME ARRESTOR Closed 28.Mar.2001

AMOC approves the use of P/N BAC27XSTN3806 stencil to be used as analternate to the P/N BAC27NFS0106 placard.1999-03-04 (ACTIVE)737-28-1026 (REF)737-28-1131-R3 (ACTIVE)PRODUCTION LINE PRR 35389-1R

ADSBSBPRR


28.Mar.2001PerfRev.:'NOTE' / Reason: DELIVERYDOCS.


737-28-1156 SB 01 MANDATORY A/C *AD* SMITHS TRANSIENT SUPPRESSION UNIT (TSU) INSTALLATION Not Applicable130S-01-495 (ACTIVE)1999-03-04 ITEM (A) (ACTIVE)737-28-1156-R1 (ACTIVE)PRODUCTION PRR35422-RST00847SE (REF)

AMOCADSBPRRSTC

Reason for this StatusSBB 737-28-1157





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1157 SB 00 MANDATORY A/C *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled

130S-00-0632 (ACTIVE)1999-03-04 ITEM (A) (ACTIVE)2009-20-11 (REF)737-28-1157-R0 (ACTIVE)PRODUCTION PRR35423-RST00127BO (REF)

AMOCADADSBPRRSTC

Perform BEFORE 09.Mar.2003737-28-1157/SB Rev.00 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled> 737-28-1157-01/EO* Rev.01 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Closed 14.Mar.2003


14.Mar.2003 42144:00/H 19904/CMALEVEO:737-28-0043/SB28-1157

> 737-28-1157MPD/EO* Rev.00 737-28-1157MPD CONTROLLED BY MPD TASKS Taskcard ControlledCarried out on the following TaskcardsTaskcard: NAS-2841-006 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks05.04.2019 88'534/H 15212:25/H Interval:24000/HPerf Dim1 (D) Perf Dim2 Perf Dim306.07.2011 64534:00/H 37798/CCarried out on the following TaskcardsTaskcard: NAS-2841-007 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks11.02.2017 81'168/H 7846:25/H Interval:39000/HCarried out on the following TaskcardsTaskcard: NAS-2841-005 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks04.02.2015 04.Feb.2015103d, 13h Interval:365/DPerf Dim1 (D) Perf Dim2 Perf Dim304.02.2014 71572:00/H 43151/C





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusAUTO ASSIGNED

737-28-1164 SB 01 MANDATORY A/C *AD* TEST OF ELECTR. CIRCUITS THAT CLOSE FUEL SHUTOFF VALVE Closed 27.Mar.20012001-13-07 (ACTIVE)737-28-1164-R1 (ACTIVE)737-28-1164-RO (REF)737-SRP-28-0058 (REF)SBB 737-28-1164 (MOD TASK)

ADSBSBSRPTA




737-28-1186 SB 02 MANDATORY A/C *AD* INST OF GOODRICH CORPORATION ISOLATED FUEL QUANTITY TX Not Applicable1999-03-04 ITEM (A)737-28-1186-R2 (ACTIVE)MARATHON SB 041-825PRODUCTION PRR35005-241RSS345U000 (BF DOODRICH)T3031-0012-0101 (BF GOODRICH)

ADSBSBPRRDWGDWG

Reason for this StatusSBB 737-28-1157/STC ST00127BO





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1193 SB 01 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - INSPECTION FOR WIRE CHAFING Closed 17.Mar.2005

2005-23-17 (ACTIVE)737-28-1193 IN 01 (REF)737-28-1193 IN 02 (REF)737-28-1193-R0 (REF)737-28-1193-R1 (ACTIVE)NPRM 2004-NM-06-AD (REF)SBB 737-28-1193 (MOD TASK)

ADSBSBSBSBADTA




737-28-1193-1 SB 01 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - INSPECTION FOR WIRE CHAFING Not Applicable by Serial Number2005-23-17 (ACTIVE)37-28-003 (ACTIVE)737-28-1193 IN 01 (REF)737-28-1193 IN 02 (REF)737-28-1193-R0 (REF)737-28-1193-R1 (ACTIVE)SBB 737-28-1193 (MOD TASK)

ADEODSBSBSBSBTA





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1196 SB 03 MANDATORY A/C *AD* ENG FUEL SHUTOFF VALVE, WIRING CHANGES IN MWW Closed 24.Jan.2004

2001-14-06 (SUPERSEDED)2005-10-11 (ACTIVE)737-28-1196 (REF)737-28-1196 R1 (REF)737-28-1196 R2 (REF)737-28-1196 R3 (ACTIVE)737-SL-24-138 (REF)PRODUCTION MRR3282-1516SBB 737-28-1196 (MOD-TASK)

ADADSBSBSBSBSLPRRTA


24.Jan.2004 43499:00/H 21327/CPerfRev.:'NOTE' / Reason: KKM 150052ITEM: 2


737-28-1208 SB 02 MANDATORY A/C FUEL - INDICATING - WING CENTER TANK WIRE BUNDLES INSPECTION AND CLAMPSCHANGE

See prev. Docstatus

All NAS aircraft modified via SB rev.: 00 + TO 37-28-001 or SBrev.:01 as required by AD.SB rev.:02 not to be performed by NAS.37-28-001 (REF)NPRM 2004-NM-166-AD

TOAD

0000

This Document SUPERSEDES 737-28-1208/SB Rev.01Reason for this StatusALL NAS AIRCRAFT MODIFIED VIA SB REV.:00+TO 37-28-001 OR SB REV.:01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1208 SB 01 MANDATORY A/C *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Superseded (Taskcard Controlled)

2006-03-12 (ACTIVE)37-28-001 (REF)737-28-1208-R0 (REF)737-28-1208-R1 (ACTIVE)NPRM 2004-NM-166-AD

ADEODSBSBAD

This Document SUPERSEDES 737-28-1208/SB Rev.00This Document has been SUPERSEDED BY 737-28-1208/SB Rev.02Perform BEFORE 15.Mar.2011

737-28-1208/SB Rev.01 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Taskcard ControlledThis Document SUPERSEDES 737-28-1208/SB Rev.00This Document has been SUPERSEDED BY 737-28-1208/SB Rev.02

> 737-28-1208-01/EO* Rev.01 WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE See prev. DocstatusThis Document SUPERSEDES 737-28-1208-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150408 ITEM: 1

> 737-28-1208MPD/EO* Rev.01 737-28-1208MPD CONTROLLED BY MPD TASKS Taskcard ControlledCarried out on the following TaskcardsTaskcard: 28-011-00-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks12.03.2015 12.Mar.2015139d, 13h Interval:10/YRPerf Dim1 (D) Perf Dim2 Perf Dim314.03.2005 00:00/H 23575/CReason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1208 SB 00 MANDATORY A/C *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Superseded (Taskcard Controlled)

2006-03-12 (ACTIVE)37-28-001 (REF)37-B28-11-00-6A (REPETITIVE)737-28-1208 IN 01 (REF)737-28-1208-R0 (REF)737-28-1208-R1 (ACTIVE)NPRM 2004-NM-166-ADSBB 737-28-1208 (MOD-TASK)

ADEODTASBSBSBADTA

This Document has been SUPERSEDED BY 737-28-1208/SB Rev.01Perform BEFORE 15.Mar.2011

737-28-1208/SB Rev.00 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Taskcard ControlledThis Document has been SUPERSEDED BY 737-28-1208/SB Rev.01

> 37-28-001/TO* Rev.00 WINGS CENTER TANK WIRE BUNDLES INSPECTION & CLAMP CANGE Closed 21.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-28-1208-01/EO* Rev.00 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Closed 14.Mar.2005This Document has been SUPERSEDED BY 737-28-1208-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-28-1208MPD/EO* Rev.01 737-28-1208MPD CONTROLLED BY MPD TASKS Taskcard ControlledCarried out on the following TaskcardsTaskcard: 28-011-00-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks12.03.2015 12.Mar.2015139d, 13h Interval:10/YR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusPerf Dim1 (D) Perf Dim2 Perf Dim314.03.2005 00:00/H 23575/CReason for this StatusAUTO ASSIGNED

737-28-1208R1 SB 01 MANDATORY A/C *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Not Applicable by Serial NumberThis modification was performed on MSN 25040 only.2006-03-12 (ACTIVE)37-28-001 (ACTIVE)37-28-011-00-01 (REPETITIVE)737-28-1208 IN 01 (REF)737-28-1208-R0 (REF)737-28-1208-R1 (ACTIVE)SBB 737-28-1208 (MOD-TASK)

ADEODTASBSBSBTA

737-28-1241 SB 02 MANDATORY A/C FUEL - ENGINE FUEL SHUTOFF VALVE - WIRE BUNDLE REPLACEMENT W802 ANDW804 AND INSPECTION OF GROMMETS AND FAIRLEADS


NAS rejects this SB revision. NAS is in comopliance with AD throughSB 737-28-1241 Rev.:01.Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1241P1 SB 01 MANDATORY A/C *AD* ENGINE FUEL SHUTOFF VALVE - WIRE BUNDLE REPLACEMENT Closed 21.Feb.2008

For airplanes in groups 3 through 8 and 10 that have accomplished theoriginal issue of this service bulletin more work is necessary.Replace two electrical connectors as given in section 3.B. WORKINSTRUCTIONS, PART 3.

For airplanes in groups 3 through 8 and 10, that have notaccomplished the original issue of this service bulletin, and havereceived Top Kits, more work is necessary. Replace two electricalconnectors in the Top Kits and reidentify the Top Kits, as given insection 3.B. WORK INSTRUCTIONS and 2.C.1, Parts Necessary For EachAirplane, Parts.2009-14-04 (ACTIVE)737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)

ADSBSBSRP

This Document SUPERSEDES 737-28-1241P1/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1241P1 SB 00 MANDATORY A/C *AD* ENGINE FUEL SHUTOFF VALVE - WIRE BUNDLE REPLACEMENT Superseded (Superseded)

2009-14-04 (ACTIVE)737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)AD 2009-14-04-2 (AD TASK)SBB 737-28-1241P1 (MOD TASK)

ADSBSBSRPTATA

This Document has been SUPERSEDED BY 737-28-1241P1/SB Rev.01

737-28-1241P2 SB 00 MANDATORY A/C *AD* ENG FUEL SHUTOFF VALVE-INSP. OF GROMMETS AND FAIRLEADS Superseded (Superseded)2009-14-04 (ACTIVE)737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)AD 2009-14-04-1 (AD TASK,REF)AD 2009-14-04-2 (AD TASK)SBB 737-28-1241P2 (MOD-TASK)

ADSBSBSRPTATATA


737-28-1241P2 SB 01 MANDATORY A/C *AD* ENG FUEL SHUTOFF VALVE-INSP. OF GROMMETS AND FAIRLEADS Closed 07.Feb.20082009-14-04 (ACTIVE)737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)

ADSBSBSRP

00000100

This Document SUPERSEDES 737-28-1241P2/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1241P3 SB 01 MANDATORY A/C ENGINE FUEL SHUTOFF VALVE - REPLACEMENT OF ELEC. CONNECTORS Not Applicable

Applicability:

737-300, 737-400 and 737-500 airplanes, line numbers 1001 through2532 with specific replacement wire bundles, divided into Groups 1through 8 and 10. Modified iaw the initial issue of the SB, using P/N65C38639-71, 65C38639-61 or 65C38639-6.737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)SBB 737-28-1241P3 (MOD-TASK)

SBSBSRPTA

This Document SUPERSEDES 737-28-1241P3/SB Rev.00Reason for this StatusNEW KIT P/N TO BE INSTALLED

737-28-1241P3 SB 00 RECOMMENDED A/C ENGINE FUEL SHUTOFF VALVE - REPLACEMENT OF ELEC. CONNECTORS Superseded (Superseded)737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)SBB 737-28-1241P3 (MOD-TASK)

SBSBSRPTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28-1286 SB 00 MANDATORY A/C FUEL - INTEGRAL FUEL TANKS - ACCESS DOOR INSPECTION/REPLACEMENT Not Applicable by Serial Number

Compliance:This SB ensures compliance with AD 2013-13-15 § (f).2013-13-152013-NM-019-AD737-28-1081737-28A1064737-28A1070737-28A1078737-SRP-57-0225AMM 28-11-11, 28-23-00IPC 28-11-11SOPM 20-50-10

ADNPRMSBSBSBSBSRPAMMIPCSOPM

00000103020200000000

737-28A1062 SB 02 MANDATORY A/C *AD* MINIMIZE FIRE HAZARD DUE TO FUEL FEED TUBE ASSY CHAFING Not Applicable by Serial Number

737-28A1072 SB 05 MANDATORY A/C *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Not Applicable by Serial NumberThis mod is applicable for LN# 1001-1523. The following LN# are Notapplicable Per PRR34394.1990-15-17 (ACTIVE)737-28A1072-R0 (REF)737-28A1072-R1 (REF)737-28A1072-R2 (REF)737-28A1072-R3 (REF)737-28A1072-R4 (REF)737-28A1072-R5 (ACTIVE)PRODUCTION PRR34394SBB 737-28A1072 (MOD-TASK)

ADSBSBSBSBSBSBPRRTA





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1077 SB 00 MANDATORY A/C *AD* ENGINE FUEL FEED SYSTEM, CLEARANCE INSPECTION Not Applicable by Serial Number

1989-10-01 (ACTIVE)737-28A1077 (ACTIVE)SBB 737-28A1077 (MOD TASK)

ADSBTA

737-28A1114 SB 03 MANDATORY A/C *AD* FUEL LOW PRESS SWITCHES REPL./INSP. OF FUEL BOOST PUMPS Closed 25.Nov.19982000-04-02 (ACTIVE)35005-218 (PRODUCTION)37-SBB-28A1114 (REP TASK)737-28A1114-R0 (REF)737-28A1114-R1 (REF)737-28A1114-R2 (REF)737-28A1114-R3 (ACTIVE)SBB 737-28A1114 (MAINT TASK)

ADPRRTASBSBSBSBTA

Perform BEFORE 29.Mar.2002737-28A1114/SB Rev.03 *AD* FUEL LOW PRESS SWITCHES REPL./INSP. OF FUEL BOOST PUMPS Closed 25.Nov.1998> 737-28A1114/EO* Rev.03 *AD* FUEL BOOST PUMPS INSPECTION Not Applicable

Reason for this StatusREPETITIVE INSPECTION TERMINATED BY MODIFICATION

> 737-28A1114-01/EO* Rev.03 *AD* FUEL LOW PRESS SWITCHES REPL./INSP. OF FUEL BOOST PUMPS Closed 25.Nov.1998Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

25.Nov.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1120 SB 04 MANDATORY A/C *AD* FUEL BOOST PUMP - INSP. OF THE WIRING IN THE FUEL TANKS Cancelled (Cancelled)

1999-21-15 (ACTIVE)37-SBB-28A1120P2 (REPETITIVE)737-28A1120-R0 (REF)737-28A1120-R1 (REF)737-28A1120-R2 (REF)737-28A1120-R3 (REF)737-28A1120-R4 (REPL BY 1263)PRODUCTION PRR35406-R

ADTASBSBSBSBSBPRR

This Document has been CANCELLED BY 737-28A1263/SB Rev.02

737-28A1132 SB 02 MANDATORY A/C *AD* FUEL/PRESSURE FUELING SYSTEM/ADD SLEEVES TO THE WIRES Cancelled (Not Applicable)1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1132-R0 (REF)737-28A1132-R1 (REF)737-28A1132-R2 (REPLACED)737-32A1141 R4 (ACTIVE)SBB 737-28A1132 (MOD-TASK)

ADADSBSBSBSBTA

This Document has been CANCELLED BY 737-28A1141/SB Rev.02Reason for this StatusSB REPLACED BY 737-28A1141





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1134 SB 01 MANDATORY A/C *AD* FUEL - ENGINE FUEL FEED SYSTEM - FUEL BOOST PUMP INSP. Not Applicable by Serial Number

The modification is for fuel pumps installed on AUX fule tanks. NASdoes not have any auxiliary fuel tanks installed.1999-24-06 (ACTIVE)737-28A1134-R0 (REF)737-28A1134-R1 (ACTIVE)737-SRP-28-0048 (REF)M-7200-98-03173 (REF)SBB 737-28A1134 (MOD TASK)

ADSBSBSRPBMTA

737-28A1141 SB 01 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH Superseded (Superseded)1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1141 IN02737-28A1141-R0 (REF)737-28A1141-R1 (REF)737-28A1141-R2 (REF)737-28A1141-R3 (REF)737-28A1141-R4 (ACTIVE)PRODUCTION PRR38060-32SBB 737-28A1141 (MOD TASK)

ADADSBSBSBSBSBSBPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1141 SB 02 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH Superseded (Superseded)

1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1141 IN02737-28A1141-R0 (REF)737-28A1141-R1 (REF)737-28A1141-R2 (REF)737-28A1141-R3 (REF)737-28A1141-R4 (ACTIVE)PRODUCTION PRR38060-32SBB 737-28A1141 (MOD TASK)


This Document CANCELS 737-28A1132/SB Rev.02This Document SUPERSEDES 737-28A1141/SB Rev.01This Document has been SUPERSEDED BY 737-28A1141/SB Rev.03





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1141 SB 04 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH See prev. Docstatus



This Document SUPERSEDES 737-28A1141/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150398 ITEM: 1

737-28A1141 SB 00 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH Superseded (Superseded)1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1141 IN02737-28A1141-R0 (REF)737-28A1141-R1 (REF)737-28A1141-R2 (REF)737-28A1141-R3 (REF)737-28A1141-R4 (ACTIVE)PRODUCTION PRR38060-32SBB 737-28A1141 (MOD TASK)







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1141 SB 03 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH Superseded (Closed 17.Mar.2005)






737-28A1141-1 SB 00 MANDATORY A/C *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH Not Applicable by Serial Number1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1141 IN02737-28A1141-R0 (REF)737-28A1141-R1 (REF)737-28A1141-R2 (REF)737-28A1141-R3 (REF)737-28A1141-R4 (ACTIVE)PRODUCTION PRR38060-32SBB 737-28A1141 (MOD TASK)






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1168 SB 02 MANDATORY A/C FUEL QTY IND SYST/INSP OF WIRING HARNESS IN WING TANK Closed 02.Apr.2001

This document is effective for LN# 1001-3132.

Compliance:This SB ensures compliance with AD 2001-01-13 § (b)/(c).2001-01-13 (ACTIVE)737-28A1168-R0 (REF)737-28A1168-R1 (REF)737-28A1168-R2 (ACTIVE)

ADSBSBSB


02.Apr.2001PerfRev.:'NOTE' / Reason: DELIVERYDOC.


737-28A1174 SB 02 MANDATORY A/C *AD* BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Closed 20.Feb.20082005-04-01 (ACTIVE)737-28A1174 (REF)737-28A1174 IN 01 (REF)737-28A1174 R1 (REF)737-28A1174 R2 (REF)SBB 737-28A1174 (MOD-TASK)

ADSBSBSBSBTA








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1174 SB 01 MANDATORY A/C BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Superseded (Superseded)

2005-04-01 (ACTIVE)737-28A1174 (REF)737-28A1174 IN 01 (REF)737-28A1174 R1 (REF)737-28A1174 R2 (REF)SBB 737-28A1174 (MOD-TASK)

ADSBSBSBSBTA


737-28A1174-1 SB 02 MANDATORY A/C *AD* BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Not Applicable2005-04-01 (ACTIVE)737-28A1174 (REF)737-28A1174 IN 01 (REF)737-28A1174 R1 (REF)737-28A1174 R2 (REF)SBB 737-28A1174 (MOD-TASK)

ADSBSBSBSBTA

737-28A1192 SB 02 MANDATORY A/C *AD* AUXILIARY FUEL TANKS - IMPROVED FUELING FLOAT SWITCH Not ApplicableNAS has no Auxiliary fuel tanks installed.2006-15-05 (ACTIVE)737-28A1192-R0 (REF)737-28A1192-R1 (REF)737-28A1192-R2 (ACTIVE)SBB 737-28A1192 (MOD-TASK)

ADSBSBSBTA

Reason for this StatusAUX. FUEL TANKS NOT INST.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1210 SB 01 RECOMMENDED A/C MODIFICATION/REPLACEMENT OF THE P5-2 FUEL SYSTEM MODULE TO SUPPLY LOW

FUEL PRESSURE MASTER CAUTION ANNUNCIATIONSuperseded (Cancelled)

This SB is devided into 2 groups.NAS AC are in Group 2.

This document is applicable to LN# 292-3132.69-37335-28-04737-FTD-28-04003

SBFTD

0200

This Document SUPERSEDES 737-28A1210/SB Rev.00This Document has been SUPERSEDED BY 737-28A1210/SB Rev.02Reason for this StatusManually deassigned after Document Cancelled or Superseded

737-28A1210 SB 00 RECOMMENDED A/C FUEL- ENGINE FUEL FEED SYSTEM - REPLACEMENT OF THE P5-2 FUEL SYSTEMMODULE TO SUPPLY LOW FUEL PRESSURE MASTER CAUTION ANNUNCIATION

Superseded (Cancelled)

This SB is devided into 28 groups.NAS AC are in Group 10 (Eff. line 2) and 12 (Eff. line 3), all AC arecovered by SB Accomplishment instructions Part 2.

This document is applicable to LN# 292-3132.PRR35440-20R PRR 00This Document has been SUPERSEDED BY 737-28A1210/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1210 SB 02 RECOMMENDED A/C FUEL- ENGINE FUEL FEED SYSTEM - REPLACEMENT OF THE P5-2 FUEL SYSTEM

MODULE TO SUPPLY LOW FUEL PRESSURE MASTER CAUTION ANNUNCIATIONRejected by Operator

This SB is devided into 2 groups.NAS AC are in Group 2.

This document is applicable to LN# 292-3132.69-37335-28-04737-28A1210737-28A1210737-FTD-28-04003

SBSBSBFTD

03000100

This Document SUPERSEDES 737-28A1210/SB Rev.01Reason for this StatusAUTO ASSIGNED

737-28A1212 SB 00 RECOMMENDED A/C FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Superseded (Superseded)37-NAS-2841-002 (AWL TASK)65-49808-24-01 (ACTIVE)

TASB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1212 SB 02 MANDATORY A/C FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULT

INTERRUPTER (GFI) RELAY INSTALLATIONOpen

NSB has not performed the initial release of SB 737-28A1212. NSBoperates Group 2,4 aircraft.

EO 737-28A1212-01 covers Group 2 ACEO 737-28A1212-02 covers Group 4 AC

NSB will comply with AD by fulfilling the requirements of § (G),(1).(AD § (g).(2) is only for Group 1 and 8 aircraft.) and AD § (j) and(k). All this throug the two NAS EO.NSB will activate NAS task NAS-2841-002 upon completion of SB,thus complying with AD § (l).(2).2009-NM-228-AD2011-12-0965-49808-24-01 (ACTIVE)737-28A1212737-28A1212NAS-2841-002 (AWL TASK)PRR35440-10RS

NPRMADSBSBSBTAPRR

0000

00010000

This Document SUPERSEDES 737-28A1212/SB Rev.01Perform BEFORE 23.Jul.2014

737-28A1212/SB Rev.02 FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULTINTERRUPTER (GFI) RELAY INSTALLATION

Open

This Document SUPERSEDES 737-28A1212/SB Rev.01> 737-28A1212-01/EO* Rev.00 FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Open


18.Jun.2016Perform initially within (effective from15.Jul.2011) (F) 1800/D

> 737-28A1212-02/EO* Rev.00 FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Not Applicable





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusTHIS AC IS NA DUE TO BEEING IN GROUP 2, REF EO 737-28A1212-01

> 737-28A1212MPD/EO* Rev.00 737-28A1212MPD CONTROLLED BY MPD TASKS Taskcard ControlledReason for this StatusAUTO ASSIGNED

737-28A1212 SB 01 MANDATORY A/C FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULTINTERRUPTER (GFI) RELAY INSTALLATION


NSB has not performed the initial release of SB 737-28A1212. NSBoperates Group 2,4 and 13 aircraft.NSB will comply with AD by fulfilling the requirements of § (G),(1).(AD § (g).(2) is only for Group 1 and 8 aircraft.) and AD § (j) and(k). NSB will activate NAS task NAS-2841-002 upon completion of SB,thus complying with AD § (l).(2).2009-NM-228-AD65-49808-24-01 (ACTIVE)737-28A1212 IN-01NAS-2841-002 (AWL TASK)PRR35440-10RS

NPRMSBSBTAPRR

00

000000






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1216 SB 01 RECOMMENDED A/C FUEL - ENGINE FUEL FEED SYSTEM - INSTALLATION OF THE AUTO SHUTOFF

PROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPSSuperseded (Superseded)

SB is devided into 31 groups, 3 Parts and 3 Work packages.There are two configurations, PRE and POST SB 737-28A1212.

NAS AC have Config 1 , i.e SB 737-28A1212 is NOT performed onall AC. This is controlled per effectivity line. Configuration iscovered in the work instrusctions.2010-NM-189-AD28-AWL-2028-AWL-21737-28A1210737-FTD-28-04003PRR 35442-RSSB 69-37335-28-04

NPRMMPDMPDSBFTDPRRSB

00000000000002






24.Oct.2014/411


PROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPSRejected by Operator

No more work is required for AC changed per Rev 02 of the SB.NAS performs changes to AC per Rev 02 of the SB.NAS predicts that forthcoming AD will provide credit for AC done perRevision 02 of the SB.NAS rejects this SB revision.


NAS AC have Config 1 , i.e SB 737-28A1212 is NOT performed onall AC. This is controlled per effectivity line. Configuration iscovered in the work instrusctions.2010-NM-189-AD28-AWL-2028-AWL-21737-28A1210737-28A1210 IN-04737-28A1216-01737-28A1216-02737-28A1216-03737-28A1216-04737-28A1216-05737-FTD-28-04003PRR 35442-RSSB 69-37335-28-04

NPRMMPDMPDSBSBEOEOEOEOEOFTDPRRSB

00000000000000000000000002






24.Oct.2014/411


PROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPSRejected by Operator


NAS AC have Config 1 , i.e SB 737-28A1212 is NOT performed onall AC. This is controlled per effectivity line. Configuration iscovered in the work instrusctions.2010-NM-189-AD28-AWL-2028-AWL-21737-28A1210737-28A1210 IN-04737-28A1216-01737-28A1216-02737-28A1216-03737-28A1216-04737-28A1216-05737-FTD-28-04003PRR 35442-RSSB 69-37335-28-04

NPRMMPDMPDSBSBEOEOEOEOEOFTDPRRSB

00000000000000000000000002

This Document SUPERSEDES 737-28A1216/SB Rev.01Perform WITHIN 1080/D (effective from 12.Nov.2012)

737-28A1216/SB Rev.02 FUEL - ENGINE FUEL FEED SYSTEM - INSTALLATION OF THE AUTO SHUTOFFPROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPS


This Document SUPERSEDES 737-28A1216/SB Rev.01> 737-28A1216-01/EO* Rev.00 FUEL-INSTALLATION OF THE AUTO SHUTOFF PROTECTION FOR THE CENTER AND

AUXILIARY FUEL TANK BOOST PUMPS; GROUP 3 ACNot Applicable by Serial Number

> 737-28A1216-02/EO* Rev.00 FUEL-INSTALLATION OF THE AUTO SHUTOFF PROTECTION FOR THE CENTER ANDAUXILIARY FUEL TANK BOOST PUMPS; GROUP 22 AC


Reason for this Status





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusAUTO ASSIGNED

> 737-28A1216-03/EO* Rev.00 FUEL-INSTALLATION OF THE AUTO SHUTOFF PROTECTION FOR THE CENTER ANDAUXILIARY FUEL TANK BOOST PUMPS; GROUP 23 AC


> 737-28A1216-04/EO* Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - INSTALLATION OF THE AUTO SHUTOFFPROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPS


> 737-28A1216-05/EO* Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - INSTALLATION OF THE AUTO SHUTOFFPROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPS


737-28A1216 SB 00 RECOMMENDED A/C FUEL - ENGINE FUEL FEED SYSTEM - INSTALLATION OF THE AUTO SHUTOFFPROTECTION FOR THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPS


SB is devided into 20 groups, 3 Parts and 3 Work packages.Group 1-16:PART 1: AC with CTR tank pumps but NO AUX fuel tanks.Group 17-18:PART 2: AC with CTR tank pumps and previsions for AUXfuel tanks.Group 19-20:PART 3: AC with CTR tank and AUX tank.

All NAS AC have Config 1 status, i.e SB 737-28A1212 is not performed.28-AWL-2028-AWL-21737-28A1210737-28A1216 IN-01737-28A1216 IN-02737-28A1216 IN-03PRR 35442-RSSB 69-37335-28-04

MPDMPDSBSBSBSBPRRSB

0000000000000002






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1227 SB 01 RECOMMENDED A/C FUEL - DISTRIBUTION - CENTER AND AUXILIARY TANK BOOST PUMPS FUEL

CONTROL SYSTEM UN-COMMANDED ON RELAY INSTALLATIONRejected by Operator

This SB is applicable for AC that have a center tank andan auxiliary tank (or provisions for an auxiliarytank). All NAS AC are group 3 AC, the modification of Group 3 AC iscovered by EO 737-28A1227-01.737-28A1210737-28A1216737-28A1227737-28A1227 IN-03737-28A1227 IN-04737-28A1227 IN-05 (REPL IN-04)737-28A1227-01737-28A1228

SBSBSBSBSBSBEOSB

0000000000000000

This Document SUPERSEDES 737-28A1227/SB Rev.00Perform BEFORE 02.Aug.2015

737-28A1227/SB Rev.01 FUEL - DISTRIBUTION - CENTER AND AUXILIARY TANK BOOST PUMPS FUELCONTROL SYSTEM UN-COMMANDED ON RELAY INSTALLATION


This Document SUPERSEDES 737-28A1227/SB Rev.00> 737-28A1227-01/EO* Rev.00 FUEL - DISTRIBUTION - CENTER AND AUXILIARY TANK BOOST PUMPS FUEL

CONTROL SYSTEM UN-COMMANDED ON RELAY INSTALLATION ON GROUP 3 ACRejected by Operator

Reason for this StatusREJECTED, NON MANDATORY MOD NOT REQUIRED FOR THESE AC PER CONTRACT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1228 SB 01 RECOMMENDED A/C FUEL - DISTRIBUTION - INSTALLATION OF THE AUTO SHUTOFF PROTECTION FOR

THE CENTER AND AUXILIARY FUEL TANK BOOST PUMPSNot Applicable by Serial Number

MOD EFFECTIVITY LN# 16-158528-AWL-2028-AWL-21737-28A1210737-28A1228737-28A1228 IN-04PRR 35442-RSSB 69-37335-28-04

MPDMPDSBSBSBPRRSB

00000000000002


737-28A1228 SB 00 RECOMMENDED A/C FUEL - DISTRIBUTION - INSTALLATION OF THE AUTO SHUTOFF PROTECTION FORTHE CENTER AND AUXILIARY FUEL TANK BOOST PUMPS

Superseded (Not Applicable bySerial Number)

MOD EFFECTIVITY LN# 16-158528-AWL-2028-AWL-21737-28A1210737-28A1228 IN-01PRR 35442-RSSB 69-37335-28-04

MPDMPDSBSBPRRSB

000000000002






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1263 SB 01 MANDATORY A/C *AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. Superseded (Superseded)

2007-11-07 (SUPERSEDED)2007-24-02 (ACTIVE)37-SBB-28A1263 (REPETITIVE)737-28A1263-R0 (REF)737-28A1263-R1 (REF)737-28A1263-R2 (ACTIVE)

ADADTASBSBSB

This Document SUPERSEDES 737-28A1263/SB Rev.00This Document has been SUPERSEDED BY 737-28A1263/EO Rev.02

737-28A1263 SB 00 MANDATORY A/C *AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. Superseded (Superseded)2007-11-07 (SUPERSEDED)2007-24-02 (ACTIVE)37-SBB-28A1263 (REPETITIVE)737-28A1263-R0 (REF)737-28A1263-R1 (REF)737-28A1263-R2 (ACTIVE)

ADADTASBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1263 SB 02 MANDATORY A/C *AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. Repetitive

2007-11-07 (SUPERSEDED)2007-24-02 (ACTIVE)37-SBB-28A1263 (REPETITIVE)737-28A1263-R0 (REF)737-28A1263-R1 (REF)737-28A1263-R2 (ACTIVE)

ADADTASBSBSB

This Document CANCELS 737-28A1120/SB Rev.04Perform within an unlimited threshold.

737-28A1263/SB Rev.02 *AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. RepetitiveThis Document CANCELS 737-28A1120/SB Rev.04

> 737-28A1263/EO* Rev.02 FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP. *** MANDATORYREPETITIVE INSPECTION ***

Repetitive

This Document SUPERSEDES 737-28A1263/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

79536:00/HPerform initially before(F) 0/H /Interval(F):15000/H

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks06.Jul.2011 64536:00/H 37799/C 205193, N/A Was due at: 4055700/H PerfRev.:'02'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-28A1307 SB 00 MANDATORY A/C FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SUCTION FEED OPERATIONAL

TESTRepetitive

Mod applicability:All 737CL

Compliance:This SB ensures compliance with AD 2013-09-09 § (g)The SB is complied with through 2 EO:EO 737-28A1307-01: LH Eng.EO 737-28A1307-02: RH Eng.

NOTEThis recent release of the Ref AD contains a typographical errorregarding a reference to SB 737-28A1407. The correct reference is theSB 737-28A1307. The FAA is aware of the issue and is in the processof correcting the error through the Office of the Federal Register.See the attachment of the AD that highlights the two locations of thetypographical error, along with comments that contain the correctreference.2007-NM-351-AD2013-09-08737-28A1307-01737-28A1307-02737-FTD-28-04001

NPRMADEOEOFTD

0000000000

Perform WITHIN 720/D (effective from 14.May.2012) for the first timePerform WITHIN 7500/H (effective from 14.May.2012) for the first timeThereafter perform in an interval of 720/DThereafter perform in an interval of 7500/H

737-28A1307/SB Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SUCTION FEED OPERATIONALTEST

Repetitive





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-28A1307-01/EO* Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - LH ENGINE FUEL SUCTION FEED OPERATIONAL

TESTRepetitive


22.Feb.2016 79072:00/HPerform initially within (effective from14.May.2012) (F) 720/D or 7500/H /Interval(F):720/D or 7500/H


04.Mar.2014 71572:00/H 43151/C 489226, N/AWas due at: 04.May.2014 and 4456560/HPerfRev.:'00'

> 737-28A1307-02/EO* Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - RH ENGINE FUEL SUCTION FEED OPERATIONALTEST

Repetitive


22.Feb.2016 79072:00/HPerform initially within (effective from14.May.2012) (F) 720/D or 7500/H /Interval(F):720/D or 7500/H


04.Mar.2014 71572:00/H 43151/C 489227, N/AWas due at: 04.May.2014 and 4456560/HPerfRev.:'00'

737-29-1056 SB 00 RECOMMENDED A/C PTU CASE DRAIN PLUMBING MODIFICATION Ex Factory737-29-1056-R0 (ACTIVE)PPRODUCTION PRR34576

SBPRR


737-29-1058 SB 00 RECOMMENDED A/C RESVOIR PRESSURIZATION SYSTEM.B SYSTEM PLUMBING MODIFICATION Ex Factory737-29-1058-R0 (ACTIVE)PRODUCTION PRR34724

SBPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-29-1061 SB 02 RECOMMENDED A/C HYDRAULIC RESERVOIR VENT LINE MODIFICATION Rejected by Operator

737-29-1061-R2 (ACTIVE)PRODUCTION PRR34864

SBPRR

737-29-1062 SB 01 RECOMMENDED A/C MAIN, STANDBY AND GROUND SERVICE PRESSURE FILTER MODIFICATIO Not Applicable737-29-1062-R1 (ACTIVE)PRODUCTION LINE PRR34907

SBPRR

737-29-1064 SB 00 RECOMMENDED A/C (PTU) RELPACEMENT OF OUTLET PORT CHECK VALVE AND TUBE ASSEM. Open737-29-1064-R0 (ACTIVE)PRODUCTION PRR35146

SBPRR

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of DocumentNO LIMIT

737-29-1065 SB 01 RECOMMENDED A/C MODIFICATION OF RESERVOIR PRESSURIZATION MODULE Rejected by Operator737-29-1065-R1 (ACTIVE)737-SL-29-59 (REF)ESSEX SB 0091520200-2 (REF)PRODUCTION PRR 35183

SBSLSBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-29-1070 SB 00 MANDATORY A/C *AD* REV OF THE STDB SYS HYDR LEADING EDGE FLOW RESTRICTOR Closed 23.Feb.2000

This modification is applicable to LN# 1001-2720. The following LN#are Not Applicable per PRR35005-109.1998-07-16 XA (ACTIVE)737-29-1070 (REF)737-29-1070 NSC 1 (REF)PRODUCTION LINE PRR35005-109SBB 737-29-1070 (MAINT TASK)

ADSBSBPRRTA




737-29-1071 SB 00 MANDATORY A/C *AD* HYDRAULIC FUSES IN THE STANDBY SYSTEM REPLACEMENT Closed 13.Mar.1999This modification is applicable to LN# 1001-2791. The following LN#are Not Applicable per PRR35005-109.1998-07-16 XB (ACTIVE)35005-109 (PRODUCTION)737-29-1071 (ACTIVE)SBB 737-29-1071 (MAINT TASK)

ADPRRSBTA




737-29-1079 SB 00 RECOMMENDED A/C HYDRAULIC POWER-PARKING BRAKE MOTOR Rejected by Operator737-29-1079 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-29-1080 SB 00 RECOMMENDED A/C HYD PUMPING, STBY HYD MOTOR PUMP Rejected by Operator

737-29-1080 SB

737-29-1091 SB 01 RECOMMENDED A/C HYDRAULIC POWER-DC MOTOR OPERATED Rejected by Operator737-29-1091 SB

737-29-1093 SB 00 RECOMMENDED A/C MODIFICATION OF THE RESERVOIR PRESSURIZATION MODULE Open737-29-1093-R0 (ACTIVE)737-SRP-29-0057 (REF)PRODUCTION PRR38275-21

SBSRPPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-29-1115 SB 01 RECOMMENDED A/C HYDRAULIC POWER - MAIN - HYDRAULIC SYSTEM(S) PRESSURE MODULE CHECK

VALVE INSPECTION AND REPLACEMENTClosed 03.Mar.2014 W/O:502760

This service bulletin gives instructions to inspect and replace, ifnecessary, the pressure module check valves in hydraulic system A for737-100/200/200C airplanes and hydraulic systems A and B for737-300/400/500 airplanes. If this service bulletin is not done andhydraulic pressure is applied to a fractured check body, theincreased pressure can cause the check valve head to separate fromthe module. Pressurized separation of the check valve head can resultin injuries to maintenance personnel and damage to the Main LandingGear (MLG) wheel well structure.

All NAS AC are group 2

EO 737-29-1115-01 issued for inspection.EO 737-29-1115-02 issued for replacement.

NAS will perform replacement of all P/N H61C0552M1 (Boeing SPEC P/N10-60491-3).BOEING FTD 737-29-09001BOEING SL 737-SL-29-108

FTDSL

0000

This Document SUPERSEDES 737-29-1115/SB Rev.00Perform BEFORE 24.Sep.2014

737-29-1115/SB Rev.01 HYDRAULIC POWER - MAIN - HYDRAULIC SYSTEM(S) PRESSURE MODULE CHECKVALVE INSPECTION AND REPLACEMENT

Closed 03.Mar.2014 W/O:502760

This Document SUPERSEDES 737-29-1115/SB Rev.00> 737-29-1115-01/EO* Rev.00 HYDRAULIC SYSTEMS A AND B PRESSURE MODULE CHECK VALVE INSPECTION Closed 26.Nov.2013 W/O:493150

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks26.Nov.2013 71152:00/H 42819/C 493150, N/A Was due at: 23.Sep.2014 PerfRev.:'00'

> 737-29-1115-02/EO* Rev.00 HYDRAULIC SYSTEMS A AND B PRESSURE MODULE CHECK VALVE REPLACEMENT Closed 03.Mar.2014 W/O:502760Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status03.Mar.2014 71572:00/H 43151/C 502760, N/A Was due at: 23.Sep.2014 PerfRev.:'00'

737-29-1115 SB 00 RECOMMENDED A/C HYDRAULIC POWER - MAIN - HYDRAULIC SYSTEM(S) PRESSURE MODULE CHECKVALVE INSPECTION AND REPLACEMENT


BOEING FTD 737-29-09001BOEING SL 737-SL-29-108

FTDSL

0000


737-29A1073 SB 04 RECOMMENDED A/C HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE INSPECTION Closed 21.Feb.19982001-11-07737-29A1073737-29A1073737-29A1073737-29A1073737-29A1073

ADSBSBSBSBSB

000001020304








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-29A1076 SB 01 MANDATORY A/C *AD* HYD SYS B MOTOR DRIVEN PUMP WIRE BUNDLE INSP/CLAMP INST Closed 23.Mar.2000

1999-26-21 (ACTIVE)737-29A1076 IN 02 (REF)737-29A1076-R0 (REF)737-29A1076-R1 (ACTIVE)PRODUCTION PRR35005-220

ADSBSBSBPRR




737-29A1078 SB 02 MANDATORY A/C REPLACEMENT OF DC MOTOR OPERATED SHUTOFF VALVE Not Applicable2001-11-07737-29A1078737-29A1078

ADSBSB

000001

Reason for this StatusNOT APPLICABLE DUE TO EFFECTED PARTS NOT INSTALLED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-29A1096 SB 02 MANDATORY A/C *AD* HYD HEAT EXCHANGER, ELECT. BONDING AT FITTING INTO TANK Closed 19.May.2002

2004-10-06 (ACTIVE)737-29A1096-R0 (REF)737-29A1096-R1 (REF)737-29A1096-R2 (ACTIVE)PRODUCTION MRR3290-1408SBB 737-29A1096 (MOD-TASK)

ADSBSBSBPRRTA




737-30-1034 SB 00 RECOMMENDED A/C P5 FORWARD OVERHEAD PANEL WIRING MODIFICATION Not Applicable by Serial Number737-30-1034-R0 SB

737-30-1039 SB 00 RECOMMENDED A/C WINDOWS AND WINDHIELDS - WINDOWS NO.2 WIRING MODIFICATION Open737-30-1039-R0 SBDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT

737-30-1041 SB 00 RECOMMENDED A/C WING THERMAL ANTI-ICING SYSTEM DUCT REPLACEMENT Rejected by Operator737 SL 57-38 (REF)737-30-1041-R0 (ACTIVE)

SLSB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-30-1043 SB 02 RECOMMENDED A/C RAIN REPELLENT SYSTEM TEMPORARY OR PERMANT DEACTIVATION Rejected by Operator

737-30-1043-R2 (ACTIVE)737-SRP-30-0009 (REF)PRR35005-157R

SBSRPPRR

Reason for this StatusNO TIME





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-30-1067 SB 00 UNKNOWN A/C ICE AND RAIN PROTECTION - PITOT STATIC TUBES, TEMPERATURE PROBE, AND

ALPHA VANE ANTI-ICING SYSTEM - J18 JUNCTION BOX INSTALLATIONRejected by Operator / Special Text:Group 1 AC

Boeing has received reports that the Pitot Heat switch is not alwaysset to ON.

Boeing Fleet Team Digest (FTD) 737 FTD 30-8001 is related to thisservice bulletin.

Boeing Service Related Problem (SRP) 737-SRP-30-0032 is related tothis service bulletin.

No more work on the classics in NAS. SB rejected by operator until ADis possibly released.737-30-1068737-SL-51-048737-SRP-30-0032AMM 24-22-00,25-52-91,30-31-00FTD 30-8001NDT MANUAL PART 6PRR 35005-295RSSOPMSWPM

SBSLSRPAMMFTDNDTBPRRSOPMSWPM

LAST00LASTLASTLASTLASTLASTLASTLAST






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-30-1068 SB 00 RECOMMENDED A/C PITOT STATIC TUBES, TEMPERATURE PROBE, AND ALPHA VANE ANTI-ICING SYSTEM

- AIR DATA PROBE HEAT AUTOMATION WIRE PROVISIONS INSTALLATIONRejected by Operator

This service bulletin provides the instructions and the kits toinstall wiring provisions for changes to the anti-icing system forthe angle of attack sensor, the total air temperature, and the pitotstatic tubes. The changes to the system will let the anti-icingsystem automatically supply power to heat the pitot static tubes.

The Federal Aviation Administration (FAA) will possibly release anAirworthiness Directive related to this service bulletin. TheAirworthiness Directive will make the compliance tasks and timesgiven in this service bulletin mandatory.737-30-1068IN01AMM 24-22-00, 25-31-11, 25-40-01BAE SB 69-37346-30-04PRR 35005-29RSSOPM 20-50-01, 20-50-05SWPM 20-10-11,12,14,18,19,27SWPM 20-30-11,12,16,22SWPM 20-60-08,09,61-11, 71-11WDM 24-54-11,21, 30-31-01WDM 78-32-01,11,21

SBAMMSBPRRSOPMSWPMSWPMSWPMWDMWDM

IN01LASTLASTLASTLASTLASTLASTLASTLASTLAST

737-30-1068/SB Rev.00 PITOT STATIC TUBES, TEMPERATURE PROBE, AND ALPHA VANE ANTI-ICING SYSTEM- AIR DATA PROBE HEAT AUTOMATION WIRE PROVISIONS INSTALLATION


> 737-30-1068-01/EO* Rev.00 PITOT STATIC TUBES, TEMPERATURE PROBE, AND ALPHA VANE ANTI-ICING SYSTEM- AIR DATA PROBE HEAT AUTOMATION WIRE PROVISIONS INSTALLATION

Rejected by Operator / Special Text:Group 5 AC

Reason for this StatusRejected due to high cost/manpower until possible AD release







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-30-1068-03/EO* Rev.00 PITOT STATIC TUBES, TEMPERATURE PROBE, AND ALPHA VANE ANTI-ICING SYSTEM

- AIR DATA PROBE HEAT AUTOMATION WIRE PROVISIONS INSTALLATIONNot Applicable by Serial Number







737-30-1069 SB 01 RECOMMENDED A/C PITOT STATIC TUBES, TEMPERATURE PROBE, AND ALPHA VANE ANTI-ICING SYSTEM- CHANGE P5 AND P18-3 PANELS DEACTIVATION

Not Applicable

This service bulletin gives the instructions to deactivate the AirData Probe Heat Automation system after Boeing Service Bulletin737-30A1064 was done. Deactivation of the Air Data Probe HeatAutomation system will allow the operator to put the airplane inservice until certification is complete.20-10-11, 20-10-12, 20-10-1920-50-0524-22-00, 30-31-00, 30-41-0030-90-11737-30A1064PRR 35005-295RS

SWPMSOPMAMMAMMSBPRR

LATELATELATELATELATELATE

This Document SUPERSEDES 737-30-1069/SB Rev.00Reason for this StatusSB 737-30-1069 not yet performed





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-30-1069 SB 00 RECOMMENDED A/C PITOT STATIC TUBES, TEMPERATURE PROBE, AND ALPHA VANE ANTI-ICING SYSTEM

- CHANGE P5 AND P18-3 PANELS DEACTIVATIONSuperseded (Not Applicable)

This service bulletin gives the instructions to deactivate the AirData Probe Heat Automation system after Boeing Service Bulletin737-30A1064 was done. Deactivation of the Air Data Probe HeatAutomation system will allow the operator to put the airplane inservice until certification is complete.20-10-11, 20-10-12, 20-10-1920-50-0524-22-00, 30-31-00, 30-41-0030-90-11737-30A1064PRR 35005-295RS

SWPMSOPMAMMAMMSBPRR

LATELATELATELATELATELATE

This Document has been SUPERSEDED BY 737-30-1069/SB Rev.01Reason for this StatusSB 737-30A1064 NOT INTRODUCED IN NAS

737-300766-28-2 SB 06 MANDATORY A/C *AD* FUEL QUANTITY - ADD BONDING STRAPS TO SAFE SIDE HARNESS Closed 08.Apr.20062005-05-17 (ACTIVE)BFG 737-300766-28-2 REV6BFG V-1520 (REF)SB 737-300766-28-2 (MOD-TASK)

ADSBSBTA


08.Apr.2006 49236:11/H 26197/CWas due at: 18.Apr.2006 PerfRev.:'06' WOKKM150651 ITEM 1

Reason for this StatusWO KKM150651 ITEM 1





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-30A1059 SB 02 MANDATORY A/C ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THE

WINDSHIELD WIPER MOTORNot Applicable

Applicable to -400 and -500 onlyThis Document SUPERSEDES 737-30A1059/SB Rev.01Reason for this StatusAUTO ASSIGNED

737-30A1059 SB 01 MANDATORY A/C ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THEWINDSHIELD WIPER MOTOR

Superseded (Not Applicable /Special Text: This aicraft is NotApplicable by Aircraft Model.)

Applicable to -400 and -500 onlyThis Document has been SUPERSEDED BY 737-30A1059/SB Rev.02Reason for this StatusAUTO ASSIGNED

737-31-1064 SB 01 RECOMMENDED A/C AURAL WARNING SYSTEM - PARKING BRAKE TAKE-OFF WARNING SYSTEM Not Applicable by Serial Number737-31-1064-R1 (ACTIVE)PRODUCTION PRR 34666

SBPRR

737-31-1072 SB NOTE

RECOMMENDED A/C DIGITAL FLIGHT DATA ACQUISITION UNIT - WIRE CHANGE Closed 31.Mar.1993

737-31-1072-R1 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Mar.1993PerfRev.:'NOTE' / Reason: DELVERY DOCWO:

Reason for this StatusDELVERY DOC WO:





24.Oct.2014/411


TERECOMMENDED A/C FLIGHT RECORDER SYSTEM - ADDITION OF SENSOR/TRANSMITTERS Closed 20.Mar.2000

737-31-1099-R1 (ACTIVE)PRODUCTION PRR35317-R

SBPRR




737-31-1112 SB NOTE

RECOMMENDED A/C FLT RECORDER SYS.- ADD. OF THE RUDDER PEDAL FORCE TRANSDUCER Closed 01.Apr.2001

737-31-1112-R0 (REF)737-31-1112-R1 (REF)737-31-1112-R2 (ACTIVE)BOEING PROGRAM LETTER6-1151-7PRODUCTION PRR35361 (REF)

SB

SB

SB

DOCR

PRR




737-31-1144 SB NOTE

RECOMMENDED A/C ADDITION OF WIRING FOR SENSORS FOR FLIGHT Rejected by Operator

737-31-1144 SB

737-31-1190 SB 00 RECOMMENDED A/C FLIGHT RECORDER SYSTEM - FLIGHT DATA ACQUISITION UNIT, REMOVAL ANDREPLACEMENT






24.Oct.2014/411


TEOPTIONAL A/C IND/REC SYS - FLIGHT DATA RECORDING SYSTEM DATA FRAME CHANGE Not Applicable by Serial Number

SBB 737-31-1226 SB

737-31-1244 SB NOTE

OPTIONAL A/C REPL. DIGITAL FLIGHT DATA ACQUISITION UNIT/DIGITAL FLIGHT D. Not Applicable by Serial Number

737-31-1244-R0 (REF)PRODUCTION LINEMC3132MK3298

SB

PRR

737-31A1325 SB 00 MANDATORY A/C IND./RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THECABIN ALT. WARNING SYS. AND TAKEOFF CONFIGURATION WARNING SYS. LIGHTS


Tek-Ops meeting decided not to implement this SB as the aircraft willbe phased out before mandate compliance date.

KKB will get the SB installed per agreement with lessor.

This SB ensures compliance with AD 2012-19-11 § (h).This Document has been SUPERSEDED BY 737-31A1325/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded

737-31A1325 SB 01 MANDATORY A/C INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INST. OF THECABIN ALTITUDE WARNING SYSTEM AND TAKEOFF CONFIG.WARNING SYSTEMLIGHTS

Closed 05.Mar.2014 W/O:436905

Rev.01 of this SB is approved as an AMOC to AD 2001-03-14, ref SBsection 1.F.This Document SUPERSEDES 737-31A1325/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Mar.2014 71572:00/H 43151/C 436905, N/A Was due at: 13.Mar.2014 PerfRev.:'01'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-31A1325 SB 02 MANDATORY A/C INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INST. OF THE

CABIN ALTITUDE WARNING SYSTEM AND TAKEOFF CONFIG.WARNING SYSTEMLIGHTS

See prev. Docstatus

No more work is necessary on the airplane(s) changed in accordancewith the original issue or Revision 1 of this service bulletin.

All NAS airplanes perf. per rev.01 of SB.Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Mar.2014 71572:00/H 43151/C N/A Was due at: 13.Mar.2014 PerfRev.:'01'

737-31A1398 SB NOTE

OPTIONAL A/C INDICATING/RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTAL Not Applicable by Serial Number

737-31A1398 SB

737-32-1123 SB 04 RECOMMENDED A/C MAIN GEAR - LUBRICATION PROVISIONS AND FUSE BOLT INSPECTION ANDREPLACEMENT


737-32-1123 SB

737-32-1129 SB 03 RECOMMENDED A/C NOSE LANDING GEAR TORSION LINK PIN AND SHAFT REPLACEMENT Rejected by Operator33194RPRR33194R737-32-1129737-32-1129 NSC 01737-32-1129 NSC 02

PRRDOCRSBSBSB

0000030000

(Same header)(Same header)





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1160 SB 01 OPTIONAL A/C 737-200 N/W AND TIRE ASSEMBLY FOR LIMITED USE ON 737-300 Not Applicable / Special Text: Not

appicable due to MSN/ Line no.NAS DOES NOT ALLOW THE USE OF 737-200 NOSE WHEEL PN ON NAS 737-300.737-32-1060-R1 (ACTIVE) SBThis Document SUPERSEDES 737-32-1160/SB Rev.00Reason for this StatusAUTO ASSIGNED

737-32-1160 SB 00 OPTIONAL A/C 737-200 N/W AND TIRE ASSEMBLY FOR LIMITED USE ON 737-300 Superseded (Not Applicable)737-32-1060-R1 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-32-1160/SB Rev.01Reason for this StatusN/A COMBINATION NOT USED

737-32-1163 SB 06 RECOMMENDED A/C LANDING GEAR-HYDRAULIC BRAKE SYSTEM ACCUMULATOR PRESSURE RELIEFVALVE ADDITION


34555737-32-1163

PRRSB

0006

737-32-1186 SB 06 OPTIONAL A/C WHEELS, TIRES, AND BRAKES REPLACEMENT WITH B. F. GOODRICH Closed 17.Aug.2013 W/O:451957737-32-1186737-32-1186 IN 02PRR 34179R

SBSBSB

0600NA

Perform within an unlimited threshold.737-32-1186/SB Rev.06 WHEELS, TIRES, AND BRAKES REPLACEMENT WITH B. F. GOODRICH Closed 17.Aug.2013 W/O:451957> 737-32-1186-01/EO* Rev.00 WHEELS, TIRES, AND BRAKES REPLACEMENT WITH B. F. GOODRICH VERIFICATION

EARLIER PERFORMEDClosed 17.Aug.2013 W/O:451957

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Aug.2013 70272:00/H 42157/C 451957, N/A Was due at: 30.Sep.2013 PerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1191 SB 04 RECOMMENDED A/C MAIN AND NOSE GEAR - INNER CYLINDER AXLE INSP AND REPAIR Superseded (Cancelled)

737-32-1191737-32-1191 IN 04

SBSB

0400

This Document has been SUPERSEDED BY 737-32-1191/SB Rev.05Reason for this StatusManually deassigned after Document Cancelled or Superseded

737-32-1191 SB 05 RECOMMENDED A/C MAIN GEAR AND NOSE GEAR - INNER CYLINDER AXLE INSPECTION AND REPAIR OpenTo be perf when required or necessary at shop visit.SB text edit only from Rev.4This Document SUPERSEDES 737-32-1191/SB Rev.04Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT

737-32-1209 SB 01 RECOMMENDED A/C NLG STEERING CYLINDER TRUNNION BEARING REPLACEMENT Not Applicable by Serial Number737-32-1209-R1 (ACTIVE)PRODUCTION LINE PRR33890-39

SBPRR

737-32-1211 SB 02 RECOMMENDED A/C NLG-STEERING METERING VALVE COVER BRACKET AND SUPPORT MOD. Rejected by Operator737-32-1211-R2 (ACTIVE)PRODUCTION LINE PRR 34474

SBPRR

737-32-1213 SB 03 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Superseded (Cancelled)This Document SUPERSEDES 737-32-1213/SB Rev.02This Document has been SUPERSEDED BY 737-32-1213/SB Rev.04Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1213 SB 05 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Superseded (Cancelled)

PRODUCTION PRR 35161 PRRThis Document SUPERSEDES 737-32-1213/SB Rev.04This Document has been SUPERSEDED BY 737-32-1213/SB Rev.06Reason for this StatusManually deassigned after Document Cancelled or Superseded

737-32-1213 SB 10 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Rejected by Operator / Special Text:GROUP 1-3 - CONFIG TO BECHECKED INDIVIDUALLY

Additional Work requiredPRR 35005-188PRR 35161

PRRPRR

NANA

This Document SUPERSEDES 737-32-1213/SB Rev.09Reason for this StatusAUTO ASSIGNED

737-32-1213 SB 00 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Superseded (Cancelled)This Document has been SUPERSEDED BY 737-32-1213/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded

737-32-1213 SB 06 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Superseded (Cancelled)PRODUCTION PRR 35161 PRRThis Document SUPERSEDES 737-32-1213/SB Rev.05This Document has been SUPERSEDED BY 737-32-1213/SB Rev.07Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411


PRODUCTION PRR 35161 PRRThis Document SUPERSEDES 737-32-1213/SB Rev.07This Document has been SUPERSEDED BY 737-32-1213/SB Rev.09Reason for this StatusManually deassigned after Document Cancelled or Superseded


737-32-1213 SB 04 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Superseded (Closed 08.Dec.1995)PRODUCTION PRR 35161 PRRThis Document SUPERSEDES 737-32-1213/SB Rev.03This Document has been SUPERSEDED BY 737-32-1213/SB Rev.05Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.1995NASDELIVERYDOCS

PerfRev.:'04'

737-32-1213 SB 01 RECOMMENDED A/C NOSE GEAR AND DOORS - WIRE CONDUIT REPLACEMENT Superseded (Cancelled)This Document SUPERSEDES 737-32-1213/SB Rev.00This Document has been SUPERSEDED BY 737-32-1213/SB Rev.02Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411


This Document SUPERSEDES 737-32-1213/SB Rev.01This Document has been SUPERSEDED BY 737-32-1213/SB Rev.03Reason for this StatusManually deassigned after Document Cancelled or Superseded


737-32-1215 SB 01 RECOMMENDED A/C REPLACEMENT OF MAIN LANDING GEAR WHEELS AND BRAKES Not Applicable by Serial Number737-32-1215-R1 (ACTIVE)PRODUCTION LINEMC3240MK3038

SB

PRR

737-32-1217 SB 04 RECOMMENDED A/C INSP, REWORK OR REPLACEMENT OF THE FORWARD TRUNNION BEARING Rejected by Operator737-300 is Group 2 AirplanesNAS might have been accomplished by other operator but rejected byNAS. Therefore NO interval for inspection.737-32-1217-R4 (ACTIVE)PRODUCTION PRR35005-91

SBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1227 SB 04 OPTIONAL A/C WHEELS, TIRES AND BRAKES REPLACEMENT WITH HONEYWELL/BENDIX Rejected by Operator

737-32-1227 R0 (REF)737-32-1227 R01 (REF)737-32-1227 R02 (REF)737-32-1227 R03 (REF)737-32-1227 R04 (ACTIVE)

SBSBSBSBSB

737-32-1234 SB 03 RECOMMENDED A/C MAIN GEAR LOCK ACTUATOR HOSE INSPECTION AND REPLACEMENT Closed 02.Mar.1994737-32-1234-R3 (ACTIVE)PRODUCTION PRR34710

SBPRR




737-32-1235 SB 00 RECOMMENDED A/C MAIN LANDING GEAR BRAKE STUD MODIFICATION Not Applicable by Serial Number737-32-1235-R0PPRODUCTION PRR 34746

SBPRR

737-32-1236 SB 01 RECOMMENDED A/C NOSE WHEEL STEERING - LANDING GEAR TRANSFER VALVE - REWORK Superseded (Not Applicable)737-32-1236-R2 (ACTIVE)PRODUCTION PRR34390-02

SBPRR


737-32-1236 SB 02 RECOMMENDED A/C NOSE WHEEL STEERING - LANDING GEAR TRANSFER VALVE - REWORK Not Applicable737-32-1236-R2 (ACTIVE)PRODUCTION PRR34390-02

SBPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1238 SB 00 OPTIONAL A/C BRAKE VALVE SUPPORT HOUSING INSPECTION AND REPLACEMENT Not Applicable by Serial Number

737-32-1238-R0 (ACTIVE)SBB 737-32-1238 (MOD-TASK)

SBTA

737-32-1245 SB 01 RECOMMENDED A/C MAIN LANDING GEAR SAFETY SENSOR COVER REPLACEMENT Closed 02.Feb.1994737-32-1245-R1 (ACTIVE)PRODUCTION LINE PRR34782

SBPRR




737-32-1253 SB 00 MANDATORY A/C LANDING GEAR - WHEEL AND BRAKES - BRAKE MOUNTING GASKET REPLACEMENTWITH ALUMINIUM-NICKEL-BRONZE GASKET.

Closed 19.Nov.2000

References:/A/: SB 737-32-1253 NSC-1/B/: SB 737-32-1253 NSC-2Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

19.Nov.200043995 ITEM704

PerfRev.:'00' / Reason: PERFORMED BYAEROPLEX

Reason for this StatusPERFORMED BY AEROPLEX

737-32-1257 SB 01 RECOMMENDED COMP MAIN LANDING GEAR ORIFICE SUPPORT TUBE REPAIR Rejected by Operator737-32-1257-R1 (ACTIVE) SBAffected Rotables (Part No/Serial No/Position) Status

65-46160-10 / 0093 Pos=RH (KKM)Rejected by Operator / Reason: AUTOASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1261 SB 01 RECOMMENDED A/C PARKING BRAKE PUSH ROD REPLACEMENT AND/OR REWORK See prev. Docstatus / Special Text:

Not appicable due to MSN/ Line no.737-32-1261-R1 (ACTIVE) SBThis Document SUPERSEDES 737-32-1261/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks31.Mar.1991 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC WO:

737-32-1261 SB 00 RECOMMENDED A/C PARKING BRAKE PUSH ROD REPLACEMENT AND/OR REWORK Superseded (Closed 31.Mar.1991)737-32-1261-R1 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-32-1261/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-32-1264 SB 00 OPTIONAL A/C LANDING GEAR - ACTUATOR HEAD AND BEARING END, REPLACEMENT OF Rejected by Operatorthis SB has been rejected by all previous operators.Reason for this StatusREJECTED BY PREVIOUS OPERATOR.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1267 SB 00 OPTIONAL A/C HYDRAULIC BRAKE SYS/INST CHECK VALVES IN THE ALTERNATE BRAKE Closed 05.May.1994

737-32-1267-R0 (ACTIVE)PRODUCTION PRR35005-20SBB 737-32-1267 (INSP-TASK)

SBPRRTA


05.May.1994PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.


737-32-1275 SB 00 RECOMMENDED A/C MAIN GEAR ACTUATOR PLUMBING MODIFICATION Rejected by Operator737-32-1275-R0 (ACTIVE) SB

737-32-1282 SB 01 RECOMMENDED A/C PARKING BRAKE SYSTEM - PARK BRAKE LIGHT ACTIVATION Rejected by Operator737-32-1282-R1 (ACTIVE)PRODUCTION LINE MRR3324-1051

SB

PRR

737-32-1289 SB 00 RECOMMENDED A/C NLG-STEERING METERING VALVE COVER MODIFICATION Rejected by Operator737-32-1289 SB 00

737-32-1298 SB 00 RECOMMENDED A/C INSP.OF WIRING AND ADDITION OF WIRE BUNDLE AND HYDRAULIC TUB Closed 13.Feb.1999737-32-1298-R1 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1303 SB 00 RECOMMENDED COMP ACTUATOR SNUBBING OPERATOR REPL, AND TAB LOCKWASHER INST. Rejected by Operator

Rejected by operator, no safety or cost benefit.737-32-1303-R0 (ACTIVE)737-SRP-32-0080 (REF)PRODUCTION PRR35005-222WARRANTY JULY 28, 1994

SBSRPPRRSB


65-44910-27 / TSC2566X Pos=LH (KKM)Rejected by Operator / Reason: AUTOASSIGNED

65-44910-32 / TSC4348 Pos=RH (KKM) Not Applicable / Reason: 125996

737-32-1322 SB 01 MANDATORY COMP *AD* MLG/NLG LIFE LIMITED COMPONENTS TRACKING & S/N ADDITION Closed 11.Sep.20062003-07-12 (ACTIVE)737-32-1322-R0 (REF)737-32-1322-R1 (ACTIVE)737-SRP-32-0058 (REF)SBB 737-32-1322P1 (REPET)SBB 737-32-1322P2 (INSP-TASK)

ADSBSBSRPTATA


65-73762-21 / T3011 Pos=FWD (KKM)Closed / Last Performed:11.Sep.200627172/C RefDocument:SRT E0553431 OH2006 Rev.01

65-73761-127 / MC03525 Pos=LH (KKM)Closed / Last Performed:08.Jul.200527929/C RefDocument:PCW SRTE0403521 OH 2005 Rev.01

65-73761-128 / MC03526 Pos=RH (KKM)Closed / Last Performed:08.Jul.200527979/C RefDocument:PCW SRTE0403522 OH 2005 Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1425 SB 00 RECOMMENDED COMP NOSE LANDING GEAR TORSION LINK PIN INSP. AND REPLACEMENT Not Applicable by Serial Number /

Special Text: PART NO. NOTAFFECTED BY BULLETIN

Applicable for Line no. 1 thru 3132 with SB 737-32-1129 incorporatedand /or suspected partno./serials installed737-32-1129 (REF)737-32-1425-R0 (ACTIVE)737-SL-32-155 (REF)

SBSBSL


65C34776-1 / OII-147 Pos=FWD (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN /Reason: 94447

65C37823-2 / 036 Pos=LOWER (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN

69-41248-3 / SI2351 Pos=FWD (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN /Reason: 94448

65C37823-2 / 038 Pos=UPPER (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32-1459 SB 00 RECOMMENDED A/C LANDING GEAR - TIRES AND WHEELS - CHANGE MAXIMUM TAXI WEIGHT TO 140,000

POUNDS AND MAXIMUM TAKEOFF WEIGHT TO 139,500 POUNDSNot Applicable by Serial Number

Publications Affected by performing this SB:737 FAA Approved Airplane Flight Manual, Section 1737 Flight Crew Operations Manual, Limitations737 Maintenance Manual 12-15, 20-10, 30-00737 Illustrated Parts Catalog, 11-20737 Weight and Balance Manual, 1-02

NOTE: Boeing has evaluated the repairs and/or changes in this servicebulletin for effects on Fatigue Critical Structure (FCS) and forchanges to Damage Tolerance Inspections (DTI) required in theMaintenance Program. This service bulletin does not affect FCS,therefore DTIs are not necessary.

737-32A1224 SB 03 MANDATORY A/C *AD* MLG TRUNNION PIN, ACTUATOR BEAM ARM, AND ACTUATOR BOLT Closed 08.Jul.20051991-05-16 (SUPERSEDED)1999-10-12 (ACTIVE)37-SBB-32A1314 (REPETITIVE)737-32-1224-R3 (ACTIVE)737-32A1314 (REF)PRODUCTION LINE PRR34875

ADADTASBSBPRR


08.Jul.2005 27979/CPCW PER OHSR-TECHREPORT 2005

PerfRev.:'03'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32A1301 SB 00 RECOMMENDED COMP REVISE THE TIE BOLTS ON THE MAIN LANDING GEAR WHEELS Not Applicable / Special Text: PART

NO. NOT AFFECTED BYBULLETIN

3-1398-32-16 (BF-GOODRICH)3-1439-32-13 (BF-GOODRICH)737-32A1301-R0 (ACTIVE)737-SRP-32-0079 (REF)PRODUCTION LINE PRR35005-217

SBSBSBSRPPRR


3-1439-6 / 3949 Pos=#3 (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN /Reason: 45855

3-1439-6 / 9284P Pos=#1 (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN /Reason: 189940

3-1439-6 / 8512 Pos=#4 (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN /Reason: 71146

3-1439-6 / 3610 Pos=#2 (KKM)Not Applicable / Special Text: PART NO.NOT AFFECTED BY BULLETIN /Reason: AUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-32A1355 SB 02 MANDATORY COMP LANDING GEAR - MAIN GEAR EXTENSION AND RETRACTION - RETRACT ACTUATOR

BEAM INSPECTION AND REWORKOpen

2009-09-07 (ACTIVE)37-SBB-32A1355P1 (REPET-TASK)37-SBB-32A1355P2 (REPET-TASK)737-32A1355-R1 (REF)737-32A1355-R2 (ACTIVE)737-32A1355-RO (REF)737-SL-20-041 (REF)737-SRP-32-0111 (REF)737-SRP-32-0138 (REF)AD 2009-09-07 (SECONDARYTASK)PRODUCTION LINEPRR35005-245RS

AD

TA

TA

SB

SB

SB

SL

SRP

SRP

AD

PRRPerform BEFORE 31.Dec.2010

737-32A1355/SB Rev.02 LANDING GEAR - MAIN GEAR EXTENSION AND RETRACTION - RETRACT ACTUATORBEAM INSPECTION AND REWORK

Open

> 737-32A1355-01/EO* Rev.00 *AD* MLG RETRACT ACTUATOR BEAM INSPECTION/REWORK/OVERHAUL Closed 10.Sep.2008Affected Rotables (Part No/Serial No/Position) Status

65-46108-19 / 1051 Pos=RH (KKM)Closed / Reason: EO403526 44610 / LastPerformed:27.Jun.2005 46143:00/H23575/C RefDocument: Rev.NOTE

65-46108-17 / 75 Pos=LH (KKM)Closed / Reason: WO EO662798 44611 /Last Performed:10.Sep.2008 54036:00/H29925/C RefDocument: Rev.NOTE

> 737-32A1355P1/EO* Rev.00 *AD* *AD* MLG RETRACT ACTUATOR BEAM REPEAT INSPECTION Not ApplicableAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

> 737-32A1355P2/EO* Rev.00 *AD* *AD* MLG RETRACT ACTUATOR BEAM REPEAT OVERHAUL OpenAffected Rotables (Part No/Serial No/Position) Status





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status65-46108-17 / 75 Pos=LH (KKM) Open / Next Due:08.Sep.201865-46108-19 / 1051 Pos=RH (KKM) Open / Next Due:25.Jun.2015

737-32A1367 SB 00 MANDATORY A/C *AD* MLG, TRUNION PIN, ACT. BEAM BOLT/TEE-FITTING BOLT INSP Closed 16.Mar.20052005-20-39 (ACTIVE)37-32-001(TECHNICAL DIRECTIVE)737-32A1367-R1 (ACTIVE)737-32A1367-RO (REF)DE#74320PRODUCTION LINEMRR3323-1546SSBB 737-32A1367 (INSP-TASK)

ADTDSBSBDOCRPRRTA




737-33-1082 SB 00 RECOMMENDED A/C PASSENGER COMPARTMENT/CB WIRE CHANGE FOR CEILING LIGHTS Closed 02.Nov.1992737-33-1082-RO (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

02.Nov.1992PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-33-1084 SB 00 RECOMMENDED A/C LIGHTS-FLIGHT COMPT-AUTOPILOT MODE CTR PANEL LIGHTING MOD Open737-33-1084-R0 (ACTIVE) SBDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-33-1087 SB 02 RECOMMENDED A/C REPLACE ACTUATION PUSH ROD WITH NEW PUSH/PULL CABLE Rejected by Operator


SBPRR

737-33-1091 SB 00 RECOMMENDED A/C CONTROL CABIN LIGHTNING. Rejected by Operator737-33-1091 SB

737-33-1093 SB 00 RECOMMENDED A/C PASSENGER SIGNS - PASSENGER SERVICE UNIT (PSU) REPLACEMENT Not Applicable by Serial Number737-33-1093-R0 (ACTIVE) SB

737-33-1097 SB 00 RECOMMENDED A/C FLIGHT COMPARTMENT/BRIGHT/DIM CONTROL FOR THE EFIS CTR PANEL Not Applicable by Serial Number737-33-1097-R0 (ACTIVE)PRODUCTION PRR34274-2R

SBPRR

737-33-1098 SB 00 RECOMMENDED A/C REPLACEMENT OF THE MISCELLANEOUS SWITCHING MODULE FOR AIRST. Rejected by Operator737-33-1098-R0 (ACTIVE)737-52-1091 (REF)737-52-1114 (REF)

SBSBSB

737-33-1109 SB 00 RECOMMENDED A/C INSTALLATION OF THE RELAYS FOR THE CARGO COMPARTMENTS LIGHTS Not Applicable737-33-1098 (REF)737-33-1109-R0 (ACTIVE)737-52-1114 (REF)

SBSBSB

737-33-1119 SB 01 RECOMMENDED A/C EMERGENCY LIGHTING/POWER SUPPLY/BATTERY PACK/INVERTER RELOC. Rejected by Operator737-33-1119-R1 (ACTIVE)737-SRP-33-0031 (REF)PRODUCTION LINEPRR35005-226R

SB

SRP

PRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-33-1129 SB 00 MANDATORY A/C *AD* TAXI LIGHT ASSEMBLY - INSPECTION & REPLACEMENT Not Applicable / Special Text: This

aircraft is Not Applicable due toVAR#.

This document is applicable to LN# 16-2374.

AMOC in SB:This service bulletin has been approved by the FAA. In addition, theManager of the FAA SeattleAircraft Certification Office approves the action (i.e. inspection ormodification) defined in this servicebulletin as an alternative method of compliance to the requirementsof paragraph (c) of AD2000-08-17. All provisions of AD 2000-08-17 that are not specificallyreferenced in the abovesentence remain fully applicable and must be complied with.2000-08-17 (ACTIVE)50-0128-33-0005 (REF)50-0199-33-0004 (REF)737-33-1129-R0 (ACTIVE)737-SL-33-016 (REF)737-SRP-33-0038 (REF)

ADSBSBSBSLSRP






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-33-1132 SB 00 MANDATORY A/C LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION Superseded (Closed 17.Mar.2005)

2006-15-18 (ACTIVE)737-33-1132-R0 (REF)737-33-1132-R1 (REF)737-33-1132-R2 (REF)737-33-1132-R3 (ACTIVE)PRODUCTION LINEMRR3331-1487SSBB 737-33-1132 (MOD-TASK)

ADSBSBSBSBPRRTA








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-33-1132 SB 02 MANDATORY A/C LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION Superseded (See prev. Docstatus)


ADSBSBSBSBPRRTA

This Document SUPERSEDES 737-33-1132/SB Rev.01This Document has been SUPERSEDED BY 737-33-1132/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150147 ITEM: 1

737-33-1132 SB 03 MANDATORY A/C LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION See prev. Docstatus2006-15-18 (ACTIVE)737-33-1132-R0 (REF)737-33-1132-R1 (REF)737-33-1132-R2 (REF)737-33-1132-R3 (ACTIVE)PRODUCTION LINEMRR3331-1487SSBB 737-33-1132 (MOD-TASK)

ADSBSBSBSBPRRTA

This Document SUPERSEDES 737-33-1132/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150147 ITEM: 1





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-33-1132 SB 01 MANDATORY A/C LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION Superseded (See prev. Docstatus)


ADSBSBSBSBPRRTA




737-33-1149 SB 00 RECOMMENDED A/C LIGHTS - STROBE POSITION LIGHTS - LIGHTNING PROTECTION OF THE TAIL STROBELIGHT AND WIRE BUNDLE


737-33A1140 SB 00 MANDATORY A/C *AD* OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRES Superseded (Cancelled)2009-14-04 (ACTIVE)2009-14-04-1 (ACTIVE, PARA F)2009-14-04-2 (REF, PARA G)737-33A1140-R0 (ACTIVE)PRODUCTION LINEMRR3335-1627S

AD

AD

AD

SB

PRR

This Document has been SUPERSEDED BY 737-33A1140/SB Rev.01Reason for this StatusSB 737-28-1241 PERFORMED, SB COVERS REQ. OF SB 737-33A1140





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-33A1140 SB 01 MANDATORY A/C *AD* OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRES Cancelled

2009-14-04 (ACTIVE)2009-14-04-1 (ACTIVE, PARA F)2009-14-04-2 (REF, PARA G)737-33A1140-R0 (ACTIVE)PRODUCTION LINEMRR3335-1627S

AD

AD

AD

SB

PRR

This Document SUPERSEDES 737-33A1140/SB Rev.00Reason for this StatusSB 737-28-1241 PERFORMED, SB COVERS REQ. OF SB 737-33A1140

737-34-1221 SB 00 RECOMMENDED A/C FLIGHT MANAGEMENT COMPUTER REPLACEMENT Not Applicable by Serial Number737-34-1221-R0PRODUCTION PRR34298

SBPRR

737-34-1241 SB NOTE

RECOMMENDED A/C GROUND PROXIMITY WARNING COMPUTER REPLACEMENT Ex Factory

737-34-1241-R0 (ACTIVE)PRODUCTION PRR34607-1

SBPRR

Reason for this StatusPRODUCTION PRR PRR34607-1

737-34-1244 SB NOTE

RECOMMENDED A/C ATTITUDE AND DIRECTION STANDBY Closed 24.Feb.1992








24.Oct.2014/411


TERECOMMENDED A/C INERTIAL REFERENCE SYSTEM Not Applicable by Serial Number

737-34-1253 SB

737-34-1263 SB NOTE

RECOMMENDED A/C FLIGHT MANAGEMENT COMPUTER REPLACEMENT Closed 19.Apr.1991




737-34-1267 SB NOTE

RECOMMENDED A/C NAVIGATION. ATTITUDE & DIRECTION Rejected by Operator

737-34-1267 SB

737-34-1274 SB NOTE

RECOMMENDED A/C NAVIGATION. AUXILIARY STATIC SYSTEM. Rejected by Operator

737-34-1274 SB

737-34-1343 SB NOTE

MANDATORY A/C ATC TRANSPONDER REPLACEMENT - MODIFICATION OF TPR720 Rejected by Operator

1992-11-09 (ACTIVE)6206-10-34-11 (GABLES)737-34-1343-R1 (ACTIVE)EMO 3-34-044 (TRANSAVIA)TRP-72-34-14 (COLLINS)TRP-720-34-08 (COLLINS)

ADSBSBEOSBSB





24.Oct.2014/411


TERECOMMENDED A/C FLIGHT MANEGMENT COMPUTER SYSTEM Rejected by Operator

737-34-1366 SB

737-34-1377 SB NOTE

RECOMMENDED A/C EFIS SYMBOL GENERATOR-CHANGES TO WIRING TO Rejected by Operator

737-34-1377 SB

737-34-1384 SB NOTE

RECOMMENDED A/C FMC SYSTEM-OPERATIONAL SOFTWARE PROGRAM Rejected by Operator

737-34-1384 SB

737-34-1388 SB NOTE

RECOMMENDED A/C UPDATED AND EXTENDED MAGNETIC VARIATION TABLE ACTIVATION Not Applicable by Serial Number

737-34-1388 SB

737-34-1398 SB NOTE

RECOMMENDED A/C FMC-OPERATIONAL SOFTWARE PROGRAM REPLACEMENT Rejected by Operator

737-34-1398 SB

737-34-1403 SB NOTE

RECOMMENDED A/C NAVIGATION-COLLISION AUDIOANCE-TRAFFIC Rejected by Operator

737-34-1403 SB

737-34-1415 SB NOTE

RECOMMENDED A/C FMC SYSTEM-OPERATIONAL SOFTWARE PROGRAM Rejected by Operator

737-34-1415 SB





24.Oct.2014/411


TERECOMMENDED A/C INERTIAL REFERENCE SYSTEM - UPDATED MAGNETIC VARIATION TABLE Not Applicable by Serial Number

737-34-1439-R0 (REF)737-34-1439-R1 (ACTIVE)

SBSB

737-34-1444 SB 00 RECOMMENDED A/C FMC-OPERATIONAL SOFTWARE PROGRAM Rejected by Operator737-34-1444 SB

737-34-1449 SB NOTE

RECOMMENDED A/C REMOVAL OF THE STATIC SOURCE SELECTOR VALUES/SEP PITOT Not Applicable by Serial Number

737-34-1449-R1 (ACTIVE)737-34A1459 (REF)PRODUCTION MC3410MK3003

SBSBPRR

737-34-1493 SB NOTE

RECOMMENDED A/C NAVIGATION-TRAFFIC ALERT AND COLLISION Rejected by Operator

737-34-1493 SB

737-34-1512 SB NOTE

RECOMMENDED A/C TCAS II SYSTEM INSTALLATION Rejected by Operator

737-34-1512 SB

737-34-1516 SB 00 RECOMMENDED A/C FLIGHT MANGAGEMENT COMPUTER SYSTEM - SOFTWARE VERSION U10.2A Not Applicable737-34-1516 (ACTIVE)PRODUCTION MC 3461MK3808

SBPRR

737-34-1547 SB NOTE

RECOMMENDED A/C REPLACEMENT OF THE ALLIEDSIGNAL TCAS COMPUTER Not Applicable by Serial Number

737-34-1547-R4 (ACTIVE)PRODUCTION MC3445MK3478

SBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-34-1554 SB 00 OPTIONAL A/C FMC - 4 MCU FLIGHT MANAGEMENT COMPUTER INSTALLATION Closed 16.Mar.2005

PRR35418-R PRR OOPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

16.Mar.2005KKM 150385ITEM: 1

737-34-1558 SB NOTE

RECOMMENDED A/C REPLACEMENT OF THE ROCKWELL/ COLLINS TCAS COMPUTER Not Applicable by Serial Number

737-34-1558-R3 (ACTIVE) SB

737-34-1570 SB NOTE

OPTIONAL A/C ACTIVATION OF THE 1995 UPDATED MAGNETIC VARIATION TABLE Closed 14.Mar.2008

737-34-1570-R1 (ACTIVE)737-34-1570-RO (REF)MC3421MK3037 (MASTERCHANGE)SBB 737-34-1570 (MOD-TASK)

SB

SB

DOCR

TA




737-34-1577 SB 00 RECOMMENDED A/C NAVIGATION-FLIGHT MANAGEMENT Not Applicable by Serial Number737-34-1577 SB

737-34-1578 SB NOTE

RECOMMENDED A/C NAVIGATION-TRAFFIC ALERT AND COLLISION Rejected by Operator

737-34-1578 SB





24.Oct.2014/411


TEOPTIONAL A/C FLIGHT MANAGEMENT COMP SYSTEM - DUAL INSTALLATION Not Applicable by Serial Number

IN 01: N/A to NAS as SB was rejected.IN 02: N/A to NAS as SB was rejected.737-34-1593 IN 01737-34-1593 IN 02737-34-1593-R0 (ACTIVE)PRODUCTION PRR35418-R

SBSBSBPRR

IN01IN02

737-34-1609 SB NOTE

RECOMMENDED A/C FLIGHT MANAGEMENT COMPUTER SYSTEM-SOFTWARE VER V10.3 UPDATE Rejected by Operator


SBPRR

737-34-1649 SB NOTE

OPTIONAL A/C FMC - UPDATE THE FMC SOFTWARE TO VERSION 10.5 Not Applicable

737-34-1649-R0 (ACTIVE)PRODUCTION PRR35434-RSBB 737-34-1649 (MOD-TASK)

SBPRRTA

Reason for this StatusSBB 737-34-1950 VERSION 10.7

737-34-1665 SB 00 RECOMMENDED A/C FMC SYSTEM - UPDATE THE FMC SOFTWARE TO VERSION 10.4A Rejected by Operator737-34-1665-RO (ACTIVE)PRODUCTION PRR35437-R

SBPRR





24.Oct.2014/411


TERECOMMENDED A/C FMC: UPDATE FLIGHT MANAGEMENT COMPUTER OPERATING SOFTWARE Not Applicable by Serial Number

737-34-1683-R1 (ACTIVE)MC3461MK3917 (MASTERCHANGE)SBB 737-34-1683 (MOD-TASK)

SB

DOCR

TA

737-34-1710 SB 01 RECOMMENDED A/C NAVIGATION - PITOT STATIC PROBE BOND AND FLEXIBLE HOSE INSP. Superseded (Superseded)737-34-1710-R2737-SL-34-171 (REF)

SBSL


737-34-1710 SB 02 RECOMMENDED A/C NAVIGATION - PITOT STATIC PROBE BOND AND FLEXIBLE HOSE INSP. Closed 05.Jul.2011 W/O:205155737-34-1710-R2737-SL-34-171 (REF)

SBSL

This Document SUPERSEDES 737-34-1710/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Jul.2011 64534:00/H 37798/C 205155, N/A Was due at: 31.Aug.2011 PerfRev.:'02'

737-34-1710 SB 00 RECOMMENDED A/C NAVIGATION - PITOT STATIC PROBE BOND AND FLEXIBLE HOSE INSP. Superseded (Superseded)737-34-1710-R2737-SL-34-171 (REF)

SBSL






24.Oct.2014/411


TEOPTIONAL A/C ACTIVATION OF UPDATED AND EXTENDED MAGNETIC VARIATION TABLE Closed 14.Mar.2008

737-34-1796-R0 (ACTIVE)MC3421MK3112 (MASTERCHANGE)SBB 737-34-1796 (MOD-TASK)

SB

DOCR

TA




737-34-1812 SB NOTE

RECOMMENDED A/C NAVIGATION-INERTIAL REFERENCE SYSTEM Cancelled (Cancelled)

Rejected. Ref Honeywell Technical Newsletter M23-3341-029 rev.2, thedifference between 1995 and 2005 magvar is less than 2 degrees inNAS` area of operation. Furthermore LHT has quoted TAT of 30 days toupgrade IRUs to 2005 magvar, hence mod program cannot be completedbefore all CLs are phased out.

26.Nov.2012:SB cancelled and reversed for KKD by TO 738-34-009.737-34-1812 SBThis Document has been CANCELLED BY 733-34-009/TO Rev.00

737-34-1836 SB 01 RECOMMENDED A/C INERTIAL REFERENCE SYSTEM-1995 MAGNETIC VARIATION TABLE ACT. Not Applicable by Serial Number737-SL-34-114 (REF)737-SL-34-177 (REF)737-SRP-34-0113 (REF)

SLSLSRP





24.Oct.2014/411


TEMANDATORY A/C FMC: CHANGE THE OPERATIONAL SOFTWARE TO VERSION 10.6 Closed 07.Aug.2006

34-62-00/201 (REF)34-62-01/201 (REF)737-34-1879-R0 (ACTIVE)737-SL-34-181 (REF)MRR3344-1599 (REF)SBB 737-34-1879 (MOD-TASK)

AMMAMMSBSLPRRTA




737-34-1950 SB NOTE

MANDATORY A/C FMC: CHANGE THE OPERATIONAL SOFTWARE TO VERSION 10.7 Closed 06.Sep.2007

34-62-01/201 (REF)737-34-1950 IN 01 (REF)737-34-1950-R1 (ACTIVE)SBB 737-34-1950 (MOD-TASK)

AMMDOCRSBTA








24.Oct.2014/411


TERECOMMENDED A/C UPDATE AND RUNWAY OFFSET IN METERS ON TAKEOFF/GO-AROUND ACT. Not Applicable by Serial Number

737-34-2034-R0 (ACTIVE)MC3461MK3917 MC3461MK3AFRSBB 737-34-2034 (MOD-TASK)

SBDOCRTA

737-34-2193 SB NOTE

OPTIONAL A/C FMC SYSTEM - INSTALLATION OF ALTERNATE DESTINATION FEATURE Not Applicable

737-34-2193 R1MC3461MK3AJY

SBCR

737-34-2215 SB NOTE

OPTIONAL A/C NAVIGATION - FLIGHT MANAGEMENT COMPUTER SYSTEM - FLIGHT MANA Not Applicable by Serial Number

737-34-2215 R00 SB

737-34A1208 SB 01 RECOMMENDED A/C LOCALIZER ANTENNA - CABLE REPLACEMENT AND ATTENUATOR INSTALLATION Superseded (Not Applicable bySerial Number)


737-34A1208 SB 02 RECOMMENDED A/C LOCALIZER ANTENNA - CABLE REPLACEMENT AND ATTENUATOR INSTALLATION Not Applicable by Serial NumberThis Document SUPERSEDES 737-34A1208/SB Rev.01

737-34A1208 SB 00 RECOMMENDED A/C LOCALIZER ANTENNA - CABLE REPLACEMENT AND ATTENUATOR INSTALLATION Superseded (Not Applicable bySerial Number)


737-34A1459 SB NOTE

RECOMMENDED A/C NAVIGATION-PITOT STATIC SYSTEM Rejected by Operator

737-34A1459 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-34A1821 SB 00 MANDATORY A/C *AD* FMC: CHANGE THE OPERATIONAL SOFTWARE TO VERSION 10,5A Closed 13.Aug.2005

2005-19-19 (ACTIVE)34-62-00/201 (REF)34-62-01/201 (REF)737-34A1821-R0 (ACTIVE)737-SL-34-179 (REF)SBB 737-34A1821 (MOD TASK)

ADAMMAMMSBSLTA




737-34A2122 SB 00 RECOMMENDED A/C FMC OPERATIONAL PROGRAM SOFTWARE U10.8 INSTALLATION Superseded (Superseded)Mod suspended, ref. IN 01. Was never installed on NAS a/c.Superseeded by 34A2217 (U10.8A).737-34A2122 IN-01737-SL-34-193737-SRP-34-0116

SBSLSRP

000000


737-34A2217 SB 00 RECOMMENDED A/C NAVIGATION - FMCS - FMC OPS U10.8A SOFTWARE INSTALLATION Closed 14.Dec.2010 W/O:130351737-34A2217 R00 SBThis Document SUPERSEDES 737-34A2122/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Dec.2010 63101:00/H 36681/C 130351, N/A Was due at: 15.Jun.2012 PerfRev.:'NOTE'

737-35-1033 SB 00 MANDATORY A/C OXYGEN SYSTEMS/CREW OXYGEN SYSTEM TUBE INSP/REPLACEMENT Not Applicable by Serial Number1990-25-12 AD 00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35-1049 SB 01 MANDATORY A/C PASSENGER & ATTENDANT OXYGEN MASK LANDYARD REPLACEMENT Closed 17.Mar.2005

This document is applicable to LN# 1-2984.2000-15-16737-35-1049737-35-1049737-35-1049 IN-02737-SRP-35-0010B/E AEROSPACE 3500-98-07B/E AEROSPACE 3500-98-07 A01

ADSBSBSBSRPSBSB

00000100000001




737-35-1049 SB 00 MANDATORY A/C PASSENGER & ATTENDANT OXYGEN MASK LANDYARD REPLACEMENT Superseded (Superseded)2000-15-16 (ACTIVE)737-35-1049 IN 02 (REF)737-35-1049 R1 (ACTIVE)737-35-1049-RO (REF)737-SRP-35-0010 (REF)B/E AEROSPACE 3500-98-07B/E AEROSPACE 3500-98-07 A01SBB 737-35-1049 (MOD-TASK)SBB 737-35-1049P1 (MOD-TASK)

ADSBSBSBSRPSBSBTATA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35-1076 SB 00 MANDATORY A/C OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION Repetitive

AMOC letter gives permission to use one of two options to comply withAD. NAS will use "Option 2" of the AMOC. NAS performs repetitivinspections of the AC oxygen generators and uses the improved AMMreferences for Removal/Installation.2001-10-14737-35-1076 IN-01737-35-1076 IN-02737-35-1076-01737-35-1076-02

ADSBSBEOEO

0000000000

Perform WITHIN 90/D (effective from 08.Jun.2001)737-35-1076/SB Rev.00 OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION Repetitive> 737-35-1076-01/EO* Rev.00 OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION See prev. Docstatus

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Aug.2001 45757:00/H 23244/C PerfRev.:'NOTE'Reason for this StatusDEL DOCS

> 737-35-1076-02/EO* Rev.00 OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

31.Jul.2015Perform initially within (effective from08.Jun.2001) (F) 540/D / Interval(F):540/D

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks06.Feb.2014 71572:00/H 43151/C 489224, N/A Was due at: 19.Apr.2014 PerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35-1078 SB 00 RECOMMENDED A/C PASSENGER OXYGEN-OXYGEN GENERATOR INSPECTION Rejected by Operator / Special Text:

Rejected by previous operator117003-14-35-3737-35-1076737-SRP-35-0020

SBSBSRP

000000

Reason for this StatusREJECTED BY PREVIOUS OPERATOR

737-35-1099 SB 01 MANDATORY A/C OXYGEN MASK ASSEMBLY INSPECTION AND MODIFICATION Closed 28.Oct.2012 W/O:2736342008-06-24 (SUPERSEEDED)2010-14-06737-35-1099 IN-01737-SRP-35-0035AMM 25-23-61, 35-00-00, 35-22-11AMM 35-22-31B/E AEROSPACE 174080-35-01

ADADSBSRPAMMAMMSB

00000000000001

This Document SUPERSEDES 737-35-1099/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Oct.2012 68139:00/H 40570/C 273634, N/A Was due at: 22.Apr.2013 PerfRev.:'01'

737-35-1099 SB 00 MANDATORY A/C OXYGEN MASK ASSEMBLY INSPECTION AND MODIFICATION Superseded (Superseded)2008-06-242010-14-06737-35-1099 IN-01B/E AEROSPACE 174080-35-01

ADADSBSB

00000000


737-35A1029 SB 01 MANDATORY A/C O2 MASK LANYARD RINGS AND O2 GENERATORS, REPLACEMENT OF Superseded (Not Applicable)This Document has been SUPERSEDED BY 737-35A1029/SB Rev.03





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35A1029 SB 03 MANDATORY A/C O2 MASK LANYARD RINGS AND O2 GENERATORS, REPLACEMENT OF Not Applicable by Serial Number

1989-26-06 AD 01This Document SUPERSEDES 737-35A1029/SB Rev.00This Document SUPERSEDES 737-35A1029/SB Rev.01This Document SUPERSEDES 737-35A1029/SB Rev.02



737-35A1031 SB 00 RECOMMENDED A/C OXYGEN.PASSENGER. INSP/REPLACEMENT OF OXYGEN BOX OR MODULE DOORLATCH ACTUATORS


Rejected by previous operator.737-35A1031 SB

737-35A1037 SB 00 MANDATORY A/C PAX OXYGEN SYSTEM - TEST STOP PLUNGERS MODIFICATION Closed 27.Mar.19921992-25-04737-35A1037

ADSB

0001


27.Mar.1992SUNEXPRESS EO007856

737-35A1038 SB 00 MANDATORY A/C PAX OXYGEN SYSTEM - OXYGEN BOX ASSEMBLY MODIFICATION Not Applicable by Serial Number1992-25-04 AD 00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35A1053 SB 00 MANDATORY A/C CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPL. Superseded (Cancelled)

PRR 38275-1 PRR 00This Document has been SUPERSEDED BY 737-35A1053/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35A1053 SB 02 MANDATORY A/C OXYGEN - CREW OXYGEN - CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE

REPLACEMENTNot Applicable / Special Text: ThisAircraft is not applicable due to PRR38275-1

This document is applicable to All 737CL.

All NSB aircraft are Group 1 AC.

AMOC in SB:In addition, the Manager of the FAA Seattle Aircraft CertificationOffice approves completing the accomplishment instructions of thisservice bulletin, 737-35A1053, Revision 2, as an AMOC to completingthe accomplishment instructions of service bulletin 737-35A1053,Revision 1, dated June 1, 2000, required by paragraph (g) of AD2010-16-06 , for applicable Boeing model 737-300, -400, -500 seriesairplanes.PRR 38275-1 PRR 00This Document SUPERSEDES 737-35A1053/SB Rev.01Perform BEFORE 10.Sep.2013

737-35A1053/SB Rev.02 OXYGEN - CREW OXYGEN - CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSEREPLACEMENT

Not Applicable / Special Text: ThisAircraft is not applicable due to PRR38275-1

This Document SUPERSEDES 737-35A1053/SB Rev.01> 737-35A1053-01/EO* Rev.00 OXYGEN - CREW OXYGEN - CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE

REPLACEMENTNot Applicable / Special Text: ThisAircraft is not applicable due to PRR38275-1

Reason for this StatusNA DUE TO HAVING PERFORMED REV 00 OR 01 OF SB, GROUP 1 CONFIG 2.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35A1053 SB 01 MANDATORY A/C CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPL. Superseded (Closed 18.Jan.2001)

This document is applicable to All 737CL.PRR 38275-1 PRR 00This Document SUPERSEDES 737-35A1053/SB Rev.00This Document has been SUPERSEDED BY 737-35A1053/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-35A1121 SB 00 RECOMMENDED COMP OXYGEN - CREW OXYGEN SYSTEM - CREW OXYGEN MASK STOWAGE BOX U Superseded (Not Applicable bySerial Number / Special Text: ThisAircraft is not applicable due to PRR38275-1)

2010-NM-094-ADMXP1/4-35-175, REV. 0.

NPRMSB

0000

This Document has been SUPERSEDED BY 737-35A1121/SB Rev.01Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

737-35A1124 SB 00 RECOMMENDED COMP OXYGEN - CREW AND PASSENGER O2 SYS. - INSP. OF CYLINDER Not Applicable by Serial Number6084-34-35-01 (AVOX SB, ACTIV) SBAffected Rotables (Part No/Serial No/Position) Status801307-00 / 599240 Pos=#1 (KKM) Not Applicable





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-35A1126 SB 00 RECOMMENDED COMP OXYGEN - CREW AND PASSENGER O2 SYS. - INSP. OF CYLINDER Not Applicable by Serial Number

6084-34-35-01 (AVOX SB, ACTIV)737-35A1126 R00 (ACTIVE)SBB 737-35A1126 (INSP TASK)

SBSBTA

Affected Rotables (Part No/Serial No/Position) Status801307-00 / 599240 Pos=#1 (KKM) Not Applicable

737-36-1014 SB 00 RECOMMENDED A/C PNEUMATIC-DISTRIBUTION-PRESSURE REGULATING Rejected by Operator737-36-1014 SB

737-36-1018 SB 00 RECOMMENDED A/C BLEED AIR REGULATOR SENSE Closed 08.Aug.1995737-36-1018 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Aug.1995PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-38-1024 SB 00 OPTIONAL A/C ENGINE BLEED AIR POTABLE WATER TANK PRESS SYST INSTALLATION Not Applicable by Serial NumberThis mod is only applicable to TAV AC, variable no: PP801-PP086.737-38-1024-R0 (ACTIVE)PRODUCTION PRR34395-01SBB 737-38-1024 (MOD-TASK)

SBPRRTA

737-38-1026 SB 02 MANDATORY A/C FORWARD LAVATORY WASTE SYSTEM MODIFICATION Not Applicable by Serial NumberRejected by previous operator.1989-11-03 (SUPERSEDED)2004-06-18 (ACTIVE)737-38-1026-R2 (ACTIVE)PRODUCTION PRR33890-68

ADADSBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38-1027 SB 01 MANDATORY A/C TOILET SYSTEM - AFT LAVATORY SERVICE PANEL MODIFICATION Rejected by Operator

Rejected by previous operator.PRODUCTION PRR33890-68 PRR 00Reason for this StatusAUTO ASSIGNED

737-38-1028 SB 00 RECOMMENDED A/C WATER DISPOSAL.TOILET SYSTEM Rejected by Operator737-38-1028 SB

737-38-1029 SB 01 MANDATORY A/C *AD* PRESS/RELIEF VALVE IN THE POTABLE WATER PNEU/PRESS/SYST Not ApplicableThis modification is applicable for Specific Var#. The Other VAR#are Not Applicable Per PRR34978.2003-26-08 XA (ACTIVE)737-38-1029-R0 (REF)737-38-1029-R1 (ACTIVE)PRODUCTION PRR34978

ADSBSBPRR


737-38-1029 SB 00 MANDATORY A/C *AD* PRESS/RELIEF VALVE IN THE POTABLE WATER PNEU/PRESS/SYST Superseded (Not Applicable bySerial Number)

This modification is applicable for Specific Var#. The Other VAR#are Not Applicable Per PRR34978.2003-26-08 XA (ACTIVE)737-38-1029-R0 (REF)737-38-1029-R1 (ACTIVE)PRODUCTION PRR34978

ADSBSBPRR


737-38-1030 SB 00 RECOMMENDED A/C WATER/WASTE-PORTABLE WATER-BLEED Rejected by Operator737-38-1030 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38-1032 SB 00 RECOMMENDED A/C WATER/WASTE-WASTE WATER SYSTEM-MODIFICATION OF WASTE SYS. Not Applicable by Serial Number

737-38-1032-R0PRODUCTION PRR33890-90R

SBPRR

737-38-1037 SB 00 RECOMMENDED A/C TOILET SYS- REPL. THE HOSE ASSEMBLY OF THE GROUND FLUSH LINE Rejected by OperatorNAS has no reliability issues with this area of the system. NAS doesnot incorperate this SB.Reason for this StatusAUTO ASSIGNED

737-38-1041 SB 00 RECOMMENDED A/C THERMAL ISOLATION OF GREY Closed 03.Apr.2001737-38-1041 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-38-1042 SB 02 RECOMMENDED A/C WATER/WASTE - WASTE WATER SYSTEM - DOOR SILL DRAINAGE MODIFICATION -FORWARD AND AFT SILL DRAINS


This Document is applicable to LN# 2800 - 2955 and 2057.Rejected by previous operator.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38-1043WP1 SB 02 MANDATORY A/C *AD* POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALL See prev. Docstatus

WP1 covers the AD 1999-01-16 requirement detailed in §A.1999-01-16 (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP1 (MOD-TASK)

ADSBSBSBPRRTA

This Document SUPERSEDES 737-38-1043WP1/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Jul.1998 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.

737-38-1043WP1 SB 01 MANDATORY A/C *AD* POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALL Superseded (See prev. Docstatus)WP1 covers the AD 1999-01-16 requirement detailed in §A.1999-01-16 (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP1 (MOD-TASK)

ADSBSBSBPRRTA

This Document SUPERSEDES 737-38-1043WP1/SB Rev.00This Document has been SUPERSEDED BY 737-38-1043WP1/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Jul.1998 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38-1043WP1 SB 00 MANDATORY A/C *AD* POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALL Superseded (Closed 28.Jul.1998)

WP1 covers the AD 1999-01-16 requirement detailed in §A.1999-01-16 (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP1 (MOD-TASK)

ADSBSBSBPRRTA

This Document has been SUPERSEDED BY 737-38-1043WP1/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-38-1043WP2 SB 01 MANDATORY A/C *AD* POTABLE WATER DRAINAGE - VALVE INSTALLATION Superseded (Closed 31.Jan.2002)WP2 covers the AD 1999-01-16 requirement detailed in §B.1999-01-16 (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP2 (MOD-TASK)

ADSBSBSBPRRTA

This Document SUPERSEDES 737-38-1043WP2/SB Rev.00This Document has been SUPERSEDED BY 737-38-1043WP2/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Jan.2002PerfRev.:'NOTE' / Reason: DELIVERYDOC.






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38-1043WP2 SB 02 MANDATORY A/C *AD* POTABLE WATER DRAINAGE - VALVE INSTALLATION See prev. Docstatus

WP2 covers the AD 1999-01-16 requirement detailed in §B.1999-01-16 (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP2 (MOD-TASK)

ADSBSBSBPRRTA

This Document SUPERSEDES 737-38-1043WP2/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks31.Jan.2002 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.

737-38-1043WP2 SB 00 MANDATORY A/C *AD* POTABLE WATER DRAINAGE - VALVE INSTALLATION Superseded (Superseded)WP2 covers the AD 1999-01-16 requirement detailed in §B.1999-01-16 (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP2 (MOD-TASK)

ADSBSBSBPRRTA

This Document has been SUPERSEDED BY 737-38-1043WP2/SB Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38-1045 SB 01 OPTIONAL A/C INSTALL LAVATORY A OVERFILL SENSOR/SHUTOFF VALVE Rejected by Operator

NAS does not have any safety or reliability issues with this part.NAS has rejected this SB.737-38-1045-R1 (ACTIVE)PRODUCTION PRR35402-1R

SBPRR


737-38-1056 SB 00 OPTIONAL A/C WATERSYSTEM TANK 50/60 USG TO 40 USG, CHANGE. Not Applicable737-38-1056-R0 (ACTIVE)MC3811MK3053 (MASTERCHANGE)

SB

DOCR

Reason for this StatusNA PER MSN, REF SB

737-38A1038 SB 02 MANDATORY A/C *AD* PRESSURE RELIEF VALVE REPLACEMENT Not Applicable by Serial NumberThis modification is applicable for LN# 2524-2696. The Other LN#are Not Applicable Per PRR35005-98.2003-26-08 XE & XF737-38A1038-R0 (REF)737-38A1038-R1 (REF)737-38A1038-R2 (ACTIVE)PRODUCTION PRR35005-98

ADSBSBSBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38A1047 SB 02 MANDATORY A/C *AD* PRESSURE RELIEF VALVE REPLACM. ON WATER TANK PRESS SYST Closed 21.Dec.2000

This modification is applicable for LN# 1629-2478.2003-26-08 XA,B,C (ACTIVE)737-38A1047-R0 (REF)737-38A1047-R1 (REF)737-38A1047-R2 (ACTIVE)737-SRP-38-0042 (REF)

ADSBSBSBSRP




737-38A1054 SB 01 MANDATORY A/C WATER/WASTE - PASSENGER WATER SYSTEM, LAVATORY A STRAIGHT TO 90 DEGREEHOSE ASSEMBLY REPLACEMENT

Closed 08.Nov.2012 W/O:273644

SB Item F Approval:This service bulletin has been approved by the FAA. In addition, theManager of the FAA Seattle Aircraft Certification Office approves theaction (i.e. inspection or modification) defined in this servicebulletin as an alternative method of compliance to the requirementsof paragraph (f) of AD 2008-17-13. All provisions of AD 2008-17-13that are not specifically referenced in the above statement remainfully applicable and must be complied with.737-38A1054 AMOC 01737-38A1054 IN-02

AMOCSB

LAST00

This Document SUPERSEDES 737-38A1054/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Nov.2012 68139:00/H 40570/C 273644, N/A Was due at: 04.Nov.2013 PerfRev.:'01'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-38A1054 SB 00 MANDATORY A/C *AD* LAVATORY A STREIGHT TO 90DEG HOSE ASSY, REPLACEMENT OF Superseded (Cancelled)

SB Item F Approval:This service bulletin has been approved by the FAA. In addition, theManager of the FAA Seattle Aircraft Certification Office approves theaction (i.e. inspection or modification) defined in this servicebulletin as an alternative method of compliance to the requirementsof paragraph (f) of AD 2008-17-13. All provisions of AD 2008-17-13that are not specifically referenced in the above statement remainfully applicable and must be complied with.This Document has been SUPERSEDED BY 737-38A1054/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded

737-47-1005 SB 00 OPTIONAL A/C NITROGEN GENERATION SYSTEM - INSTALLATION OF WIRING AND THE NITROGENGENERATION SYSTEM COMPONENTS

Not Applicable

This service bulletin gives instructions for installation of thewiring and the Nitrogen Generation System (NGS) components. The NGSdecreases the oxygen content of the air mixture in the center fueltank to a specified level as it makes nitrogen enriched air (NEA).

This SB is not applicable to any NAS AC. Only for Boeing 737-400737-26A1082737-47-1004

SBSB

0300






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-47-1007 SB 00 MANDATORY A/C INERT GAS SYSTEM - INSTALLATION OF THE NITROGEN GENERATION SYSTEM

PROVISIONSRejected by Operator

Rejected due to too expensive and classic to be phased out.737-47-1007737-47-1008737-SL-51-042AMM 12,21,24,27,28,29,36,51,78NDT MANUAL PART 6. 51-00-00PRR 35453SOPM 20SRM 51-40-01,-02,-08,-09SWPM 20

SBSBSLAMMNDTBPRRSOPMSRMSWPM

000D000000

Reason for this StatusTOO EXPENSIVE AND CLASSIC TO BE PHASED-OUT

737-47-1008 SB 00 OPTIONAL A/C INERT GAS SYSTEM - INSTALLATION OF THE NITROGEN GENERATION SYSTEM Rejected by OperatorThis service bulletin gives instructions for installation of thewiring and the Nitrogen Generation System (NGS) components. The NGSdecreases the oxygen content of the air mixture in the center fueltank to a specified level as it makes nitrogen enriched air (NEA).

NAS has rejected the SB due to high cost, and pr. 06.03.2013, onlyN-registered AC (US) are applicable. The rquirement is 50 % of thefleet by december 2014 and 100 % of the fleet by 2017 ref737-FTD-47-06001.737-26A1082737-47-1007

SBSB

0300






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-49-1029 SB 00 RECOMMENDED A/C APU COMBUSTION CHAMBER DRAIN CUP MODIFICATION Not Applicable by Serial Number


SBPRR

737-49-1063 SB 03 OPTIONAL A/C INTERCHANGE OF APU MODEL GTCP85-129H, J OR K WITH APU MODEL Information OnlyThis SB provides information about APU interchangability only.737-49-1063-R3 (ACTIVE)PRR33890-41

SBPRR


737-49-1063 SB 00 OPTIONAL A/C INTERCHANGE OF APU MODEL GTCP85-129H, J OR K WITH APU MODEL Superseded (Information Only)This SB provides information about APU interchangability only.737-49-1063-R3 (ACTIVE)PRR33890-41

SBPRR



SBPRR



SBPRR






24.Oct.2014/411


TEOPTIONAL A/C APU - OPTIONAL APU STARTER MOTOR ASSEMBLY INSTALLATION Rejected by Operator

737-49-1066-R1 (ACTIVE) SB

737-49-1071 SB 01 MANDATORY A/C *AD* APU / EXHAUST GAS TEMPERATURE GAGE-WIRE MODIFICATION Not Applicable by Serial NumberThis mod is applicable for LN# 1001-1823. The following LN# are Notapplicable Per PRR34787.1990-23-12 (ACTIVE)737-49-1071-R0 (REF)737-49-1071-R1 (ACTIVE)PRODUCTION PRR34787

ADSBSBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-49-1073 SB 00 MANDATORY A/C *AD* AIRBORNE AUXILIARY POWER - FUEL DRAIN SYSTEM CHANGES Closed 05.May.1993

The changes specified in Garrett Service Bulletin GTC85-49-6547 orGTC85-49-6578 must be made on airplanes specifiied in this servicebulletin before or during the changes specified in this servicebulletin.

Federal Aviation Administration (FAA) Airworthiness Directives89-08-11 are 90-05-02 are related tothis service bulletin.1989-08-11 (SUPERSEDED)1990-05-02 (SUPERSEDED)1992-03-07 (ACTIVE)737-49-1073-R0 (ACTIVE)737-SL-49-014B (REF)GTCP85 49-6547-R0 (REF)GTCP85 49-6547-R1 (ACTIVE)GTCP85 49-6578-R0 (REF)GTCP85 49-6578-R1 (REF)GTCP85 49-6578-R2 (ACTIVE)PRODUCTION PRR33890-86SBB 737-49-1073 (MOD-TASK)

ADADADSBSLSBSBSBSBSBPRRTA








24.Oct.2014/411


TEOPTIONAL A/C APU REPLACEMENT OF APU BLEED AIR DUCT SHROUD AND INSULATION Rejected by Operator

737-49-1081-R1 (ACTIVE)737-49-1081-RO (REF)PRODUCTION PRR 35005-10

SBSBPRR

737-49-1099 SB NOTE

RECOMMENDED A/C APU REMOTE FIRE SWITCH WIRING CHANGE Rejected by Operator

737-49-1099-R0 (REF)737-49-1099-R1 (REF)737-49-1099-R2 (ACTIVE)

SBSBSB

737-49-1101 SB NOTE

RECOMMENDED A/C APU EXHAUST DUCT MUFFLER-LINER REPL. Closed 20.Mar.1996




737-49-1103 SB NOTE

RECOMMENDED A/C APU FULL AUTHORITY DIGITAL ELECTRONIC CONTROLLER (FADEC) Not Applicable by Serial Number

737-49-1103-R0 (ACTIVE)PRR35195

SBPRR

737-49-1104 SB NOTE

OPTIONAL A/C APU BLEED AIR SYSTEM - BLEED AIR VALVE WIRING CHANGE Rejected by Operator

737-49-1104-R1 (ACTIVE) SB





24.Oct.2014/411


TEOPTIONAL A/C APU ELECTRONIC SPEED SWITCH CASE GROUND INSTALLATION Open

737-49-1110-R1 (REF)737-49-1110-R2 (ACTIVE)737-49-1110-RO (REF)

SBSBSB


737-49-1112 SB NOTE

RECOMMENDED A/C APU - TORQUE BOX - AFT BULKHEAD INSTALLATION INSP. & MOD. Closed 18.Mar.2009

737-49-1112 IN 01 (REF)737-49-1112 IN 02 (REF)737-49-1112 IN 03 (REF)737-49-1112-R0 (REF)737-49-1112-R1 (ACTIVE)SBB 737-49-1112 (MOD-TASK)

SBSBSBSBSBTA




737-49-1115 SB NOTE

RECOMMENDED A/C APU AIR INLET DUCT REWORK TO FIRE PROOF CONFIGURATION Not Applicable by Serial Number

737-49-1115-R0 (ACTIVE)PRR35239 PRR35239-1R

SBPRR





24.Oct.2014/411


TEOPTIONAL A/C APU BLEED AIR SYSTEM - APU BLEED AIR VALVE SUPPRESSION DIODE Closed 22.May.2002

737-49-1129-R0 (REF)737-49-1129-R1 (REF)737-49-1129-R2 (REF)737-49-1129-R3 (ACTIVE)MRR3490-1399SBB 737-49-1129 (MOD-TASK)

SBSBSBSBPRRTA


22.May.2002PerfRev.:'NOTE' / Reason: DELIVERYDOCS.


737-49-1132 SB 00 OPTIONAL A/C AUXILARY POWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MOD Rejected by Operator737-49-1132-R0 (ACTIVE)SBB 737-49-1132 (MOD-TASK)

SBTA

737-49-1132 SB 01 OPTIONAL A/C AIRBORNE AUXILIARY POWER - AUXILIARY POWER UNIT AIR INLET - AUXILIARYPOWER UNIT FLAP AND VORTEX GENERATOR ASSEMBLY MODIFICATION

Open

No compliance time is given.24-22-0049-15-0049-15-2249-15-2351-10-0151-21-9951-40-02

AMMAMMAMMAMMSRMAMMSRM

LASTLASTLASTLASTLASTLASTLAST






24.Oct.2014/411


TERECOMMENDED A/C INTERNAL AIRFRAME DRAINAGE - CLEARANCE OF MOISTURE DRAINAGE Ex Factory

737-51-1013-R0 (REF)PRODUCTION PRR34545-1R

SBPRR

Reason for this StatusPRODUCTION PRR34545-1R

737-51-1015 SB NOTE

RECOMMENDED A/C FUSELAGE - VORTEX GENERATOR INSTALLATION Rejected by Operator

737-51-1015-R0 (REF)737-51-1015-R1 (ACTIVE)PRODUCTION PRR34997SBB 737-51-1015 (MOD-TASK)

SBSBPRRTA

737-52-1051 SB 03 RECOMMENDED A/C LOWER CARGO DOOR - LATCH SPRING RELOCATION AND REPLACEMENT Closed 04.May.1994737-52-1051 SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

04.May.1994PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-52-1061 SB NOTE

RECOMMENDED A/C FORWARD AIRSTAIR - IRSTAIR HANDRAIL SAFETY IMPROVEMENTS Rejected by Operator

737-52-1061-R0 (ACTIVE)PRODUCTION PRR35005-279RS

SBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1092 SB 00 OPTIONAL A/C FORWARD AIRSTAIR - TEMPORARY REMOVAL Superseded (Superseded)

1-733755945-252-61-10737-52-1092 (REF)737-52-1092 R1 (REF)737-52-1092 R2 (ACTIVE)

BMAMMSBSBSB


737-52-1092 SB 02 OPTIONAL A/C FORWARD AIRSTAIR - TEMPORARY REMOVAL Reopened1-733755945-252-61-10737-52-1092 (REF)737-52-1092 R1 (REF)737-52-1092 R2 (ACTIVE)

BMAMMSBSBSB

This Document SUPERSEDES 737-52-1092/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document25.Aug.2024 Perform initially before(F) 01.Oct.2009Reason for this StatusRef. NAS WO 557594, Re-inst of Airstair

737-52-1092 SB 01 OPTIONAL A/C FORWARD AIRSTAIR - TEMPORARY REMOVAL Superseded (Superseded)1-733755945-252-61-10737-52-1092 (REF)737-52-1092 R1 (REF)737-52-1092 R2 (ACTIVE)

BMAMMSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1094 SB 03 RECOMMENDED A/C DOORS - ENTRY AND GALLEY SERVICE DOOR TORQUE TUBE AND BEARING

REPLACEMENTSRejected by Operator

737-52-1094 SB

737-52-1096 SB 01 RECOMMENDED A/C FORWARD ENTRY AND GALLEY DOOR - HINGE CUTOUT MODIFICATION Ex Factory737-52-1096-R1 (REF)PRODUCTION PRR34424

SBPRR


737-52-1097 SB NOTE

MANDATORY A/C *AD* FWD GALLEY SERVICE DOOR - LWR GATE HINGE REPLACEMENT Not Applicable by Serial Number

1996-10-062004-225 (REF)737-52-1097-R2 (REF)PRODUCTION LINE PRR34473

ADADSBPRR

00

737-52-1100 SB NOTE

RECOMMENDED A/C DOORS-FORWARD CARGO-LOWER FORWARD AND Rejected by Operator

737-52-1100 SB

737-52-1109 SB NOTE

RECOMMENDED A/C FORWARD AND AFT CARGO DOOR COUNTERBALANCE SYSTEM PULLEY SUPP Rejected by Operator


SBPRR

737-52-1112 SB NOTE

RECOMMENDED A/C DOORS-EQUIPMENT ACCESS DOOR Rejected by Operator

737-52-1112 SB





24.Oct.2014/411


TERECOMMENDED A/C DOORS-DOOR WARNING SYSTEM Rejected by Operator

737-52-1114 SB

737-52-1119 SB NOTE

RECOMMENDED A/C FORWARD AND AFT CARGO DOOR - COUNTERBALANCE SYSTEM REPLACEM. Open

737-52-1109 (REF)737-52-1119-R1PRODUCTION PRR35005-11

SBSBPRR


737-52-1119WP1 SB NOTE

RECOMMENDED A/C COUNTERBALANCE SYSTEM REPLACEMENT, FWD CARGO DOOR Closed 03.May.1994

737-52-1119737-52-1119 IN 03737-52-1119 IN 04737-52-1119 IN 05737-52-1119 NSC02737-52-1119 R1

SBSBSBSBSBSB








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1119WP2 SB NO

TERECOMMENDED A/C COUNTERBALANCE SYSTEM REPLACEMENT, AFT CARGO DOOR Closed 07.Feb.2008

737-52-1119737-52-1119 IN 03737-52-1119 IN 04737-52-1119 IN 05737-52-1119 NSC02737-52-1119 R1

SBSBSBSBSBSB




737-52-1119WP3 SB NOTE

RECOMMENDED A/C COUNTERBALANCE SYSTEM REWORK, FWD & AFT CARGO DOOR Closed 07.Feb.2008

737-52-1119737-52-1119 IN 03737-52-1119 IN 04737-52-1119 IN 05737-52-1119 NSC02737-52-1119 R1

SBSBSBSBSBSB








24.Oct.2014/411


TERECOMMENDED A/C REPLACEMENT OF THE HANDLE FOR THE OVERWING ESCAPE HATCH Closed 31.Mar.1993

737-52-1120-R2 (ACTIVE) SBPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-52-1122 SB NOTE

RECOMMENDED A/C AFT ENTRY DOOR AND GALLEY SERVICE DOORS Rejected by Operator

737-52-1122 SB

737-52-1125 SB NOTE

RECOMMENDED A/C AFT ENTRY DOOR FWD AFT SERVICE DOOR Rejected by Operator

737-52-1125 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1128 SB 01 MANDATORY A/C CONTROL CABIN DOOR - EMERGENCY EXIT PANEL INSPECTION See prev. Docstatus

Compliance:This SB ensures compliance with AD 1999-22-16 § (a) and (b).

This document is effective for LN# 1717-3028.1999-22-16 (ACTIVE)737-52-1128737-52-1128-R1 (ACTIVE)PRODUCTION PRR38060-24

ADSBSBPRR

00

This Document SUPERSEDES 737-52-1128/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks21.Feb.2001 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.

737-52-1128 SB 00 MANDATORY A/C CONTROL CABIN DOOR - EMERGENCY EXIT PANEL INSPECTION Superseded (Closed 21.Feb.2001)Compliance:This SB ensures compliance with AD 1999-22-16 § (a) and (b).

This document is effective for LN# 1717-3028.1999-22-16 (ACTIVE)737-52-1128737-52-1128-R1 (ACTIVE)PRODUCTION PRR38060-24

ADSBSBPRR

00








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1141 SB 02 RECOMMENDED A/C DOOR - ENTRY - UPPER AFT CORNER DOOR STOP REPLACEMENT Not Applicable by Serial Number


737-52-1141 SB 01 RECOMMENDED A/C DOOR, FWD ENTRY - UPPER AFT CORNER DOOR STOP REPLACEMENT Superseded (Not Applicable bySerial Number)

737-52-1141-R0 (REF)737-52-1141-R1 (ACTIVE)PRODUCTION PRR38060-33SBB 737-52-1141 (MOD-TASK)

SBSBPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1149 SB 00 RECOMMENDED A/C DOORS - FORWARD CARGO DOOR - NUMBER 4 CROSS BEAM INSPECTION REPAIR

AND MODIFICATIONOpen

References:Ref/A/: (SRP) 737-SRP-52-0070.Ref/B/: (SIIA) 737-287Ref/C/: SB 737-52A1100 Rev04Perform WITHIN 9000/C (effective from 11.Dec.2003) for the first timeThereafter perform in an interval of 20000/C

737-52-1149/SB Rev.00 DOORS - FORWARD CARGO DOOR - NUMBER 4 CROSS BEAM INSPECTION REPAIRAND MODIFICATION

Open

> 737-52-1149-01/EO* Rev.00 FWD CARGO DOOR - NDT INSP. NUMBER 4 CROSS BEAM RepetitiveThis Document is terminated with implementation of 737-52-1149-03/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

60570/CPerform initially within (effective from11.Dec.2003) (F) 9000/C /Interval(F):20000/C

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Nov.2012 68139:00/H 40570/C 273640, N/A Was due at: 43575/C PerfRev.:'00'

> 737-52-1149-02/EO* Rev.00 DOORS - FORWARD CARGO DOOR - NUMBER 4 CROSS BEAM REPAIR Term.Action openThis Document is terminated with implementation of 737-52-1149-03/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> 737-52-1149-03/EO* Rev.00 DOORS - FORWARD CARGO DOOR - NUMBER 4 CROSS BEAM MODIFICATION Term.Action open

This Document terminates 737-52-1149-01/EO Rev.00This Document terminates 737-52-1149-02/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1154 SB 00 MANDATORY A/C DOORS - CARGO COMPARTMENT DOORS - AFT CARGO DOOR - CROSS BEAM D

INSPECTION, REPAIR AND PREVENTIVE MODIFICATIONSuperseded (Cancelled)

NOTE:Boeing Service Bulletin 737-52A1079 and Boeing Service Bulletin737-52A1153 have similar access requirements as this service bulletin.

NOTE:Federal Aviation Administration (FAA) Airworthiness Directives AD98-11-04 R1, AD 2008-08-23 and AD 2008-09-13 are related to thisservice bulletin.737-52A1079737-SRP-52-0079

SBSRP

0700

This Document has been SUPERSEDED BY 737-52-1154/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1154 SB 01 MANDATORY A/C DOORS - CARGO COMPARTMENT DOORS - AFT CARGO DOOR - CROSS BEAM INSP. Superseded (Superseded)


NOTE:Federal Aviation Administration (FAA) Airworthiness Directives AD98-11-04 R1, AD 2008-08-23 and AD 2008-09-13 are related to thisservice bulletin.

NOTE: As specified per SB 737-52-1154 Paragraph E., for subject Group2., the inteval is controlled by Service Bulletin 737-52A1153.737-52A1079737-SRP-52-0079

SBSRP

0700

This Document SUPERSEDES 737-52-1154/SB Rev.00This Document has been SUPERSEDED BY 737-52-1154/SB Rev.02Perform WITHIN 4500/C (effective from 13.Jul.2011)

737-52-1154/SB Rev.01 DOORS - CARGO COMPARTMENT DOORS - AFT CARGO DOOR - CROSS BEAM INSP. SupersededThis Document SUPERSEDES 737-52-1154/SB Rev.00This Document has been SUPERSEDED BY 737-52-1154/SB Rev.02

> 737-52-1154-01/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, INSPECTION SupersededThis Document has been SUPERSEDED BY 737-52-1154-01/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52-1154 SB 02 MANDATORY A/C DOORS - CARGO COMPARTMENT DOORS - AFT CARGO DOOR - CROSS BEAM INSP. On Attrition


NOTE:Federal Aviation Administration (FAA) Airworthiness Directives AD98-11-04 R1, AD 2008-08-23 and AD 2008-09-13 are related to thisservice bulletin.

NOTE: As specified per SB 737-52-1154 Paragraph E., for subject Group2., the inteval is controlled by Service Bulletin 737-52A1153.2013-13-12737-52A1079737-52A1153737-SRP-52-0079

ADSBSBSRP

00070100

This Document SUPERSEDES 737-52-1154/SB Rev.01737-52-1154/SB Rev.02 DOORS - CARGO COMPARTMENT DOORS - AFT CARGO DOOR - CROSS BEAM INSP. On Attrition

This Document SUPERSEDES 737-52-1154/SB Rev.01> 737-52-1154-01/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM D, INSPECTION On Attrition

This Document SUPERSEDES 737-52-1154-01/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition / NO LIMIT

> 737-52-1154-02/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, FORWARD END REPAIR On AttritionAffected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52-1154-03/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, AFT END REPAIR On AttritionAffected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52-1154-04/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, REPETITIVE INSPECTION AFTER REPAIR On AttritionAffected Rotables (Part No/Serial No/Position) Status





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

737-52-1161 SB NOTE

OPTIONAL A/C DOORS - FORWARD AIRSTAIR - HANDRAIL SAFETY IMPROVEMENTS Open

737-52-1161 SBDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT

737-52A1079 SB 07 MANDATORY A/C DOORS - AFT CARGO - FRAME AND BEAM INSPECTION, REPAIR AND MODIFICATION Not Applicable by Serial NumberSupplemental information to AD 2000-06-13 RI (a):Aircraft LN-KKR (msn:24256) was inspected per AD 98-25-06 (Air EuropaEO 3/52/1400).1998-25-06 (SUPERSEDED)2006-06-13 (ACTIVE)737-52A1153737-SRP-52-0077

ADADSBSRP

00010000






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52A1079 SB 00 MANDATORY A/C *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD Superseded (Not Applicable by

Serial Number)1998-25-06 (SUPERSEDED)2000-06-13 (SUPERSEDED)2000-06-13-R1 (ACTIVE)737-52A1079-R0 (REF)737-52A1079-R1 (REF)737-52A1079-R2 (REF)737-52A1079-R3 (REF)737-52A1079-R4 (REF)737-52A1079-R5 (REF)737-52A1079-R6 (ACTIVE)SBB 737-52A1079 (MOD TASK)

ADADADSBSBSBSBSBSBSBTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52A1100 SB 04 MANDATORY A/C *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005

2000-07-06 (ACTIVE)37-SBB-52A1100 (REPETITIVE)737-52A1100 IN 07737-52A1100 IN 09737-52A1100-R0 (REF)737-52A1100-R1 (REF)737-52A1100-R2 (REF)737-52A1100-R3 (REF)737-52A1100-R4 (ACTIVE)SBB 737-52A1100 (MOD-TASK)

ADTASBSBSBSBSBSBSBTA

Perform BEFORE 12000/CPerform BEFORE 16.May.2004

737-52A1100/SB Rev.04 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005> 737-52A1100/EO* Rev.04 *AD* FWD CARGO DOORS, LOWER FWD AND AFT CORNER INSP, MOD AN Not Applicable by Serial Number

This Document is terminated with implementation of 737-52A1100-01/EO Rev.04> 737-52A1100-01/EO* Rev.04 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005

This Document terminates 737-52A1100/EO Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52A1100 SB 05 MANDATORY A/C *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Open

This AD supersedes AD 2000-07-06, Amendment 39-11660 (65 FR 19302,April 11, 2000).

This AD applies to all The Boeing Company Model 737-100, -200, -200C,-300, -400, and - 500 series airplanes, certificated in any category.

§ 39.13 [Amended]2. The FAA amends § 39.13 by removing airworthiness directive (AD)2000-07-06, Amendment 39-11660 (65 FR 19302, April 11, 2000), andadding the following new AD:

2013-09-10 The Boeing Company: Amendment 39-17452; Docket No.FAA-2012-0855; Directorate Identifier 2011-NM-136-AD.

Compliance:AD § 39.13 is complied with through SB 737-52A1100 rev 05.Cargo Door modification pr:EO 737-52A1100-01 - *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNERMOD/REPL.2000-07-06 (ACTIVE)37-SBB-52A1100 (REPETITIVE)737-52A1100 IN 07737-52A1100 IN 09737-52A1100-R0 (REF)737-52A1100-R1 (REF)737-52A1100-R2 (REF)737-52A1100-R3 (REF)737-52A1100-R4 (ACTIVE)SBB 737-52A1100 (MOD-TASK)

ADTASBSBSBSBSBSBSBTA

Perform BEFORE 12000/C





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusPerform BEFORE 16.May.2004

737-52A1100/SB Rev.05 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Open> 737-52A1100-01/EO* Rev.05 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER MOD/REPL. See prev. Docstatus

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150399 ITEM: 1

> 737-52A1100-02/EO* Rev.00 FWD CARGO DOORS, LOWER FWD AND AFT CORNER INSPECTION. PART V -SUPPLEMENTAL STRUCTURAL INSPECTIONS.

Open / Special Text: Additional workper SB Rev.5, EO not amended by AD2013-09-10


46328/CPerform initially within (effective from28.Jun.2013) (F) 4500/C /Interval(F):4500/C

737-52A1105 SB 02 MANDATORY A/C *AD* DOORS - CTRL CABIN DOOR BLOWOUT PANELS,INSP. OF SEALANT Not Applicable by Serial Number1989-04-03 (ACTIVE)737-52A1105-R0 (REF)737-52A1105-R1 (REF)737-52A1105-R2 (ACTIVE)SBB 737-52A1105(MOD-TASK)

ADSBSBSBTA

737-52A1124 SB 00 MANDATORY A/C AD* FWD GALLEY SERVICE DOOR - LWR GATE HINGE REPLACEMENT Not Applicable by Serial NumberThis document is applicable to LN# 241-1727. The following LN# areNot Applicable per PRR 34473.1996-10-06 (ACTIVE)2004-225 (REF)737-52A1124 (ACTIVE)PRODUCTION LINE PRR34473

ADADSBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52A1153 SB 00 MANDATORY A/C DOORS - AFT CARGO - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES AND

REINFORCING ANGLES - INSPECTION, REPAIR AND MODIFICATIONSuperseded (Event-Triggered14.Feb.2014 W/O:502763)

ATTN: Part-M Planning:

Service Bulletin 737-52-1154 must be performed together with ServiceBulletin 737-52A1153.

MATERIAL:Top kits 65C37547-50 and 65C37547-60 are only necessary if theforward and/or aft lower frame and reinforcing angle are cracked.2013-13-12737-52-1154737-52A1079737-52A1079

ADSBSBSB

00010007

This Document has been SUPERSEDED BY 737-52A1153/SB Rev.01Perform within an unlimited threshold.

737-52A1153/SB Rev.00 DOORS - AFT CARGO - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES ANDREINFORCING ANGLES - INSPECTION, REPAIR AND MODIFICATION

Event-Triggered 14.Feb.2014W/O:502763

This Document has been SUPERSEDED BY 737-52A1153/SB Rev.01> 737-52A1153-01/EO* Rev.02 AFT CARGO DOOR - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES AND

REINFORCING ANGLES - INSPECTION.Superseded

This Document SUPERSEDES 737-52A1153-01/EO Rev.00This Document SUPERSEDES 737-52A1153-01/EO Rev.01This Document has been SUPERSEDED BY 737-52A1153-01/EO Rev.03Affected Rotables (Part No/Serial No/Position) Status

65-47952-337 / 001649 Pos=AFT (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

> 737-52A1153-02/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM E, PREVENTATIVE MOD TO BOTH ENDS, ANDLOWER CORNER FRAME TERMINATING INSPECTION

Superseded

This Document has been SUPERSEDED BY 737-52A1153-02/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status





24.Oct.2014/411


65-47952-337 / 001649 Pos=AFT (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

> 737-52A1153-03/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM E, FORWARD END REPAIR SupersededThis Document has been SUPERSEDED BY 737-52A1153-03/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-04/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM E, AFT END REPAIR SupersededThis Document has been SUPERSEDED BY 737-52A1153-04/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-05/EO* Rev.00 AFT CARGO DOOR - FORWARD LOWER CORNER FRAME AND REINFORCING ANGLES -REPLACEMENT

Superseded

This Document has been SUPERSEDED BY 737-52A1153-05/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-06/EO* Rev.00 AFT CARGO DOOR - AFT LOWER CORNER FRAME AND REINFORCING ANGLES -REPLACEMENT

Superseded

This Document has been SUPERSEDED BY 737-52A1153-06/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-10/EO* Rev.01 SUPPLEMENTAL STRUCTURAL INSPECTIONS, AFT CARGO DOOR - CROSS BEAM EAND ADJACENT LOWER CORNER FRAMES AND ANGLES.

Event-Triggered

This Document SUPERSEDES 737-52A1153-10/EO Rev.00This Document has been SUPERSEDED BY 737-52A1153-10/EO Rev.02Affected Rotables (Part No/Serial No/Position) Status

65-47952-337 / 001649 Pos=AFT (KKM)Event-Triggered / Reason: The performeddate is never defined for the firstEvent-triggered history entry





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-52A1153 SB 01 MANDATORY A/C DOORS - AFT CARGO - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES AND

REINFORCING ANGLES - INSPECTION, REPAIR AND MODIFICATIONOpen

ATTN: Part-M Planning:

Service Bulletin 737-52-1154 must be performed together with ServiceBulletin 737-52A1153.

MATERIAL:Top kits 65C37547-50 and 65C37547-60 are only necessary if theforward and/or aft lower frame and reinforcing angle are cracked.2013-13-12737-52-1154737-52A1079737-52A1079

ADSBSBSB

00010007

This Document SUPERSEDES 737-52A1153/SB Rev.00737-52A1153/SB Rev.01 DOORS - AFT CARGO - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES AND

REINFORCING ANGLES - INSPECTION, REPAIR AND MODIFICATIONOpen

This Document SUPERSEDES 737-52A1153/SB Rev.00> 737-52A1153-01/EO* Rev.03 AFT CARGO DOOR - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES AND

REINFORCING ANGLES - INSPECTION.Open

This Document SUPERSEDES 737-52A1153-01/EO Rev.02This Document is terminated with implementation of 737-52A1153-02/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) Open / Next Due: 42971/C

> 737-52A1153-02/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM E, PREVENTATIVE MOD TO BOTH ENDS, ANDLOWER CORNER FRAME TERMINATING INSPECTION

Open

This Document terminates 737-52A1153-01/EO Rev.03This Document SUPERSEDES 737-52A1153-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) Open / Next Due:09.Sep.2017 46633/C

> 737-52A1153-03/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM E, FORWARD END REPAIR On Attrition





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-52A1153-03/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status

65-47952-337 / 001649 Pos=AFT (KKM)On Attrition / Reason: To be performed ifcracks are found on EO-01

> 737-52A1153-04/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM E, AFT END REPAIR On AttritionThis Document SUPERSEDES 737-52A1153-04/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-05/EO* Rev.01 AFT CARGO DOOR - FORWARD LOWER CORNER FRAME AND REINFORCING ANGLES -REPLACEMENT

On Attrition

This Document SUPERSEDES 737-52A1153-05/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-06/EO* Rev.01 AFT CARGO DOOR - AFT LOWER CORNER FRAME AND REINFORCING ANGLES -REPLACEMENT

On Attrition

This Document SUPERSEDES 737-52A1153-06/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1153-10/EO* Rev.02 SUPPLEMENTAL STRUCTURAL INSPECTIONS, AFT CARGO DOOR - CROSS BEAM EAND ADJACENT LOWER CORNER FRAMES AND ANGLES.

Event-Triggered

This Document SUPERSEDES 737-52A1153-10/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status

65-47952-337 / 001649 Pos=AFT (KKM)Event-Triggered / Reason: To be performed4500 CY after rep or preventative mod /Last Performed: RefDocument:





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1088 SB 01 RECOMMENDED A/C OUTBOARD CHORD STA 727 BULKHEAD INSPECTION Repetitive

37-SBB-53-1088-1 (REPETITIVE)737-53-1088 R0 (REF)737-53-1088 R1 (ACTIVE)737-SRP-53-0162 (REF)SBB 737-53-1088-1 (MOD)

TASBSBSRPTA

Perform within an unlimited threshold.737-53-1088/SB Rev.01 OUTBOARD CHORD STA 727 BULKHEAD INSPECTION Repetitive> 737-53-1088-1/EO* Rev.01 OUTBOARD CHORD STA 727 BULKHEAD FASTENES INSPECTION Repetitive

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document48151/C Interval(F):5000/C

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Feb.2014 71572:00/H 43151/C 489477, N/A Was due at: 45000/C PerfRev.:'01'

> 737-53-1088-2/EO* Rev.00 FLAP TRACK SUPPORT FITTING FASTENER INSPECTION. ONE TIME INSPECTION Closed 13.Feb.2014 W/O:501277Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks13.Feb.2014 71572:00/H 43151/C 501277, N/A Was due at: 11.Dec.2015 PerfRev.:'00'

737-53-1088L SB 01 RECOMMENDED A/C OUTBOARD CHORD REPLACEMENT - STA 727 BULKHEAD. LEFT HAND OpenSBB 737-53-1088SBB 737-53-1088 R1

SBSB


737-53-1088L/SB* Rev.01 OUTBOARD CHORD REPLACEMENT - STA 727 BULKHEAD. LEFT HAND OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> 07-1040/TD* Rev.00 STA 727 FRAME OUTBOARD CHORD - REPLACEMENT OF REPAIR/MOD. Not Applicable by Serial Number





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1088R SB 01 RECOMMENDED A/C OUTBOARD CHORD REPLACEMENT - STA 727 BULKHEAD, R/H SIDE Open

SBB 737-53-1088SBB 737-53-1088 R1

SBSB


737-53-1089 SB NOTE

MANDATORY A/C *AD* FUSELAGE - SKIN CRACKS AT STRINGER 17 - INSP. & MOD. Not Applicable by Serial Number

1988-22-11 R1737-53-1089737-53-1089 R1737-53-1089 R2737-53-1089 R3737-53-1089 R4737-53A1039 R4

ADSBSBSBSBSBSB

737-53-1096 SB 05 MANDATORY A/C *AD* FUSELAGE - AFT LOWER CARGO DOORWAY FRAME INSP/MOD/REP Not Applicable by Serial Number1993-14-10 (ACTIVE)737-53-1096 (REF)737-53-1096 R1 (REF)737-53-1096 R2 (REF)737-53-1096 R3 (REF)737-53-1096 R4 (REF)737-53-1096 R5 (ACTIVE)SBB 737-53-1096 (MAINT TASK)

ADSBSBSBSBSBSBTA





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1104 SB 04 OPTIONAL A/C FUSELAGE, KEEL BEAM LWR SKIN PANEL INSP & MOD OR REPLACEMENT Open

737-53-1104737-53-1104 R1737-53-1104 R2737-53-1104 R3737-53-1104 R4

SBSBSBSBSB

Perform within an unlimited threshold.737-53-1104/SB Rev.04 FUSELAGE, KEEL BEAM LWR SKIN PANEL INSP & MOD OR REPLACEMENT Open> 737-53-1104-01/EO* Rev.04 FUSELAGE, KEEL BEAM LWR SKIN PANEL - MOD OR REPLACEMENT Term.Action open


> 737-53-1104P1/EO* Rev.04 FUSELAGE KEEL BEAM LWR SKIN PANEL CRACKS BS 661-726 -VISUAL INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



737-53-1107 SB 00 MANDATORY A/C *AD* FUSELAGE - FIN AFT, BOLT INSP. & REPLACEMENT Not Applicable by Serial NumberThis document is Applicable to LN#: 1-1485. All other LN# are NotApplicable per Boeing SB.1999-04-23 (ACTIVE)737-53-1107 (REF)737-53-1107 R1 (REF)737-53-1107 R2 (REF)737-53-1107 R3 (REF)737-53-1107 R4 (ACTIVE)

ADSBSBSBSBSB





24.Oct.2014/411


TERECOMMENDED A/C BS 520 FLOORBEAM MODIFICATION AND REPAIR Ex Factory


SBPRR

Reason for this StatusSET BY EFFECTIVE-FROM ON MOD

737-53-1122 SB NOTE

RECOMMENDED A/C FUSELAGE - CREASE BEAM WEB MODIFICATION Ex Factory


SBPRR

Reason for this StatusSET BY EFFECTIVE-FROM ON MOD

737-53-1123 SB 00 RECOMMENDED A/C FUSELAGE - BODY STATION 1016 BULKHEAD INSPECTION SCHEDULE Not Applicable by Serial Number737-53-1123-R0 (ACTIVE) SB

737-53-1125 SB NOTE

RECOMMENDED A/C FUSELAGE-FRAMES AND BULKHEADS-FRAME Rejected by Operator

737-53-1125 SB

737-53-1127 SB NOTE

RECOMMENDED A/C FUSELAGE - BODY STATION 235.8 FRAME, MISSING FASTENER INSP. Not Applicable by Serial Number

737-53-1127-R0 (ACTIVE) SB

737-53-1133 SB NOTE

RECOMMENDED A/C BODY STATION 664 VERTICAL PRESSURE WEB - FASTENER OMITTED Not Applicable by Serial Number

737-53-1133-R0 (ACTIVE) SB





24.Oct.2014/411


TERECOMMENDED A/C FUSELAGE-FORWARD CORNERS OF HORIZONTAL BEAM, BODY STN 1138 Rejected by Operator


SBPRR

737-53-1142 SB 01 RECOMMENDED A/C ATC CONTROL MODE ""S"" TRANSPONDER ANTENNAS STRUCTURE CHANGE Rejected by Operator737-53-1142-R1 (ACTIVE)737-SL-53-20 (REF)

SBSL

737-53-1143 SB 00 RECOMMENDED A/C FUSELAGE - BODY STATION 927 FRAME AND FAIL SAFE CHORD INSP Rejected by Operator737-53-1143-R0 (ACTIVE) SB

737-53-1144 SB 00 RECOMMENDED A/C STRINGER 16 RIGHT STATION 440 THROUGH STATION 480 INSPECTION Rejected by OperatorSBB 737-53-1144-R0 (ACTIVE) SB

737-53-1145 SB 00 RECOMMENDED A/C STRINGER 16 AT WING SCANNING LIGHT CUTOUT, INSP/PREVENT/MOD Rejected by Operator737-53-1145-R0 (ACTIVE) SB

737-53-1146 SB 00 RECOMMENDED A/C AFT ENTRY AND AFT GALLEY FORWARD DOOR FRAM - FASTENERS INSP Rejected by OperatorSBB 737-53-1146-R0 (ACTIVE) SB

737-53-1153 SB NOTE

RECOMMENDED A/C FUSELAGE.NAINFRAME BS951. Closed 13.Feb.1999








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1154 SB 02 MANDATORY A/C *AD* FUSELAGE, GALLEY NO 2 UPPER ATTACHMENT SUPPORT Not Applicable

AC that have status Not Applicable are either NA per SB effectivityor have reduced Galley weight.1995-02-08 (SUPERSEDED)2004-23-07 (ACTIVE)737-53-1154 (REF)737-53-1154-R1 (REF)737-53-1154-R2 (ACTIVE)PRODUCTION PRR349612SBB 737-53-1154 (MOD-TASK)

ADADSBSBSBPRRTA

Reason for this StatusN/A - SB EFFECTIVITY

737-53-1159 SB NOTE

RECOMMENDED A/C FUSELAGE - VHF ANTENNA SUPPORT STRUCTURE MOD AND REPAIR Rejected by Operator


SBPRR

737-53-1162 SB 00 RECOMMENDED A/C NOSE LANDING GEAR VIEWING TUBE CHANNEL SUPPORT MOD Rejected by Operator737-53-1162-R0 (ACTIVE) SB

737-53-1163 SB NOTE

RECOMMENDED A/C FUSELAGE - FORWARD ENTRY DOORWAY SKIN CUTOUT-INSP/MOD/REP Rejected by Operator

737-53-1163-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1168 SB 03 MANDATORY A/C FUSELAGE SKIN BS 727-1016 S-14/25 L/R - INSPECTION, MOD, REPLACEMENT Open

This Mod is applicable to LN# 1001-2565. The following LN# are NotApplicable per PRR35040.2009-21-01 (ACTIVE)6-1151-737-PGM-108 (REF)737-53-1168-R0 (REF)737-53-1168-R1 (REF)737-53-1168-R2 (REF)737-53-1168-R3 (ACTIVE)737-SRP-53-0131 (REF)PRODUCTION PRR 35040

ADBMSBSBSBSBSRPPRR

Perform within an unlimited threshold.737-53-1168/SB Rev.03 FUSELAGE SKIN BS 727-1016 S-14/25 L/R - INSPECTION, MOD, REPLACEMENT Open> 737-53-1168/EO* Rev.00 FUSELAGE SKIN BS 727-1016 S-14/25 L/R - INSPECTION *** REPETITIVE MANDATORY

INSPECTION ***Repetitive




> 737-53-1168-01/EO* Rev.00 FUSELAGE SKIN BS 727-1016 S-14/25 L/R - MOD, REPLACEMENT (NO SKIN CHANGECARRIED OUT)

Term.Action open


737-53-1170 SB 00 RECOMMENDED A/C STRINGER 18A WEB AT BS 727- INSP, REPAIR AND PREVENTIVE MOD Rejected by Operator737-53-1170-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1171 SB 00 RECOMMENDED A/C E1 ELECTRONIC RACK - RWD LEFT STANCHION INSPECTION AND REP Rejected by Operator


SBPRR

737-53-1178 SB 00 RECOMMENDED A/C FUSELAGE FRAME BSTA 663.75 - INTERNAL INSPECTION Open37-SBB-53-1178 (REPETITIVE)737-53-1178-R0 (ACTIVE)SBB 737-53-1178 (MOD)

TASBTA

Perform within an unlimited threshold.737-53-1178/SB Rev.00 FUSELAGE FRAME BSTA 663.75 - INTERNAL INSPECTION Open> 737-53-1178/EO* Rev.00 FRAME BS 663.75, OUTBD CHORD AT STRINGERS 3L-3R - INSPECTION *** VISUAL AND

NDT REPETITIVE INSPECTION ****Repetitive




> 737-53-1178-01/EO* Rev.00 FUSELAGE FRAME BSTA 663.75 - INTERNAL INSPECTION Term.Action openDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1179 SB 02 MANDATORY A/C BONDED SKIN DOUBLERS (TEAR STRAPS) DELAMINATION INSPECTION Closed 07.Feb.2008

2003-14-06 (ACTIVE)737-53-1179-R0 (REF)737-53-1179-R1 (REF)737-53-1179-R2 (ACTIVE)M-7200-03-01505SBB 737-53-1179 (MOD-TASK)

ADSBSBSBBMTA

0

This Document terminates AD-2003-14-06-1/EO Rev.00This Document terminates AD-2003-14-06-2/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-53-1180 SB 00 RECOMMENDED A/C FUSELAGE - SECTION 41 SKIN - QUALIFICATION FOR REDUCED VERTICALSEPARATION MIMIMUM (RVSM) OPERATION



SBPRR

737-53-1181 SB NOTE

RECOMMENDED A/C FUSELAGE FRAMES - BSTA 727 OUTBOARD CORD INSP/PREVENTIVE MOD Rejected by Operator

737-53-1181-R0 (ACTIVE) SB





24.Oct.2014/411


TEOPTIONAL A/C FUSELAGE FRAME INNER CHORD BS 616 AND 639 REPAIR AND MOD Closed 01.Sep.2006

737-53-1182737-53-1182 IN 01737-53-1182 R1

SBSBSB

Perform within an unlimited threshold.737-53-1182/SB Rev.NOTE FUSELAGE FRAME INNER CHORD BS 616 AND 639 REPAIR AND MOD Closed 01.Sep.2006> 737-53-1182-01/EO*Rev.NOTE

FUSELAGE FRAME INNER CHORD BS 616 AND 639 REPAIR AND MOD Closed 01.Sep.2006


01.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: WO 150778PAGE 6

Reason for this StatusWO 150778 PAGE 6

737-53-1184 SB NOTE

RECOMMENDED A/C INSPECTION AT BS 663.75 COMPRESSION CHORD Rejected by Operator

737-53-1184 SB

737-53-1192 SB NOTE

OPTIONAL A/C FWD ENTRY AND GALLEY - FLOOR PANEL AND GREY WATER DRAIN MOD Rejected by Operator

737-53-1192-R0 (ACTIVE)737-SRP-53-005 (REF)PRODUCTION PRR35005-123

SBSRPPRR





24.Oct.2014/411


TEMANDATORY A/C *AD* STRINGERS S7L - S-16L FWD & AFT OF FWD ENTRY DOOR INSP. Closed 17.Mar.2005

2005-20-03 (ACTIVE)737-53-1204 IN 01 (REF)737-53-1204-R0 (SUPERSDED)737-53A1204-R1 (ACTIVE)PRODUCTION LINE MRR3537-1153

ADSBSBSBPRR








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1216 SB 01 MANDATORY A/C *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008

2006-26-09 (ACTIVE)37-SBB-53-1216 (REPETITIVE)737-53-1216-R0 (REF)737-53-1216-R1 (AVTIVE)SBB 737-53-1216 (REP-TASK)

ADTASBSBTA

Perform within an unlimited threshold.737-53-1216/SB Rev.01 *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008> 737-53-1216/EO* Rev.01 *AD* AIRCONDITIONING BRACKET ATTACHMENTS ST 360 - 907, INSP Cancelled

This Document is terminated with implementation of 737-53-1216-01/EO Rev.01Reason for this StatusCANCELLED DUE TO EO 737-53-1216-01 PERFORMED

> 737-53-1216-01/EO* Rev.01 *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008This Document terminates 737-53-1216/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



737-53-1216-2 SB 01 MANDATORY A/C *AD* AIR-COND. BRACKET ATTACHMENTS POST MOD / REPAIR INSP. Open2006-26-09 PARAGRAPH K737-53-1216 R1, PART 4737-53-1216-R0 (REF)SBB 737-53-1216-2 (INSP-TASK)

ADSBSBTA

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document54315/C Perform initially before(F) 54315/C





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1229 SB 00 RECOMMENDED A/C BS 1016 AFT PRESSURE BULKHEAD TENSION BOLTS - INSP. & REPL. Closed 07.Feb.2008

737-53-1229737-FTD-53-07001

SBFTD








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1230 SB 00 MANDATORY A/C *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006

2005-19-25 (ACTIVE)37-SBB-53-1230P1(REPETITIVE)737-53-1230-R0 (ACTIVE)SBB 737-53-1230 (MOD TASK)

ADTASBTA

Perform within an unlimited threshold.737-53-1230/SB Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006> 737-53-1230-01/EO* Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006

This Document terminates 737-53-1230P1/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-53-1230P1/EO* Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT INSPEC CancelledThis Document is terminated with implementation of 737-53-1230-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

04.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150738 KKM SBB 737-53-1230*AD*ANTENNA C

Reason for this StatusPREVENTIVE MODIFIACTION PERF. ON EO 737-53-1230-01

737-53-1230P3 SB NOTE

MANDATORY A/C *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT REPAIR Not Applicable

2005-19-25737-53-1230

ADSB

Reason for this StatusSB 737-53-1230 PART 2 C/W





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1234 SB 01 MANDATORY A/C FUSELAGE SKIN - NDT INSP OF CRACKS AT CHEM-MILLED STEPS Superseded (Not Applicable)

EO R-01. Repeat inspection changed to Eddy Current inspection only,to match Service Bulletin R1.2005-13-27 (ACTIVE)737-53-1234-R0 (REF)737-53-1234-R1 (ACTIVE)

ADSBSB

This Document has been SUPERSEDED BY 737-53A1234/SB Rev.02737-53-1234/SB Rev.01 FUSELAGE SKIN - NDT INSP OF CRACKS AT CHEM-MILLED STEPS Not Applicable

This Document has been SUPERSEDED BY 737-53A1234/SB Rev.02> 737-53-1234-P1A/EO* Rev.01 *AD* FUSELAGE SKIN - NDT INSP - CRACKS AT CHEM MILLED STEPS Not Applicable by Serial Number

This Document SUPERSEDES 737-53-1234-P1A/EO Rev.00This Document has been SUPERSEDED BY 737-53A1234-01/EO Rev.00

> 737-53-1234-P1A/EO* Rev.00 *AD* FUSELAGE SKIN - NDT INSP - CRACKS AT CHEM MILLED STEPS Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-53-1234-P1A/EO Rev.01

> 737-53-1234-P1B/EO* Rev.00 *AD* FUSELAGE SKIN - NDT INSP - CRACKS AT CHEM MILLED STEPS. Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-53A1234-01/EO Rev.00

737-53-1246 SB 00 RECOMMENDED A/C FRAME LOWER FITTING BS 685 INSPECTION, REPAIR & REPLACEMENT Open737-53-1246 SBPerform within an unlimited threshold.

737-53-1246/SB Rev.00 FRAME LOWER FITTING BS 685 INSPECTION, REPAIR & REPLACEMENT Open> 737-53-1246/EO* Rev.00 BS 685 FRAME LOWER FITTING - POST MOD INSPECTION Open



> 737-53-1246-01/EO* Rev.00 FRAME LOWER FITTING BS 685 INSPECTION, REPAIR & REPLACEMENT Closed 23.Mar.2010Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

23.Mar.2010 60867:00/H 35008/C2-MOD520108 ITEM:4





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1260 SB 01 MANDATORY A/C FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK LINK

ASSEMBLIES - REPLACEMENT/MODIFICATIONOpen

This service bulletin gives instructions to repair or replace thecabin floor seat track link assemblies between BS 520 and BS 540. Ifthe work given in this service bulletin is not accomplished, thecurrent seat track crowns and seat track link assemblies couldseparate during a 9G emergency landing condition. If the seat trackcrown and the seat track link assembly separate, the passenger seatswould not have adequate support during a 9G emergency landing. Thiscould result in injury to passengers.2013-24-13 AD 00This Document SUPERSEDES 737-53-1260/SB Rev.00Perform WITHIN 1825/D (effective from 07.Jan.2014)

737-53-1260/SB Rev.01 FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK LINKASSEMBLIES - REPLACEMENT/MODIFICATION

Open

This Document SUPERSEDES 737-53-1260/SB Rev.00> 737-53-1260-01/EO* Rev.00 FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK LINK

ASSEMBLIES - REPLACEMENT/MODIFICATIONOpen


06.Jan.2019Perform initially within (effective from07.Jan.2014) (F) 1825/D

737-53-1260 SB 00 RECOMMENDED A/C STATION 520 TO 540/SEAT TRACK LINK ASSEMBLIES - REPLACEMENT Superseded (Superseded)737-53-1120-R1 (REF)737-53-1260-R0 (ACTIVE)737-SRP-53-0179 (REF)PRR35005-252RS (ECM)WARRANTY AS OF NOV 18, 2002

SBSBSRPPRRSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1267 SB 00 MANDATORY A/C *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD Open

2007-26-04 (ACTIVE)37-SBB-53-1267 (REPETITIVE)737-53-1267-R0 (ACTIVE)SBB 737-53-1267 (MOD-TASK)

ADTASBTA

Perform BEFORE 75000/C737-53-1267/SB Rev.00 *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD Open> 737-53-1267/EO* Rev.00 *AD* FUSELAGE - SKIN - CIRCUMFERENTIAL BUTT SPLICE - MODIFI Open

This Document is terminated with implementation of 737-53-1267-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> 737-53-1267-01/EO* Rev.00 *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD OpenThis Document terminates 737-53-1267/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

75000/C Perform initially before(F) 75000/C





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1268 SB 00 MANDATORY A/C *AD* STRINGER TIE CLIPS - STA 360 TO 907, S10R/L INSP/REPAIR Repetitive

1993-08-04 (REF)2009-04-15 (ACTIVE)37-SBB-53-1268-A (REPETITIVE)737-53-1085-R1 (REF)737-53-1268-R0 (ACTIVE)737-SRP-53-0212 (REF)NPRM 2007-NM-085-AD (REF)PRODUCTION LINEMRR3534-1595S

ADADTASBSBSRPADPRR

Perform within an unlimited threshold.737-53-1268/SB Rev.00 *AD* STRINGER TIE CLIPS - STA 360 TO 907, S10R/L INSP/REPAIR Repetitive> 737-53-1268-A/EO* Rev.00 *AD* FUSELAGE - STRINGER TIE CLIPS - STA 360 TO 907, S10R/L *** MANDATORY

REPETITIVE NDT AND DETAILED INSPECTION ***Repetitive




07.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151295 KKM 37-SBB-53-1268-ASTRINGER TIE

737-53-1287 SB 00 OPTIONAL A/C SKIN CRACKING UNDER THE NUMBER 3 VHF ANTENNA - INSPECTION Superseded (Not Applicable)737-53-1287-R0 (ACTIVE)737-SRP-53-0313 (REF)NO 3 VHF ANTENNA NOTINSTALLED

SB

SRP

SB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53-1287 SB 01 OPTIONAL A/C FUSELAGE - SKIN - SKIN CRACKING UNDER THE NUMBER 3 VHF ANTENNA -

INSPECTION, REPAIR AND PREVENTIVE MODIFICATIONNot Applicable / Special Text:Service Bulletin not applicable forNAS fleet.

737-53A1042737-SRP-53-0313 (REF)NO 3 VHF ANTENNA NOTINSTALLED

SB

SRP

SB

00

N/A

N/A


737-53A1075 SB 03 MANDATORY A/C *AD* AFT PRESSURE BULKHEAD INSPECTION Repetitive2002-10-11 (ACTIVE)37-SBB-53A1075 (REPETITIVE)737-53A1075-R0 (REF)737-53A1075-R1 (REF)737-53A1075-R2 (REF)737-53A1075-R3 (ACTIVE)

ADTASBSBSBSB

Perform within an unlimited threshold.737-53A1075/SB Rev.03 *AD* AFT PRESSURE BULKHEAD INSPECTION Repetitive> 737-53A1075-01/EO* Rev.00 *AD* AFT PRESSURE BULKHEAD INSPECTION/MOD AND REP *** MANDATORY

REPETITIVE DETAILED VISUAL INSPECTION ***Repetitive

This Document SUPERSEDES 737-53A1075/EO Rev.03NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

25.Feb.2016Perform initially within (effective from08.Apr.2014) (L) 120/D / Interval(F):730/D


25.Feb.2014 71572:00/H 43151/C N/APerfRev.:'03' / Reason: Initialized: Last perf.with 737-53A1075/EO/03





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1108 SB 05 MANDATORY A/C *AD* FUSELAGE - FWD SERVICE DOORWAY AFT FRAME INSP. & REPAIR Superseded (Not Applicable by

Serial Number)This document is applicable to LN# 1-1426. The following LN# are NotApplicable per PRR34320R.1998-22-10 (ACTIVE)737-53-1108-R0 (REF)737-53-1108-R1 (REF)737-53-1108-R2 (REF)737-53-1108-R3 (REF)737-53-1108-R4 (REF)737-53-1108-R5 (ACTIVE)PRODUCTION PRR34320RSBB 737-53A1108 (INSP-TASK)

ADSBSBSBSBSBSBPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1108 SB 06 MANDATORY A/C FUSELAGE - FRAMES AND BULKHEADS - FORWARD GALLEY SERVICE DOORWAY AFT

FRAME - INSPECTION AND REPAIRSuperseded (Superseded)

NAS aircraft added as Group 31998-22-10 (ACTIVE) ADThis Document SUPERSEDES 737-53A1108/SB Rev.05This Document has been SUPERSEDED BY 737-53A1108/SB Rev.07Perform within an unlimited threshold.

737-53A1108/SB Rev.06 FUSELAGE - FRAMES AND BULKHEADS - FORWARD GALLEY SERVICE DOORWAY AFTFRAME - INSPECTION AND REPAIR

Superseded


> 737-53A1108-01/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEAD - FWD GALLEY SERVICE DOORWAY, AFTFRAME - INSP AND REPAIR

Superseded

This Document has been SUPERSEDED BY 737-53A1108-01/EO Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1116 SB 04 MANDATORY A/C FUSELAGE - SKIN - FORWARD GALLEY SERVICE DOORWAY UPPER AND LOWER

CORNERS - INSPECTION AND REPAIROpen

All Aircraft are in Group 3 of SB 737-53A1116R4Perform within an unlimited threshold.

737-53A1116/SB Rev.04 FUSELAGE - SKIN - FORWARD GALLEY SERVICE DOORWAY UPPER AND LOWERCORNERS - INSPECTION AND REPAIR

Open

> 737-53A1116-01/EO* Rev.00 FUSELAGE - SKIN - FORWARD GALLEY SERVICE DOORWAY UPPER FWD CORNER -INSPECTION

Open

NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

46953/CPerform initially before(L) 35000/C Performinitially within (effective from 30.Sep.2013)(L) 4500/C / Interval(F):4500/C

> 737-53A1116-02/EO* Rev.00 FUSELAGE - SKIN - FORWARD GALLEY SERVICE DOORWAY LOWER FWD CORNER -INSPECTION

Open



> 737-53A1116-03/EO* Rev.00 FUSELAGE - SKIN - FORWARD GALLEY SERVICE DOORWAY UPPER AFT CORNER -INSPECTION

Open



> 737-53A1116-04/EO* Rev.00 FUSELAGE - SKIN - FORWARD GALLEY SERVICE DOORWAY LOWER AFT CORNER -INSPECTION

Open






24.Oct.2014/411



737-53A1137 SB NOTE

MANDATORY A/C *AD* FUSELAGE - FWD ENTRY DOORWAY - LWR DOOR STOP FAST. INSP Not Applicable by Serial Number

1989-23-52737-53A1137737-53A1137 R1

ADSBSB

737-53A1152 SB 01 MANDATORY A/C *AD* FUSELAGE-SIDE OF BODY FLOOR PANEL INSERTS-INSP./REP Not ApplicableNA per SB effectivity.1992-16-01 (ACTIVE)737-53A1152-R1 (ACTIVE)

ADSB

This Document SUPERSEDES 737-53A1152/SB Rev.00Reason for this StatusNA DUE TO SB EFFECTIVITY

737-53A1152 SB 00 MANDATORY A/C *AD* FUSELAGE-SIDE OF BODY FLOOR PANEL INSERTS-INSP./REP Superseded (Superseded)NA per SB effectivity.1992-16-01 (ACTIVE)737-53A1152-R1 (ACTIVE)

ADSB

This Document has been SUPERSEDED BY 737-53A1152/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1163 SB 01 RECOMMENDED A/C FUSELAGE - SKIN - FORWARD ENTRY DOORWAY SKIN CUTOUT - UPPER FORWARD

AND UPPER AFT CORNERS - INSPECTION, MODIFICATION, AND REPAIROpen

737-53A1163-01/EO INITIAL AND REPETITIVE INSP737-53A1163-02/EO REPAIR (IF FINDINGS)737-53A1163-03/EO INSP OF REPDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT737-53A1163/SB* Rev.01 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY SKIN CUTOUT - UPPER FORWARD

AND UPPER AFT CORNERS - INSPECTION, MODIFICATION, AND REPAIROpen


> 737-53A1163-01/EO* Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY SKIN CUTOUT - UPPER FORWARDAND UPPER AFT CORNERS - INSPECTION

Repetitive


47651/CPerform initially within (effective from08.Jan.2014) (F) 4500/C /Interval(F):4500/C


> 737-53A1163-02/EO* Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY SKIN CUTOUT - UPPER FORWARDAND UPPER AFT CORNERS - REPAIR

On Attrition

> 737-53A1163-03/EO* Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY SKIN CUTOUT - UPPER FORWARDAND UPPER AFT CORNERS - INSP OF REP

On Attrition





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1166 SB 02 RECOMMENDED A/C FUSELAGE - FRAMES - BODY STATION 727 OUTBOARD CHORD AT STRINGER 18A

INSPECTION AND PREVENTIVE MODIFICATIONOpen

37-SBB-53A1166-P1 (REPETITIVE)37-SBB-53A1166-P2 (REPETITIVE)37-SBB-53A1166-P3 (REPETITIVE)737-53A1166 IN02 (REF)737-53A1166 IN03 (REF)737-53A1166-R0 (REF)737-53A1166-R1 (REF)737-53A1166-R2 (ACTIVE)SBB 737-53A1166 (MOD TASK)

TATATASBSBSBSBSBTA

Perform within an unlimited threshold.737-53A1166/SB Rev.02 FUSELAGE - FRAMES - BODY STATION 727 OUTBOARD CHORD AT STRINGER 18A

INSPECTION AND PREVENTIVE MODIFICATIONOpen

> 07-1040/TD* Rev.00 STA 727 FRAME OUTBOARD CHORD - REPLACEMENT OF REPAIR/MOD. Not Applicable by Serial Number> 737-53A1166-F1/EO* Rev.01 FUSELAGE, FRAMES BST 727 OUTB CHORD AT STR 18A INSP & MOD Term.Action open


> 737-53A1166-P1/EO* Rev.01 FUSELAGE FRAME BS727 AUX & OUTB CHORD AT STR 18A INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> 737-53A1166-P2/EO* Rev.00 FUSELAGE FRAME BS727 STRINGER 18A OUTBOARD CHORD INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1166-P3/EO* Rev.00 FUSELAGE FRAME, BS727 OUTB CHORD AT STR 18A INSPECTION OPEN HOLE EDDY

CURRENT INSPECTIONOpen







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1173 SB 04 MANDATORY A/C FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION, REPAIR AND PREVENTIVE

MODIFICATIONClosed 21.Feb.2008

2000-05-29 (ACTIVE)37-SBB-53A1173 (REPETITIVE)737-53-1173 IN 06 (REF)737-53A1173-R0 (REF)737-53A1173-R1 (REF)737-53A1173-R2 (REF)737-53A1173-R3 (REF)737-53A1173-R4 (ACTIVE)SBB 737-53A1173 (MOD TASK)

ADTASBSBSBSBSBSBTA

Perform BEFORE 50000/C737-53A1173/SB Rev.04 FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION, REPAIR AND PREVENTIVE

MODIFICATIONClosed 21.Feb.2008

> 737-53A1173/EO* Rev.04 FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION CancelledPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

05.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150725 KKM 37-SBB-53A1173 BS 178BULKHEA

Reason for this StatusPREVENTIVE MODIFICATION PERFORMED ON EO 737-53A1173-01

> 737-53A1173-01/EO* Rev.04 *AD* FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION Closed 21.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1173-1 SB NO

TEMANDATORY A/C FUSELAGE - BODY STATION 178 BULKHEAD - REPAIR OF CENTER WEB Not Applicable

2000-05-29737-53-1173 IN 06737-53A1173737-53A1173 R1737-53A1173 R2737-53A1173 R3737-53A1173 R4

ADSBSBSBSBSBSB

Reason for this StatusSB 737-53A1173 C/W WO 151384

737-53A1173-2 SB NOTE

MANDATORY A/C FUSELAGE - BS 178 BULKHEAD - REPAIR OF VERTICAL CHORDS Not Applicable

2000-05-29737-53-1173 IN 06737-53A1173737-53A1173 R1737-53A1173 R2737-53A1173 R3737-53A1173 R4

ADSBSBSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1173-3 SB NO

TEMANDATORY A/C FUSELAGE - BS 178 BULKHEAD - REPAIR OF SIDE CHORD AREAS Not Applicable

2000-05-29737-53-1173 IN 06737-53A1173737-53A1173 R1737-53A1173 R2737-53A1173 R3737-53A1173 R4

ADSBSBSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1177 SB 07 MANDATORY A/C FUSELAGE - SKIN - REPAIR METHODS FOR CRACKS IN LOWER SKINS AT LAP JOINTS

AND WINDOW CORNERSOpen

This service bulletin describes inspection and repair methods forcracks in lower skins at lap joints and window corners. If the cracksin the lower skins at lap joints and window corners remainundetected, those cracks could grow large and cause a suddendecompression.

The compliance times for this SB is mandated by AD 2002-07-08.

NOTE:If earlier repair acc to SRM 53-00-01, Figure 227 is performed on lapjoints, between body station (BS) 259.5 and BS 1016, then AD2002-07-10 also mandates this SB to be performed.No A/C in current NAS 737-300 fleet is affected by AD 2002-07-10.(2013-09-16)2002-07-082002-07-10

ADAD

0000

This Document SUPERSEDES 737-53A1177/SB Rev.06Perform within an unlimited threshold.

737-53A1177/SB Rev.07 FUSELAGE - SKIN - REPAIR METHODS FOR CRACKS IN LOWER SKINS AT LAP JOINTSAND WINDOW CORNERS

Open

This Document SUPERSEDES 737-53A1177/SB Rev.06> 737-53A1177-01/EO* Rev.01 FUSELAGE - SKIN - LAP JOINTS MODIFICATION (REPAIR) Open

This Document SUPERSEDES 737-53A1177-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

50000/C Perform initially before(F) 50000/C> 737-53A1177-02/EO* Rev.00 FUSELAGE - SKIN - REPETITIVE LFEC INSP FOR AREAS OUTSIDE CROWN AREA Open







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1177-03/EO* Rev.00 FUSELAGE - SKIN - FOLLOW ON LFEC LAP JOINT INSPECTIONS Open


> 737-53A1177-04/EO* Rev.00 FUSELAGE - SKIN - INSPECTION -- WINDOW CORNERS OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> 737-53A1177-05/EO* Rev.00 FUSELAGE - SKIN - SB 737-53A1177 TABLE 10 WINDOW CORNERS INSPECTION OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> 737-53A1177-06/EO* Rev.00 FUSELAGE - SKIN - SB 737-53A1177 TABLE 11 WINDOW CORNERS INSPECTION OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> 737-53A1177-07/EO* Rev.00 FUSELAGE - SKIN - SB 737-53A1177 TABLE 16-18 BUTT JOINT INSPECTION OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> 737-53A1177-08/EO* Rev.00 FUSELAGE - SKIN - INSPECTION -- WINDOW CORNERS PROVENTIVE MODIFICATION Open






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1177 ->0/ SB 06 MANDATORY A/C *AD* TO FIND & FIX CRACKING OF CERTAIN FUSELAGE LAP JOINTS Superseded (Cancelled)

2002-07-08 (ACTIVE)37-SBB-53A1177P1 (REPETITIVE)37-SBB-53A1177P2 (REPETITIVE)37-SBB-53A1177P5 (REPETITIVE)737-53A1177-R1 (REF)737-53A1177-R2 (REF)737-53A1177-R3 (REF)737-53A1177-R4 (REF)737-53A1177-R5 (REF)737-53A1177-R6 (ACTIVE)737-53A1177-RO (REF)AMOC LETTER 120S-04-53SBB 737-53A1177 (MOD-TASK)

ADTATATASBSBSBSBSBSBSBDOCRTA

This Document has been SUPERSEDED BY 737-53A1177/SB Rev.07Perform BEFORE 50000/C

737-53A1177/SB Rev.06 *AD* TO FIND & FIX CRACKING OF CERTAIN FUSELAGE LAP JOINTS CancelledThis Document has been SUPERSEDED BY 737-53A1177/SB Rev.07

> 737-53A1177-01/EO* Rev.00 *AD* TO FIND & FIX CRACKING OF CERTAIN FUSELAGE LAP JOINTS CancelledThis Document has been SUPERSEDED BY 737-53A1177-01/EO Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-53A1177P1/EO* Rev.06 *AD* FUSELAGE - CRACKS IN LOWER SKINS AT LAP JOINTS INSIDE **REPETITIVEHIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION**

Cancelled

Reason for this StatusDUE TO NEW SETUP AND REVISION 7 OF SB 53A1177

> 737-53A1177P2/EO* Rev.06 *AD* FUSELAGE - CRACKS IN LOWER SKINS AT LAP JOINTS OUTSIDE **REPETITIVEHIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION**

Cancelled






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1177P5/EO* Rev.06 *AD* INSP. FOR CRACKING OF LOWER SKIN AT LOWER ROW OF FASTE IN THE LAP

JOINTS - WINDOW CORNERS.Cancelled


737-53A1188 SB 02 MANDATORY A/C *AD* FR BS303.9,WEB CRACKS, HOLES FOR DOOR STOP FITT STRAP Superseded (Not Applicable bySerial Number)

2008-17-03 (ACTIVE)737-53-1188 (REF)737-53-1188 R1 (REF)737-53A1188 IN 02 (REF)737-53A1188 R2 (ACTIVE)737-SRP-53-149 (REF)PRODUCTION PRR 35005-246RSSBB 737-53A1188 (MAINT TASK)

ADSBSBSBSBSRPPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1188 SB 03 MANDATORY A/C FUSELAGE - BODY STATION 303.9 FRAME - WEB CRACKS AT HOLES FOR DOOR STOP

INTERCOSTAL STRAP AT STRINGERS 15 AND 16 LEFT -Not Applicable

Revision adds AC LN# 2766 through 3132 to the effectivity. These areGroup 2 AC.NAS has no Group 1 AC (2350,2438-2765).2008-17-03737-53A1188737-53A1188737-53A1188

ADSBSBSB

00000102

This Document SUPERSEDES 737-53A1188/SB Rev.02737-53A1188/SB Rev.03 FUSELAGE - BODY STATION 303.9 FRAME - WEB CRACKS AT HOLES FOR DOOR STOP

INTERCOSTAL STRAP AT STRINGERS 15 AND 16 LEFT -Not Applicable

This Document SUPERSEDES 737-53A1188/SB Rev.02> 737-53A1188-01/EO* Rev.00 FUSELAGE - BODY STATION 303.9 FRAME - WEB CRACKS AT HOLES FOR DOOR STOP

INTERCOSTAL STRAP AT STRINGERS 15 AND 16 LEFT -Not Applicable by Serial Number





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1197 SB 02 MANDATORY A/C *AD* FUSE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 Closed 18.Feb.2008

2008-17-03 (ACTIVE)37-SBB-53A1197 (REPETITIVE)737-53A1197-R0 (ACTIVE)PRR35005-246RS PRR35328-RSBB 737-53A1197 (MOD-TASK)

ADTASBPRRTA

Perform within an unlimited threshold.737-53A1197/SB Rev.02 *AD* FUSE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 Closed 18.Feb.2008> 737-53A1197/EO* Rev.00 FUSELAGE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 L/H Cancelled


18.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151168 KKM 37-SBB-53A1197 BS303.9FRAME

Reason for this StatusPREVENTIVE MODIFICATION PERFORMED ON EO 737-53A1197-01

> 737-53A1197-01/EO* Rev.00 *AD* FUSE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 Closed 07.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1200 SB 02 MANDATORY A/C FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARD

GALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUTRepetitive

This Document SUPERSEDES 737-53A1200/SB Rev.00This Document SUPERSEDES 737-53A1200/SB Rev.01Perform within an unlimited threshold.

737-53A1200/SB Rev.02 FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARDGALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUT

Repetitive

This Document SUPERSEDES 737-53A1200/SB Rev.00This Document SUPERSEDES 737-53A1200/SB Rev.01

> 737-53A1200-01/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Closed 07.Jul.2011

This Document SUPERSEDES 737-53A1200-1/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

07.Jul.2011 54542:00/H 30315/C

Was due at: 48315/C PerfRev.:'00' PERFPERMANENT REP ON FWD ENTRYDOOR UPPER HINGE ACC SR1-748133531 AND FAA 8100-9

Reason for this StatusPERF PERMANENT REP ON FWD ENTRY DOOR UPPER HINGE ACC SR 1-748133531 ANDFAA 8100-9

> 737-53A1200-02/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY LOWERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive

This Document SUPERSEDES 737-53A1200-1/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

48315/C

Perform initially within (effective from25.Jun.2008) (L) 3000/C Perform initiallywithin (effective from 25.Jun.2008) (L)20000/C / Interval(F):18000/C






24.Oct.2014/411


07.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151169 KKM 37-SBB-53A1200-1 HINGECUTOUT

> 737-53A1200-03/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 3 AIRPLANES


This Document SUPERSEDES 737-53A1200-2/EO Rev.00> 737-53A1200-04/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY LOWER

HINGE CUTOUT INSPECTION. GROUP 3 AIRPLANESNot Applicable by Serial Number

This Document SUPERSEDES 737-53A1200-2/EO Rev.00> 737-53A1200-05/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER


This Document SUPERSEDES 737-53A1200-3/EO Rev.00> 737-53A1200-06/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY LOWER


This Document SUPERSEDES 737-53A1200-3/EO Rev.00> 737-53A1200-07/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPER

HINGE CUTOUT INSPECTION. GROUP 2 AIRPLANESRepetitive

This Document SUPERSEDES 737-53A1200-4/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

48315/C

Perform initially within (effective from22.Apr.2014) (L) 3000/C Perform initiallywithin (effective from 22.Apr.2014) (L)20000/C / Interval(F):18000/C



> 737-53A1200-08/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY LOWERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive

This Document SUPERSEDES 737-53A1200-4/EO Rev.00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

48315/C

Perform initially within (effective from22.Apr.2014) (L) 3000/C Perform initiallywithin (effective from 22.Apr.2014) (L)20000/C / Interval(F):18000/C



> 737-53A1200-09/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANES


This Document SUPERSEDES 737-53A1200-5/EO Rev.00> 737-53A1200-10/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY LOWER

HINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANESNot Applicable by Serial Number


737-53A1200 SB 01 RECOMMENDED A/C FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARDGALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUT







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1200 SB 00 MANDATORY A/C *AD* ENTRY & GALLEY DOORWAY, FWD. UPPET & LOWER HINGE CUTOUT Superseded (Taskcard Controlled)

2008-11-04 (ACTIVE)37-NAS-5312-001 (REPET)37-SBB-53A1200-1 (REPET)37-SBB-53A1200-2 (REPET)37-SBB-53A1200-3 (REPET)37-SBB-53A1200-4 (REPET)37-SBB-53A1200-5 (REPET)737-53A1200-R0 (ACTIVE)737-SRP-53-0134 (REF)

ADTATATATATATASBSRP


737-53A1200/SB Rev.00 *AD* ENTRY & GALLEY DOORWAY, FWD. UPPET & LOWER HINGE CUTOUT Taskcard ControlledThis Document has been SUPERSEDED BY 737-53A1200/SB Rev.02

> 737-53A1200-1/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Superseded

This Document has been SUPERSEDED BY 737-53A1200-01/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-02/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks


Reason for this StatusAMICOS WO 151169 KKM 37-SBB-53A1200-1 HINGE CUTOUT INSP, ATCL REF MRC



This Document has been SUPERSEDED BY 737-53A1200-03/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-04/EO Rev.00



This Document has been SUPERSEDED BY 737-53A1200-05/EO Rev.00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusThis Document has been SUPERSEDED BY 737-53A1200-06/EO Rev.00

> 737-53A1200-4/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Cancelled

This Document has been SUPERSEDED BY 737-53A1200-07/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-08/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks


Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-53A1200-5/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANES


This Document has been SUPERSEDED BY 737-53A1200-09/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-10/EO Rev.00

> 737-53A1200MPD/EO* Rev.00 737-53A1200MPD CONTROLLED BY MPD TASKS Taskcard ControlledReason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1204 SB 01 MANDATORY A/C *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - NDT INSPECTION Cancelled

Subject SB is in compliance with AD 2012-12-05 Paragraph (p) and (q).2005-20-03 (SUPERSEDED)2009-16-14 (ACTIVE)37-SBB-53A1204 (REPETITIVE)737-53-1204 IN 01 (REF)737-53-1204-R0 (REF)737-53A1204-R1 (ACTIVE)737-53A1240-R0 (REF)737-SL-53-087 (REF)737-SRP-53-0266 (REF)PRODUCTION MRR3537-1153WARRANTY AS OF SEP 11, 1997

ADADTASBSBSBSBSLSRPPRRSB

Perform within an unlimited threshold.737-53A1204/SB Rev.01 *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - NDT INSPECTION Cancelled> 737-53A1204/EO* Rev.01 NDT - INTERCOASTALS - BS360 & 294.5 S-6/17L - INTERNAL NDT INSPECTION

REPETITIVE INSPECTIONCancelled

This Document has been SUPERSEDED BY 737-53A1204-01/EO Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Jul.2011 64534:00/H 37798/C 205164, N/A Was due at: 38852/C PerfRev.:'01'Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1204 SB 02 MANDATORY A/C *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - NDT INSPECTION Repetitive

SB in compliance with AD 2012-12-05 Paragraph (k).2012-12-05737-53A1204-R1 (ACTIVE)737-SL-53-087 (REF)737-SRP-53-0266 (REF)PRODUCTION MRR3537-1153WARRANTY AS OF SEP 11, 1997

ADSBSLSRPPRRSB

00

Perform within an unlimited threshold.737-53A1204/SB Rev.02 *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - NDT INSPECTION Repetitive> 737-53A1204-01/EO* Rev.02 *AD* NDT - INTERCOASTALS - BS360 & 294.5 S-6/17L - INTERNAL NDT INSP. REPETITIVE

INSPECTIONRepetitive / Special Text: Group 1.

This Document SUPERSEDES 737-53A1204/EO Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1208 SB 01 MANDATORY A/C *FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable

This document is applicable to LN# 2738-3071. All other LN# are NotApplicable per Boeing SB.

Compliance:AD § (a) and (b) is covered by EO 737-53A1208AD § (c) is covered by EO 737-53A1208-012001-02-01737-53A1208737-53A1208-01

ADEOEO

000101

737-53A1208/SB Rev.01 *FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable> 737-53A1208/EO* Rev.01 FUSELAGE - BODY STATION 178 BULKHEAD INSPECTION AND RE Not Applicable by Serial Number

This Document is terminated with implementation of 737-53A1208-01/EO Rev.01> 737-53A1208-01/EO* Rev.01 FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable by Serial Number

This Document terminates 737-53A1208/EO Rev.01

737-53A1208-2 SB NOTE

MANDATORY A/C FUSELAGE - BODY STATION 178 BULKHEAD REPAIR Not Applicable by Serial Number

2001-02-01737-53A1208737-53A1208 R1

ADSBSB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1210 SB 03 MANDATORY A/C *AD* FUSELAGE SKIN CHEM-MILL LINE CRACK INSPECTION/REPAIR Open

2013-18-08737-53A1210-R0 (REF)737-53A1210-R1 (REF)737-53A1210-R2 (REF)737-53A1210-R3 (ACTIVE)737-53A1210P7 (PREVENTIVEMOD)737-SRP-53-0281 (REF)

ADSBSBSBSBSBSRP

00

Perform within an unlimited threshold.737-53A1210/SB Rev.03 *AD* FUSELAGE SKIN CHEM-MILL LINE CRACK INSPECTION/REPAIR Open> 737-53A1210-P1/EO* Rev.03 *AD* FUSELAGE SKIN - CROWN AREA SKIN INSPECTION Repetitive


44951/C 556938Perform initially before(F) 35000/C /Interval(F):1800/C


> 737-53A1210-P2/EO* Rev.03 *AD* FUSELAGE SKIN - WINDOW BELT INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

44951/C Interval(F):1800/CPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks07.Feb.2014 71572:00/H 43151/C 489232, N/A Was due at: 44372/C PerfRev.:'03'

> 737-53A1210-P3/EO* Rev.03 *AD* FUSELAGE SKIN CHEM-MILL LINE- VERTICAL CRACK INSP RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

44951/CPerform initially before(L) 55000/H Performinitially within (effective from 06.Nov.2013)(L) 1800/C or 55000/C / Interval(F):1800/C






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1210-P4/EO* Rev.03 *AD* FUSELAGE SKIN CHEM-MILL LINE - LOWER LOBE AREA SECTION 41 -

INSPECTION.Repetitive




> 737-53A1210-P5/EO* Rev.00 *AD* FUSELAGE SKIN - PERMANENT REPAIR On Attrition> 737-53A1210-P6/EO* Rev.00 *AD* FUSELAGE SKIN - TIME LIMITED REPAIR On Attrition> 737-53A1210P7/EO* Rev.03 PREVENTIVE MOD: FUSELAGE SKIN CHEM-MILL LINE CRACK AFFECTS AREA AT

BS500D - BS520.Not Applicable by Serial Number





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1214 SB 02 MANDATORY A/C *AD* BS 10016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Superseded (Closed 13.Nov.2012)

37-SBB-53A1214-1A (REP TASK)37-SBB-53A1214-1F (REP TASK)37-SBB-53A1214-3 (REP TASK)737-53A1214-R0 (REF)737-53A1214-R1 (REF)737-53A1214-R2 (ACTIVE)99-08-23 (ACTIVE)SBB 737-53A1214 (MAINT TASK)

TATATASBSBSBADTA

This Document has been SUPERSEDED BY 737-53A1214/SB Rev.03Perform BEFORE 25750/C

737-53A1214/SB Rev.02 *AD* BS 10016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Closed 13.Nov.2012This Document has been SUPERSEDED BY 737-53A1214/SB Rev.03

> 737-53A1214-01/EO* Rev.00 BS 1016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Closed 16.Feb.2002Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

16.Feb.2002DELIVERYDOC.

> 737-53A1214-1A/EO* Rev.00 NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R AFT *** MANDATORYREPETITIVE NDT INSPECTION AFT SIDE ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1214-1A1/EO Rev.00This Document has been SUPERSEDED BY 737-53A1214-1A2/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Nov.2012 68139:00/H 40570/C 354128, N/A Was due at: 41126/C PerfRev.:'00'Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-53A1214-1F/EO* Rev.00 NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R FWD *** MANDATORYREPETITIVE NDT INSPECTION FWD SIDE ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1214-1F1/EO Rev.00This Document has been SUPERSEDED BY 737-53A1214-1F2/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks





24.Oct.2014/411


24.Mar.2010 60867:00/H 35008/CPerfRev.:'NOTE' / Reason: AMICOS WO510114 2-INSPHEAVY-SERV-12YR/SI/CPCP.NA

Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-53A1214-3/EO* Rev.00 NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R *** MANDATORYREPETITIVE NDT INSPECTION AFT SIDE ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1214-3A/EO Rev.00This Document has been SUPERSEDED BY 737-53A1214-3F/EO Rev.00Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1214 SB 04 MANDATORY A/C FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB CRACKS

INSPECTION AND REPAIROpen

SB 737-53A1214 is dived into ten Engineering Orders for compliance.1999-08-232008-09-132012-18-13737-53-1123737-53A1075

ADADADSBSB

0000000003


737-53A1214/SB Rev.04 FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB CRACKSINSPECTION AND REPAIR

Open

This Document SUPERSEDES 737-53A1214/SB Rev.03> 737-53A1214-1A1/EO* Rev.00 PART I - NDT INSP OF WEB AT "Y" CHORD - S-5L TO 7L AND S-5R TO 9R FROM AFT Repetitive

This Document SUPERSEDES 737-53A1214-1A/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks03.Dec.2013 71211:00/H 42863/C 490746, N/A Was due at: 42940/C PerfRev.:'00'

> 737-53A1214-1A2/EO* Rev.00 PART I - NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R EXCEPT S-5L TO 7LAND S-5R TO 9R. FROM AFT.

Repetitive

This Document SUPERSEDES 737-53A1214-1A/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



29.Jun.2012 67212:00/H 39926/C N/APerfRev.:'00' / Reason: Initialized: Last perf.with 737-53A1214-1A/EO/00

> 737-53A1214-1F1/EO* Rev.00 PART I - NDT INSP OF WEB AT "Y" CHORD - S-5L TO 7L AND S-5R TO 9R FROMFORWARD

Repetitive





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-53A1214-1F/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> 737-53A1214-1F2/EO* Rev.00 PART I -NDT INSPECTION OF WEB AT "Y" CHORD -ABOVE S-15L/R EXCEPT S-5L TO 7LAND S-5R TO 9R. FROM FORWARD.

Repetitive

This Document SUPERSEDES 737-53A1214-1F/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> 737-53A1214-2/EO* Rev.00 PART II - DETAILED INSPECTION FOR OIL-CANNING FROM AFT RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

47740/CPerform initially within (effective from24.Oct.2012) (L) 1200/C /Interval(F):6000/C


> 737-53A1214-3A/EO* Rev.00 PART III - NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R FROM AFT OpenThis Document SUPERSEDES 737-53A1214-3/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

55151/C 489483Perform initially within (effective from24.Oct.2012) (F) 6000/C or 730/D /Interval(F):6000/C

> 737-53A1214-3F/EO* Rev.00 PART III - NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R FROM FWD. RepetitiveThis Document SUPERSEDES 737-53A1214-3/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document





24.Oct.2014/411


55151/CPerform initially within (effective from24.Oct.2012) (F) 6000/C or 730/D /Interval(F):12000/C


14.Feb.2014 71572:00/H 43151/C 489480, N/AWas due at: 46563/C and 24.Oct.2014PerfRev.:'00'

> 737-53A1214-4/EO* Rev.00 PART IV - NDT INSPECTION OF THE DOME CAP AT THE CENTER OF THE BULKHEADFROM AFT

Repetitive





> 737-53A1214-5/EO* Rev.00 PART V -NDT INSP OF FWD FLANGE OF THE "Z" STIFFENERS AT THE DOME CAPFROM FWD

Repetitive





> 737-53A1214-6/EO* Rev.00 PART VI - DETAILED INSPECTION FOR EXISTING REPAIRS ON THE BULKHEAD FROMAFT

Closed 03.Feb.2014 W/O:489479






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1225 SB 01 MANDATORY A/C *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Repetitive

2007-03-03 (ACTIVE)37-SBB-53A1225 (REPETITIVE)737-53A1225-R0 (REF)737-53A1225-R1 (ACTIVE)737-SRP-53-0126 (REF)SBB 737-53A1225 (MOD-TASK)

ADTASBSBSRPTA

Perform BEFORE 50000/C737-53A1225/SB Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Repetitive> 737-53A1225/EO* Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD - CRAC Repetitive

This Document is terminated with implementation of 737-53A1225-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

05.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150786 KKM 37-SBB-53A1225 STA 178BEAM I

Reason for this StatusAMICOS WO 150786 KKM 37-SBB-53A1225 STA 178 BEAM INSP -ATC

> 737-53A1225-01/EO* Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Closed 21.Feb.2008This Document terminates 737-53A1225/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-53A1225-1/EO* Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/REPAIR CancelledReason for this StatusPERMANENT MODIFICATION PERFORMED, REF EO 737-53A1225-01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1228 SB 00 MANDATORY A/C *AD* CARGO DOOR CUTOUT, SKIN, BEARSTRAP AND FRAME INSPECTION Open

2005-07-19 (ACTIVE)37-NAS-5313-001 (REPETITIVE)37-NAS-5313-002 (REPETITIVE)37-NAS-5313-003 (REPETITIVE)37-SBB-53A1228-1 (REPETITIVE)37-SBB-53A1228-2 (REPETITIVE)737-53A1228 IN01 (REF)737-53A1228-R0 (ACTIVE)737-SRP-53-0128 (REF)

ADTATATATATASBSBSRP

Perform within an unlimited threshold.737-53A1228/SB Rev.00 *AD* CARGO DOOR CUTOUT, SKIN, BEARSTRAP AND FRAME INSPECTION Open> 737-53A1228-1/EO* Rev.00 *AD* FORWARD CARGO CUTOUT/DOORWAY - SKIN, BEARSTRAP & FRAME IAW SB

COMPLIANCE TABLE 1 & 2.Repetitive




> 737-53A1228-2/EO* Rev.00 *AD* AFT CARGO CUTOUT/DOORWAY - SKIN, BEARSTRAP & FRAME INS IAW SBCOMPLIANCE TABLES 1 & 3.

Repetitive




> 737-53A1228MPD/EO* Rev.00 ADDITIONAL INSPECTION CONTROLLED BY MAINTENANCE TASK Taskcard Controlled / Special Text:Repaired after findings from SB -Additional inspection required.

Carried out on the following TaskcardsTaskcard: NAS-5313-006 Maint. Progr.: AMP 737-CL





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks22.10.2015 47151/C 2'656/C Interval:4000/CPerf Dim1 (D) Perf Dim2 Perf Dim313.02.2014 71572:00/H 43151/CReason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1234 SB 02 MANDATORY A/C FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS - INSPECTION AND REPAIR Not Applicable





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusR2: All inspections changed to NDT. Thresholds and intervalsshortened. Area increased.

Service Bulletin 737-53A1234-R2.C. ReasonRevision 2 is sent to add additional inspections for horizontalchem-mill cracks away from the lap joints over the entire crown, newinspections for vertical chem-mill cracks adjacent to the butt jointsand adding internal tear strap doublers at the tear strap adjacent tonew and existing permanent repairs.

F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.

If an airplane has a non-Boeing modification or repair that affects acomponent or system also affected by this service bulletin, theoperator is responsible for obtaining appropriate regulatory agencyapproval before incorporating this service bulletin.

In addition, the Manager of the FAA Seattle Aircraft CertificationOffice approves the inspections and repairs defined in this servicebulletin as an alternative method of compliance to the inspections andrepairs required by paragraphs (g), (h) and (i) of FAA AD 2005-13-27.All provisions of FAA AD 2005-13-27 that are not specifically





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Statusreferenced in the above statement remain fully applicable and mustbe complied with.2005-13-272012-26-02737-53-1234-R0737-53-1234-R1737-53A1234-AMOC-01

ADADSBSBSB

0000000000

This Document SUPERSEDES 737-53-1234/SB Rev.01737-53A1234/SB Rev.02 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS - INSPECTION AND REPAIR Not Applicable

This Document SUPERSEDES 737-53-1234/SB Rev.01> 737-53A1234-01/EO* Rev.01 NDT FUSELAGE SKINS S-10L/R FIG 2 - MFEC INSP FOR CRACKS AT CHEM-MILLED

STEPS. FIGURE 2 - THRESHOLD 25000 FC.Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-01/EO Rev.00> 737-53A1234-02/EO* Rev.01 NDT FUSELAGE SKINS S-10L/R FIG 2 - UTPA INSP FOR CRACKS AT CHEM-MILLED

STEPS. LAP JOINTS. - THRESHOLD 25000 FC.(NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-02/EO Rev.00> 737-53A1234-03/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 11 - MFEC INSP FOR CRACKS AT CHEM-MILLED

STEPS. LAP JOINTS. THRESHOLD 28000 FC.Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-03/EO Rev.00> 737-53A1234-04/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 11 - UTPA INSP FOR CRACKS AT CHEM-MILLED

STEPS. LAP JOINTS. THRESHOLD 28000 FC. (NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-04/EO Rev.00> 737-53A1234-05/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 16 - MFEC INSP FOR CRACKS AT CHEM-MILLED

STEPS LAP JOINTS. THRESHOLD 42000 FC.Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-05/EO Rev.00> 737-53A1234-06/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 16 - UTPA INSP FOR CRACKS AT CHEM-MILLED

STEPS LAP JOINTS. THRESHOLD 42000 FC.(NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-06/EO Rev.00> 737-53A1234-07/EO* Rev.01 NDT FUSELAGE SKINS S-6/9L & 6/9R FIG 20 - MFEC INSP FOR CRACKS AT

CHEM-MILLED STEPS - SHEAR WRINKLE AREAS- - THRESHOLD 33000 FC.Not Applicable by Serial Number






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1234-08/EO* Rev.01 NDT FUSELAGE SKINS S-6/9L & 6/9R FIG 20 - UTPA INSP FOR CRACKS AT

CHEM-MILLED STEPS-SHEAR WRINKLE AREAS-THRESHOLD 33000 FC.(NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-08/EO Rev.00> 737-53A1234-09/EO* Rev.00 PERMANENT SKIN REPAIR AT S-10 ABOVE LAP SPLICE. Not Applicable by Serial Number> 737-53A1234-10/EO* Rev.00 FUSELAGE CROWN SKINS - NDT INSP FOR VERTICAL CHEM-MILL CRACKING AT

SPECIFIED LOCATIONS- FIGURE 24 - 1800 FC/FH INTERVALNot Applicable by Serial Number

> 737-53A1234-12/EO* Rev.00 FUSELAGE SKIN NDT INSP AT CHEM-MILL STEPS IN GEN POCKET-TO-POCKET AREAS10L TO S-10R STA 360 TO STA 1016- FIGURE 28 - 500 FC INTERVAL


> 737-53A1234-14/EO* Rev.00 FUSELAGE SKIN NDT INSP AT CHEM-MILL STEPS IN GEN POCKET-TO-POCKET AREASTA259.5 TO STA360 S-4L TO S-4R - FIGURE 33 - 500 FC/FH INTERVAL


737-53A1240 SB 01 MANDATORY A/C *AD* FUSELAGE - FRAME BS 348.5 S-14/16L - INTERNAL NDT INSPECTION RepetitiveSubject SB is in compliance with AD 2012-12-05 Paragraph (p) and (q).2012-12-05737-53A1204737-53A1240 R0737-53A1240 R1

ADSBSBSB

00

Perform BEFORE 15000/C for the first timeThereafter perform in an interval of 6000/C

737-53A1240/SB Rev.01 *AD* FUSELAGE - FRAME BS 348.5 S-14/16L - INTERNAL NDT INSPECTION Repetitive> 737-53A1240/EO* Rev.01 *AD* NDT - FUSELAGE - FRAME BS 348.5 S-14/16L - INTERNAL NDT INSP. Repetitive / Special Text: Group 3.








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1241 SB 01 RECOMMENDED A/C FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 328 FRAME INSPECTIONS

STRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUTOpen


737-53A1241/SB Rev.01 FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 328 FRAME INSPECTIONSSTRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUT

Open

This Document SUPERSEDES 737-53A1241/SB Rev.00> 737-53A1241-01/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEADS - STA 291.5 FRAME WEB INSPECTIONS

AROUND STR 16R - FORWARD GALLEY DOOR CUTOUTRepetitive


47651/C Interval(F):4500/CPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks06.Feb.2014 71572:00/H 43151/C 489487, N/A Was due at: 45070/C PerfRev.:'00'

> 737-53A1241-02/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 291.5 FRAME INSPECTIONSSTRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUT

Open


46238/CPerform initially before(L) 30000/C Performinitially within (effective from 11.Jun.2013)(L) 4500/C / Interval(F):9000/C

> 737-53A1241-03/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 328 FRAME INSPECTIONSSTRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUT

Open


46238/CPerform initially before(L) 30000/C Performinitially within (effective from 11.Jun.2013)(L) 4500/C / Interval(F):9000/C





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1241 SB 00 MANDATORY A/C *AD* FWD GALLEY DOOR CUTOUT FR. INSP. STA 291.5, STRING.16R Superseded (Cancelled)

2005-07-12 (ACTIVE)37-SBB-53A1241 (REPETITIVE)737-53A1241-R0 (ACTIVE)

ADTASB


737-53A1241/SB Rev.00 *AD* FWD GALLEY DOOR CUTOUT FR. INSP. STA 291.5, STRING.16R CancelledThis Document has been SUPERSEDED BY 737-53A1241/SB Rev.01

> 737-53A1241/EO* Rev.00 *AD*FWD GALLEY DOOR COUTOUT, STA 291.5 FRAME INSP AT STR 16R ***MANDATORY REPETITIVE DETAILED & NDT INSPECTION ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1241-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks02.Nov.2012 68139:00/H 40570/C 273627, N/A Was due at: 42298/C PerfRev.:'00'Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1254 SB 02 MANDATORY A/C FUSELAGE - BODY FRAME AND OVERWING STUB BEAM INSPECTION AND REPAIR

BODY STATIONS 597 TO 639Repetitive

2010-25-06737-SRP-53-0182NAS-5311-001NAS-5311-002

ADSRPTATA

00LATELATELATE

This Document SUPERSEDES 737-53-1182/SB Rev.02This Document SUPERSEDES 737-53A1254/SB Rev.01Perform within an unlimited threshold.

737-53A1254/SB Rev.02 FUSELAGE - BODY FRAME AND OVERWING STUB BEAM INSPECTION AND REPAIRBODY STATIONS 597 TO 639

Repetitive

This Document SUPERSEDES 737-53-1182/SB Rev.02This Document SUPERSEDES 737-53A1254/SB Rev.01

> 737-53A1254-01/EO* Rev.02 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 597 TO 639 RepetitiveThis Document SUPERSEDES 737-53A1254/EO Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1254 SB 01 MANDATORY A/C FUSELAGE - BODY FRAME AND OVERWING STUB BEAM INSPECTION AND REPAIR

BODY STATIONS 597 TO 639Superseded (Cancelled)

37-NAS-5311-001 (REPETITIVE)37-NAS-5311-002 (REPETITIVE)37-SBB-53A1254 (REPETITIVE)737-53A1254 IN 01 (REF)737-53A1254-RO (ACTIVE)737-SRP-53-0182 (REF)

TATATASBSBSRP

This Document SUPERSEDES 737-53A1254/SB Rev.00This Document has been SUPERSEDED BY 737-53A1254/SB Rev.02Perform within an unlimited threshold.

737-53A1254/SB Rev.01 FUSELAGE - BODY FRAME AND OVERWING STUB BEAM INSPECTION AND REPAIRBODY STATIONS 597 TO 639

Cancelled


> 737-53A1254/EO* Rev.01 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 597 TO 639 CancelledThis Document SUPERSEDES 737-53A1254/EO Rev.00This Document has been SUPERSEDED BY 737-53A1254-01/EO Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks31.Oct.2012 68139:00/H 40570/C 273628, N/A Was due at: 42298/C PerfRev.:'01'Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1254 SB 00 RECOMMENDED A/C BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 616 & 639 Superseded (Superseded)

37-NAS-5311-001 (REPETITIVE)37-NAS-5311-002 (REPETITIVE)37-SBB-53A1254 (REPETITIVE)737-53A1254 IN 01 (REF)737-53A1254-RO (ACTIVE)737-SRP-53-0182 (REF)

TATATASBSBSRP


737-53A1254/SB Rev.00 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 616 & 639 SupersededThis Document has been SUPERSEDED BY 737-53A1254/SB Rev.01

> 737-53A1254/EO* Rev.00 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 616 & 639 CancelledThis Document has been SUPERSEDED BY 737-53A1254/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks


Reason for this StatusManually deassigned after Document Cancelled/Superseeded

> 737-53A1254MPD/EO* Rev.00 737-53A1254MPD CONTROLLED BY MPD TASKS SupersededThis Document has been SUPERSEDED BY 737-53A1254MPD/EO Rev.01Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1255 SB 00 MANDATORY A/C FUSELAGE, CROWN SKIN LAP JOINT INSPECTION FOR CRACKING Superseded (Cancelled)

This mod is applicable to LN# 1-2552.2003-08-15 (ACTIVE)737-53A1255-R0 (ACTIVE)AD 2003-08-15 (SEC-TASK)SBB 737-53A1255 (INSP-TASK)

ADSBTATA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1255 SB 02 MANDATORY A/C FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Open / Special Text: Group 5serialnumbers


737-53A1255/SB Rev.02 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKINGAT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908

Open / Special Text: Group 5serialnumbers

This Document SUPERSEDES 737-53A1255/SB Rev.01> 737-53A1255-01/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Closed 12.Feb.2014 W/O:489216

This Document is terminated with implementation of 737-53A1255-03/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

12.Feb.2014 71572:00/H 43151/C 489216, N/AWas due at: 43445/C PerfRev.:'00' / Reason:Document terminated manually.

Reason for this StatusDocument terminated manually.

> 737-53A1255-02/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKINGAT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908


This Document is terminated with implementation of 737-53A1255-04/EO Rev.00> 737-53A1255-03/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Closed 14.Feb.2014 W/O:489486

This Document terminates 737-53A1255-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Feb.2014 71572:00/H 43151/C 489486, N/A Was due at: 45000/C PerfRev.:'00'



This Document terminates 737-53A1255-02/EO Rev.00> 737-53A1255-05/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Open / Special Text: post EO737-53A1255-03






24.Oct.2014/411


45651/CPerform initially within (effective from13.Jun.2013) (F) 2500/C /Interval(F):2500/C



737-53A1255 SB 01 MANDATORY A/C FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKINGAT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908



737-53A1261 SB 00 MANDATORY A/C *AD* FRAME&BULK:UPPER FRAME TO SIDE FRAME SPLICE INSP & MOD OpenThis mod is applicable to LN# 1-1919.2008-13-12 (ACTIVE)2008-13-12 R1 (ACTIVE)37-SBB-531261 (REPETITIVE)737-53A1261 (REF.)SBB 737-53A1261 (TERMINATING)

ADADTASBTA

Perform within an unlimited threshold.737-53A1261/SB Rev.00 *AD* FRAME&BULK:UPPER FRAME TO SIDE FRAME SPLICE INSP & MOD Open> 737-53A1261/EO* Rev.00 FRAMES AND BULKHEAD - UPPER FRAME TO SIDE FRAME SPLICE INSP REPETITIVE

INSP.Repetitive




> 737-53A1261-01/EO* Rev.00 *AD* FRAME&BULK:UPPER FRAME TO SIDE FRAME SPLICE MODIFICATION. Term.Action openDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1262-1 SB 03 MANDATORY A/C FUSELAGE SKIN - INSPECTION FOR SCRIBE LINES - ZONE 1 Closed 20.Feb.2008

Service Bulletin 737-53A1262-R3.F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/ JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.


This service bulletin has been reviewed with respect to therequirements of AD 98-11-04 R1, Paragraph (g), and the inspections donot affect a SSI. However, any repair that results from theinspection findings of this service bulletin, should be assessed withrespect to the requirements of AD 98-11-04 R1, paragraph (g), todetermine if it affects or creates a SSI.

This service bulletin has been approved by the FAA. In addition, theManager of the FAA Seattle Aircraft Certification Office approves theinspections defined in this service bulletin as an alternativemethod of compliance to the requirements of paragraph (f), (g), (j),(l), (m), (n) and (q) of AD 2006-07-12. All provisions of AD2006-07-12 that are not specifically referenced in the abovestatement remain fully applicable and must be complied with.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status2006-07-12 (SUPERSEDED)2010-05-13 (REF)2010-05-13-SUB1 (ACTIVE)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2010-05-13SUB1 (SEC-TASK)SBB 737-53A1262-1 (ACTIVE)SBB 737-53A1262-1 (MAIN-TASK)

ADADADSBSBSBSBTASBTA




737-53A1262-1/SB* Rev.03 FUSELAGE SKIN - INSPECTION FOR SCRIBE LINES - ZONE 1 Closed 20.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-53A1262-1-01/EO* Rev.00 LN-KKB. FUSELAGE SKIN - LAP JOINT S-4L & 4R BS 360-1016. REPEAT EXTERNAL NDTINSPECTION OF SCRIBE LINES. UT PHASED ARRAY.


This Document is terminated with implementation of 737-53A1262-1-02/EO Rev.00> 737-53A1262-1-02/EO* Rev.00 LN-KKB. FUSELAGE SKIN - LAP JOINT S-4L & 4R BS 360-1016. REPEAT EXTERNAL NDT

INSPECTION OF SCRIBE LINES. UT PHASED ARRAY.Not Applicable by Serial Number

This Document terminates 737-53A1262-1-01/EO Rev.00> 737-53A1262-1-03/EO* Rev.00 LN-KKB. FUSELAGE SKIN - BUTT JOINT BS360 & 907 S-10L-10R. REPEAT EXTERNAL

NDT INSPECTION OF SCRIBE LINES.Not Applicable by Serial Number

> 737-53A1262-1-04/EO* Rev.00 LN-KKB. FUSELAGE SKIN - WING TO BODY FAIRINGS - S-14L BS 907-1016 EXTERNALREPAIR AT BS 920 S-19L. REPEAT NDT INSPECTION OF SCRIBE LINES






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1262-1-05/EO* Rev.00 LN-KKB. FUSELAGE SKIN LAP JOINT S4L & 4R BS 360-1016. ONE TIME INTERNAL NDT

INSPECTIONNot Applicable by Serial Number

> 737-53A1262-1-06/EO* Rev.00 LN-KKB. FUSELAGE SKIN LAP JOINT S-4L & 4R SCRIBE LINES REPAIR Not Applicable by Serial Number

737-53A1262-2 SB 03 MANDATORY A/C FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 2 Open2006-07-12 (SUPERSEDED)2010-05-13 (REF)2010-05-13SUB2 (ACTIVE)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2010-05-13SUB2 (SEC-TASK)SBB 737-53A1262-2 (ACTIVE)SBB 737-53A1262-2 (MAIN-TASK)







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1262-3 SB 02 MANDATORY A/C *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 3 Open

2006-07-12 (SUPERSEDED)2010-05-13 (REF)2010-05-13SUB3 (ACTIVE)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2010-05-13SUB3 (SEC-TASK)SBB 737-53A1262-3 (ACTIVE)SBB 737-53A1262-3 (INSP-TASK)



737-53A1262-4 SB 03 MANDATORY A/C *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 4 Open2006-07-12 (SUPERSEDED)2010-05-13 (REF)2010-05-13SUB4 (ACTIVE)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2010-05-13SUB4 (SEC-TASK)SBB 737-53A1262-4 (ACTIVE)SBB 737-53A1262-4 (MAIN-TASK)







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1262-5 SB 03 MANDATORY A/C *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 5 Open

2006-07-12 (SUPERSEDED)2010-05-13 (REF)2010-05-13SUB5 (ACTIVE)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2010-05-13SUB5 (SEC-TASK)SBB 737-53A1262-5 (ACTIVE)SBB 737-53A1262-5 (INSP-TASK)



737-53A1266 SB 00 MANDATORY A/C *AD* FUSELAGE - DORSAL FIN NOSE CAP MODIFICATION Closed 27.Jun.2011 W/O:205174Mandated by AD 2009-07-11120S-07-572 (ACTIVE)2004-22-05 (SUPERSEDED)2009-07-11 (ACTIVE)37-SBB-53A1266 (INSP/REP/MOD)737-53A1266-R0 (ACTIVE)737-SRP-53-0250 (REF)

AMOCADADTASBSRP






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1269 SB 00 MANDATORY A/C *AD* AIRSTAIR DOOR CUTOUT - WEB & INTERCOASTAL INSP./MOD. Closed 07.Feb.2008

2009-09-06 (ACTIVE)737-53A1269-RO (ACTIVE)737-SRP-53-0249 (REF)SBB 737-53A1269 (INSP-TASK)

ADSBSRPTA




737-53A1279 SB 00 MANDATORY A/C *AD* FUSELAGE FRAMES-WIRE PENETRATION HOLE-INSP/REPAIR & MOD Superseded (Superseded)2009-02-06 (REF)2009-02-06R1 (ACTIVE)37-SBB-53A1279 (REPETITIVE)737-53A1279-R0 (ACTIVE)737-SRP-53-0289 (REF)SBB 737-53A1279 (TERMINATING)

ADADTASBSRPTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1279 SB 01 MANDATORY A/C FUSELAGE - FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19 TO

STRINGER 21 - FRAMES AND FRAME REINFORCEMENTS - INSPECTION, REPAIROpen

This Document SUPERSEDES 737-53A1279/SB Rev.00Perform BEFORE 30000/C for the first timeThereafter perform in an interval of 4500/C

737-53A1279/SB Rev.01 FUSELAGE - FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19 TOSTRINGER 21 - FRAMES AND FRAME REINFORCEMENTS - INSPECTION, REPAIR

Open

This Document SUPERSEDES 737-53A1279/SB Rev.00> 737-53A1279/EO* Rev.01 NDT - FUSELAGE - FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19

TO STRINGER 21 - FRAMES AND FRAME REINFORCEMENTS - INSPECTIONRepetitive

This Document SUPERSEDES 737-53A1279/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentNOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

47651/C

Perform initially within (effective fromManufacturer Date 13.Mar.1990) (L)30000/C Perform initially within (effectivefrom 02.Sep.2011) (L) 90/D /Interval(L):4500/C


> 737-53A1279-01/EO* Rev.00 *AD* FUSELAGE FRAMES-WIRE PENETRATION HOLE-INSP/REPAIR & MOD Term.Action openDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1293 SB 00 MANDATORY A/C FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL NDT INSP Superseded (Cancelled)

2008-19-03 (ACTIVE)737-53A1293-R0737-53A1293-R1 (ACTIVE)FAA LETTER 120S-09-460

ADSBSBAMOC

This Document has been SUPERSEDED BY 737-53A1293/SB Rev.01Perform WITHIN 33000/C

737-53A1293/SB Rev.00 FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL NDT INSP CancelledThis Document has been SUPERSEDED BY 737-53A1293/SB Rev.01

> 737-53A1293/EO* Rev.00 FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL NDT INSP - UTPA CancelledThis Document has been SUPERSEDED BY 737-53A1293/EO Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Jul.2011 64534:00/H 37798/C 205163, N/A Was due at: 38836/C PerfRev.:'00'Reason for this StatusManually deassigned after Document Cancelled/Superseeded

737-53A1293 SB 01 MANDATORY A/C FUSELAGE SKIN - STRINGER S-1 AND S-2R, STATION 400 TO 460 INSPECTION ANDREPAIR


2008-19-03 (ACTIVE)737-53A1293-R0737-53A1293-R1 (ACTIVE)FAA LETTER 120S-09-460

ADSBSBAMOC






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1293 SB 02 MANDATORY A/C FUSELAGE - SKIN - STRINGER S-1 AND S-2R, STATION 400 TO 460 INSPECTION AND

REPAIROpen

LN-KKR, VAR PM381, has been removed from applicablilty by Boeing.This Document SUPERSEDES 737-53A1293/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT737-53A1293/SB* Rev.02 FUSELAGE - SKIN - STRINGER S-1 AND S-2R, STATION 400 TO 460 INSPECTION AND

REPAIROpen

This Document SUPERSEDES 737-53A1293/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> 737-53A1293/EO* Rev.02 NDT - FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL UTPA INSPECTION Repetitive




> 737-53A1293-1/EO* Rev.02 NDT - FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL MFEC INSPECTION Not ApplicableReason for this StatusTEMPORATY NOT APPLIC DUE TO UTPA INSP PERF ON EO 737-53A1293





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1301 SB 02 MANDATORY A/C FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS IN CROWN SKINS AT SPECIFIED

LOCATIONS - INSPECTIONRepetitive





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusBOEING SERVICE BULLETIN 737-53A1301-R2.

F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.


In addition, the Manager of the FAA Seattle Aircraft CertificationOffice (ACO) approves the inspections with the correspondingcompliance times specified in Tables 1 through 4, under paragraph1.E., "Compliance," of Service Bulletin 737-53A1301 Revision 2 as anAMOC to the inspections with the corresponding compliance timesspecified in Table 1 under paragraph 1.E., "Compliance," of ServiceBulletin 737-53A1301, dated September 3, 2009, required by paragraph(g) of AD 2010-01-09.

When this service bulletin specifies contacting Boeing for repairinstructions, the repair instructions must be approved by the FAA isaccordance with the AD. All provisions of AD 2010-01-09 that are notspecifically referenced in the above statement remain fullyapplicable and must be complied with.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status2010-01-09737-53A1301 R0737-53A1301 R1

ADSBSB

This Document SUPERSEDES 737-53A1301/EO Rev.01This Document SUPERSEDES 737-53A1301/SB Rev.01Perform within an unlimited threshold.

737-53A1301/SB Rev.02 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS IN CROWN SKINS AT SPECIFIEDLOCATIONS - INSPECTION

Repetitive

This Document SUPERSEDES 737-53A1301/EO Rev.01This Document SUPERSEDES 737-53A1301/SB Rev.01

> 737-53A1301/EO* Rev.02 FUSELAGE CROWN SKINS -NDT AT SPECIFIEC LOCATIONS- EXTERNAL UTPAINSPECTION FOR CRACKS AT CHEM-MILLED STEPS.

Repetitive




> 737-53A1301-1/EO* Rev.02 FUSELAGE CROWN SKINS - NDT AT SPECIFIEC LOCATIONS - MFEC INSPECTION FORCRACKS AT CHEM-MILLED STEPS.


737-53A1318 SB 00 MANDATORY A/C *AD* FUSELAGE - SKIN - SKIN CRACKING AT THE AFT WASTE WATER DRAIN MASTINSPECTION AND REPAIR

Closed 12.Nov.2012 W/O:273636

To be performed at next Heavy Maitenance Stop.2012-23-14737-FTD-53-10002737-SL-51-042737-SRP-53-0367

ADFTDSLSRP

00N/ADN/A






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1319 SB 00 MANDATORY A/C FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW

CRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908Superseded (Not Applicable)

EAD US-2011-08-51 AD 00This Document has been SUPERSEDED BY 737-53A1319/SB Rev.01

737-53A1319/SB Rev.00 FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROWCRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908

Not Applicable

This Document has been SUPERSEDED BY 737-53A1319/SB Rev.01> 737-53A1319-01/EO* Rev.00 FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW

CRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908Not Applicable by Serial Number

This Document has been SUPERSEDED BY 737-53A1319-01/EO Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1319 SB 01 MANDATORY A/C FUSELAGE - SKIN - CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW

CRACKING AT STRINGER S-4, BETWEEN BS 360 AND BS 908Superseded (Not Applicable)

Service Bulletin 737-53A1319-R1.F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.


In addition, the Manager of the FAA Seattle Aircraft CertificationOffice approves accomplishment of the inspection methods and crackconfirmation in accordance with Boeing Alert Service Bulletin737-53A1319, Revision 1, as an AMOC to accomplishment of theinspection methods and crack confirmation required by paragraphs (g)and (i) of AD 2011-08-51. All provisions of AD 2011-08-51 that arenot specifically referenced in this paragraph remain fully applicableand must be complied with accordingly.EAD US-2011-08-51 AD 00This Document SUPERSEDES 737-53A1319/SB Rev.00This Document has been SUPERSEDED BY 737-53A1319/SB Rev.02

737-53A1319/SB Rev.01 FUSELAGE - SKIN - CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROWCRACKING AT STRINGER S-4, BETWEEN BS 360 AND BS 908

Not Applicable





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-53A1319/SB Rev.00This Document has been SUPERSEDED BY 737-53A1319/SB Rev.02

> 737-53A1319-01/EO* Rev.01 FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROWCRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908


This Document SUPERSEDES 737-53A1319-01/EO Rev.00This Document has been SUPERSEDED BY 737-53A1319-01/EO Rev.02





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1322 SB 00 MANDATORY A/C FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R -

INSPECTION AND REPLACEMENTOpen

Group 3 Config 2 covers airplane line numbers 520-2552 that have notaccomplished the lap modification in accordance with SB 737-53A1177.

Group 4 covers airplane line numbers 2553-3132.737-53A1322 SB 00Perform within an unlimited threshold.

737-53A1322/SB Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R -INSPECTION AND REPLACEMENT

Open

> 737-53A1322-01/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R -INITIAL INSPECTION

Open

NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentNOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

50000/CPerform initially before(L) 50000/C Performinitially within (effective from 14.Mar.2014)(L) 5000/C

> 737-53A1322-02/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 S-5L TO S-3L, S-3R TOS-5R - REPETETIVE INSPECTION

Postponed (open) / Special Text: PostEO 737-53A1322-01

Reason for this StatusTO BE TRIGGERD WHEN EO 737-53A1322-01 IS POST

> 737-53A1322-03/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 908 S-5L TO S-3L, S-3R TOS-5R - REPETETIVE INSPECTION



> 737-53A1322-04/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908 S-10L TO S-5L,S-3L TO S-3R, S-5R TO S-10R - REPETETIVE INSPECTION







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-53A1322-05/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 AND 908 S-5L TO S-3L,

S-3R TO S-5R - FASTENER REMOVAL AND REINSTALLATIONOn Attrition

> 737-53A1322-06/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 - STRINGER SPLICEREMOVAL AND REPLACEMENT

On Attrition

> 737-53A1322-07/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 908 - STRINGER SPLICEREMOVAL AND REPLACEMENT

On Attrition

> 737-53A1322-08/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908 - POSTSTRINGER SPLICE REMOVAL AND REPLACEMENT - INSPECTION

On Attrition / Special Text: post EO737-53A1322-06 and/or737-53A1322-07





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1323 SB 00 RECOMMENDED A/C FUSELAGE - FRAMES - CRACKING OF FRAMES AT STA 328 BETWEEN STRINGERS S TO

S-21R, STA 360 BETWEEN STRINGERS S-19R TO S-21R, AND STA 380 BETWEEOpen

NAS fleet has 3 different groups - 2,4 & 7

This SB is divided into 7 EO`s, as given below;

737-53A1323-01 - Insp of strap installation STA312

737-53A1323-02 - Insp of frame for cracking STA328




737-53A1323-06 - Rep of frame, STA328

737-53A1323-07 - Post rep insp, STA328Perform within an unlimited threshold.

737-53A1323/SB Rev.00 FUSELAGE - FRAMES - CRACKING OF FRAMES AT STA 328 BETWEEN STRINGERS S TOS-21R, STA 360 BETWEEN STRINGERS S-19R TO S-21R, AND STA 380 BETWEE

Open

> 737-53A1323-01/EO* Rev.00 FUSELAGE - FRAMES - VERIFICATION OF STRAP INSTALLATION, STA312 Closed 13.Feb.2014 W/O:510114Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks13.Feb.2014 71572:00/H 43151/C 510114, N/A Was due at: 45080/C PerfRev.:'00'

> 737-53A1323-02/EO* Rev.00 FUSELAGE - FRAMES - INSPECTION FOR CRACKS, STA328 RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status11.Feb.2014 71572:00/H 43151/C 510110, N/A Was due at: 44130/C PerfRev.:'00'







> 737-53A1323-05/EO* Rev.00 FUSELAGE - FRAMES - INSPECTION FOR CRACKS, STA380 OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> 737-53A1323-06/EO* Rev.00 FUSELAGE - FRAMES - REPAIR OF FRAME, STA328 On Attrition> 737-53A1323-07/EO* Rev.00 FUSELAGE - FRAMES - POST REPAIR INSPECTION, STA328 On Attrition





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1328 SB 00 RECOMMENDED A/C FUSELAGE - SKIN - INSPECTION, PREVENTIVE MODIFICATION AND REPAIRS FOR

WINDOW CORNERSNot Applicable

This service bulletin gives instructions to inspect for cracks andaccomplish a preventive modification and/or limited repairs atfastener locations in window corners of the window belt area betweenSTA 360 to STA 540 and STA 727 to STA 908, left and right side at andbetween stringers S-11 and S-13. If not corrected, the crackingaround the fastener holes could cause multiple window corner skincracks which can result in rapid decompressionand loss of structural integrity.

737-53A1328/SB Rev.00 FUSELAGE - SKIN - INSPECTION, PREVENTIVE MODIFICATION AND REPAIRS FORWINDOW CORNERS

Not Applicable

> 737-53A1328-01/EO* Rev.00 FUSELAGE - SKIN - INSPECTION, PREVENTIVE MODIFICATION AND REPAIRS FORWINDOW CORNERS


737-53A1329 SB 00 MANDATORY A/C FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTIONAND REPAIR

Not Applicable

Variable number effectivity used to determine if airplane have anairstair door cutout.

737-53A1329/SB Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTIONAND REPAIR

Not Applicable

> 737-53A1329-01/EO* Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTIONAND REPAIR


This Document has been SUPERSEDED BY 737-53A1329-01/EO Rev.01> 737-53A1329-01/EO* Rev.01 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTION

AND REPAIRNot Applicable by Serial Number






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-53A1339 SB 00 RECOMMENDED A/C FUSELAGE - FRAMES AND BULKHEADS - UPPER FRAME TO SIDE FRAME SPLICE AT

STA 360 BETWEEN STRINGER 13 AND STRINGER 14 - INSPECTION,Not Applicable by Serial Number

LN-KKN phased out. No other A/C in Eff

737-54-1015 SB NOTE

RECOMMENDED A/C NACELLES/PYLONS-PYLON NACELLE STRUT-HEAT SHIELD REINFORCEM. Not Applicable by Serial Number

737-53-1015-R2 (ACTIVE) SB

737-54-1028 SB 01 MANDATORY A/C *AD* PYLON NACELLE STRUT - FIREWALL SEALANT INSP./INST. Not Applicable by Serial Number737-54-1028-R0 (REF)737-54-1028-R1 (ACTIVE)

SBSB

737-54-1029 SB 00 RECOMMENDED A/C GROUND SUPPORT EQUIPMENT ATTACH POINTS - NUT REPLACEMENT Not Applicable by Serial Number737-54-1029-R0 (ACTIVE) SB

737-54-1031 SB 00 RECOMMENDED A/C NACELLE STRUT INSPECTION AND MODIFICATION OF THE STRUT SKIN Rejected by Operator737-54-1031-R0 (ACTIVE) SB





24.Oct.2014/411


TERECOMMENDED A/C NACELL-STRUT SKIN CRACKS AROUND ACCESS OPENING 5724 AND 5824 Repetitive

37-SBB-54-1032P1L (REPET)37-SBB-54-1032P1R (REPET)737-54-1032-R0 (ACTIVE)SBB 737-54-1032P2L (MOD-TASK)SBB 737-54-1032P2R (MOD-TASK)SBB 737-54-1032P3L (MOD-TASK)SBB 737-54-1032P3R (MOD-TASK)

TATASBTATATATA


27.Jan.2004 43514:00/H 21346/CPerfRev.:'NOTE' / Reason: TASK37-SBB-54-1032P1L AND R

Reason for this StatusTASK 37-SBB-54-1032P1L AND R





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-54-1032L SB NO

TEOPTIONAL A/C NACELLE/PYLON - NACELLE STRUT - CRACK INSPECTION & REPAIR Open

737-54-1032737-54-1032 IN04737-54-1032 NSC1737-54-1032 NSC2737-54-1032 NSC3

SBSBSBSBSB

Perform within an unlimited threshold.737-54-1032L/SB Rev.NOTE NACELLE/PYLON - NACELLE STRUT - CRACK INSPECTION & REPAIR Open> 737-54-1032L-F1/EO*Rev.NOTE

NACELLE/PYLON - NACELLE STRUT - CRACK INSPECTION & REPAIR Term.Action open


> 737-54-1032P1L/EO*Rev.NOTE

NACELLES/PYLON - NACELLE STRUT - CRACK INSPECTION AND REPAIR ***REPETITIVE INSPECTION ***

Repetitive



Reason for this StatusAMICOS WO 510114 2-INSP HEAVY-SERV-12YR/SI/CPCP.NAS TASK/BOEING INSP.T





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-54-1032R SB NO

TEOPTIONAL A/C NACELLE/PYLON, NACELLE STRUT - CRACK INSPECTION & REPAIR R/H Open

737-54-1032737-54-1032 IN04737-54-1032 NSC1737-54-1032 NSC2737-54-1032 NSC3

SBSBSBSBSB

Perform within an unlimited threshold.737-54-1032R/SB Rev.NOTE NACELLE/PYLON, NACELLE STRUT - CRACK INSPECTION & REPAIR R/H Open> 737-54-1032P1R/EO*Rev.NOTE

NACELLES/PYLON - NACELLE STRUT - CRACK INSPECTION R/H *** REPETITIVEINSPECTION ***

Repetitive



Reason for this StatusAMICOS WO 510114 2-INSP HEAVY-SERV-12YR/SI/CPCP.NAS TASK/BOEING INSP.T

> 737-54-1032R-F1/EO*Rev.NOTE

NACELLE/PYLON, NACELLE STRUT - CRACK INSPECTION & REPAIR R/H Term.Action open


737-54-1033 SB 00 RECOMMENDED A/C NACELLE/PYLONS - STRUT FAIRING PANEL - NUTPLATE REPLACEMENT Rejected by Operator737-54-1033-R0 (ACTIVE)PRODUCTION PRR34879

SBPRR

737-54-1034 SB 00 RECOMMENDED A/C AFT FAIRING-PLUME SUPPRESSOR HEAT SHIELD-LOWER SKIN CRACKS Superseded (Superseded)737-54-1034-R1 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-54-1034/SB Rev.01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-54-1034 SB 01 RECOMMENDED A/C AFT FAIRING-PLUME SUPPRESSOR HEAT SHIELD-LOWER SKIN CRACKS Rejected by Operator

737-54-1034-R1 (ACTIVE) SBThis Document SUPERSEDES 737-54-1034/SB Rev.00

737-54-1035 SB 00 RECOMMENDED A/C INSPECTION AND REPAIR OF STRUT SKIN CRACKS AROUND OPENINGS Rejected by OperatorThis Document is Applicable to LN# 1001-2452, 2267,2268,2270,2296,2298. NAS has rejected this SB. NAS considers that 15 month and 45month Pylon inspections per MPD is adequate.737-54-1035-R0 (ACTIVE)PRODUCTION PRR35005-24

SBPRR

Reason for this StatusNAS PERFORMS 15 AND 45 MONTH PYLON INSPECTIONS, THIS COVERS SB

737-54-1036 SB NOTE

RECOMMENDED A/C THRUST REV HINGE FITTING AND VIBRATION ISOLATOR REPLACEMENT Rejected by Operator


SBPRR





24.Oct.2014/411


TERECOMMENDED A/C MID SPAR BUSHING AND UPPER LINK BUSHING INSP. AND REPLACEM. Repetitive

37-54-001 (MOD TASK)37-54-002 (MOD TASK)37-54-003 (MOD TASK)37-SBB-54-1037P1L (REPET)37-SBB-54-1037P1R (REPET)737-54-1037-R1 (ACTIVE)PRODUCTION PRR35005-142SBB 737-54-1037-L (DELETED)SBB 737-54-1037-R (DELETED)

EODEODEODTATASBPRRTATA

Perform within an unlimited threshold.737-54-1037/SB Rev.NOTE MID SPAR BUSHING AND UPPER LINK BUSHING INSP. AND REPLACEM. Repetitive> 737-54-1037P1L/EO* Rev.00 NACELLE/PYLON L/H - STRUT - BUSHING INSPECTION Repetitive

This Document is terminated with implementation of 737-54-1037-L-01/EO Rev.NOTEPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

05.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150719 KKM 37-SBB-54-1037P1L/1RSTRUT BU

Reason for this StatusAMICOS WO 150719 KKM 37-SBB-54-1037P1L/1R STRUT BUSHING INSP -ATC

> 737-54-1037P1R/EO* Rev.00 NACELLE/PYLON R/H - STRUT - BUSHING INSPECTION RepetitiveThis Document is terminated with implementation of 737-54-1037-R-01/EO Rev.NOTEPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-54-1037-L SB 01 RECOMMENDED A/C NACELLE/PYLON - STRUT - BUSHING INSPECTION/ REPLACEMENT Repetitive

1-234466455-2737-54-1037737-54-1037 IN 07737-54-1037 R1

BMSBSBSB

Perform BEFORE 23.Oct.1996Perform BEFORE 51676/C

737-54-1037-L/SB Rev.01 NACELLE/PYLON - STRUT - BUSHING INSPECTION/ REPLACEMENT Repetitive> 737-54-1037-L-01/EO*Rev.NOTE

NACELLE/PYLON - STRUT - BUSHING INSPECTION/ REPLACEMENT Closed 07.Feb.2008

This Document terminates 737-54-1037P1L/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-54-1037P1L/EO* Rev.00 NACELLE/PYLON L/H - STRUT - BUSHING INSPECTION RepetitiveThis Document is terminated with implementation of 737-54-1037-L-01/EO Rev.NOTEPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-54-1037-R SB 01 RECOMMENDED A/C NACELLE/PYLON - STRUT - BUSHING INSPECTION/REPLACEMENT R/H Repetitive

1234466455-2737-54-1037737-54-1037 IN 01737-54-1037 R1

BMSBSBSB

Perform BEFORE 23.Oct.1996Perform BEFORE 51676/C

737-54-1037-R/SB Rev.01 NACELLE/PYLON - STRUT - BUSHING INSPECTION/REPLACEMENT R/H Repetitive> 737-54-1037-R-01/EO*Rev.NOTE

NACELLE/PYLON - STRUT - BUSHING INSPECTION/REPLACEMENT R/H Closed 07.Feb.2008

This Document terminates 737-54-1037P1R/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-54-1037P1R/EO* Rev.00 NACELLE/PYLON R/H - STRUT - BUSHING INSPECTION RepetitiveThis Document is terminated with implementation of 737-54-1037-R-01/EO Rev.NOTEPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-54A1044 SB 02 MANDATORY A/C *AD* NACELLE STRUT - MIDSPAR FUSE PIN - INSPECT/REPAIR/MOD Open

This SB is devided into two EO.EO 737-54A1044-01 covers the replacement per AD§ (h).EO 737-54A1044 covers the repetitive inspection per AD §(g).2008-21-03 (ACTIVE)37-SBB-54A1044 (REPETITIVE)737-54-1044-R1 (REF)737-54A1044-R2 (ACTIVE)PRODUCTION PRR35005-273RS

ADTASBSBPRR

Perform within an unlimited threshold.737-54A1044/SB Rev.02 *AD* NACELLE STRUT - MIDSPAR FUSE PIN - INSPECT/REPAIR/MOD Open> 737-54A1044/EO* Rev.02 *AD* NACELLE STRUT - MIDSPAR FUSE PIN - INSPECTION & REPAIR *** REPETITIVE

MANDATORY INSPECTION ***Repetitive


16.Feb.2019Perform initially within (effective fromManufacturer Date 13.Mar.1990) (F)7211/D / Interval(F):1825/D

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Feb.2014 71572:00/H 43151/C 436906, N/A Was due at: 17.Mar.2014 PerfRev.:'02'

> 737-54A1044-01/EO* Rev.02 *AD* NACELLE STRUT - MIDSPAR FUSE PIN - REPALCEMENT OF OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

07.Feb.2020Perform initially within (effective from09.Feb.2010) (F) 3650/D

737-55-1044 SB 03 RECOMMENDED A/C JACKSCREW SUPPORT FITTING ATTACH BOLTS - INSPECTION AND REP. Rejected by Operator737-55-1044-R3 (ACTIVE) SBThis Document SUPERSEDES 737-55-1044/SB Rev.02





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55-1044 SB 01 RECOMMENDED A/C JACKSCREW SUPPORT FITTING ATTACH BOLTS - INSPECTION AND REP. Superseded (Superseded)

737-55-1044-R3 (ACTIVE) SBThis Document SUPERSEDES 737-55-1044/SB Rev.00This Document has been SUPERSEDED BY 737-55-1044/SB Rev.02

737-55-1044 SB 00 RECOMMENDED A/C JACKSCREW SUPPORT FITTING ATTACH BOLTS - INSPECTION AND REP. Superseded (Superseded)737-55-1044-R3 (ACTIVE) SBThis Document has been SUPERSEDED BY 737-55-1044/SB Rev.01

737-55-1044 SB 02 RECOMMENDED A/C JACKSCREW SUPPORT FITTING ATTACH BOLTS - INSPECTION AND REP. Superseded (Superseded)737-55-1044-R3 (ACTIVE) SBThis Document SUPERSEDES 737-55-1044/SB Rev.01This Document has been SUPERSEDED BY 737-55-1044/SB Rev.03

737-55-1048 SB NOTE

RECOMMENDED A/C HORIZONTAL STAB. - CHANGES TO THE LIGHTING STRIKE PROTECTION Rejected by Operator


SBPRR

737-55-1049-L SB NOTE

RECOMMENDED A/C ELEVATOR TAB L/H - HINGE FITTING AND BEARING REPLACEMENT Closed 19.Feb.2008

737-55-1049737-55-1049 R1

SBSB








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55-1049-R SB NO

TERECOMMENDED A/C ELEVATOR TAB R/H - HINGE FITTING AND BEARING REPLACEMENT Closed 19.Feb.2008

737-55-1049737-55-1049 R1

SBSB




737-55-1052 SB 01 MANDATORY A/C *AD* VERTICAL STAB, TRAILING EDGE BEAM INSPECTION & REWORK Closed 10.Mar.20052002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-55-1052-R0 (REF)737-55-1052-R1 (ACTIVE)MRR3553-951SBB 737-55-1052 (MOD-TASK)

ADADSBSBPRRTA




737-55-1054 SB NOTE

RECOMMENDED A/C SLIDING BEARING PLATE ASSEMBLY INSPECTION, REWORK OR REPL. Rejected by Operator

737-55-1054-R2 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55-1057 SB 00 MANDATORY A/C *AD* VERTICAL STAB. AUX STRUC., DORSAL FIN AY INSP/PREV MOD Closed 13.Feb.1999

120S-04-485 (ACTIVE)2004-22-05 (SUPERSEDED)2009-07-11 (ACTIVE)37-SBB-55-1057P1 (REPLACED)737-55-1057 IN 03(REPLACED)737-55-1057-R0 (REPLACED)737-55-1057-R1 (REPLACED)737-55-1057-R2 (REPLACED)737-55-1057-R3 (REPLACED)AD 2004-22-05 (SUPERSEDED)SBB 737-53A1266 (ACTIVE)SBB 737-55-1057 (REPLACED)

AMOCADADTASBSBSBSBSBTASBTA


13.Feb.1999PerfRev.:'NOTE' / Reason: REPLACED BYSB737-53A1266

Reason for this StatusREPLACED BY SB737-53A1266

737-55-1058 SB NOTE

RECOMMENDED A/C STABILIZERS - HORIZONTAL STABILIZER ATTACHMENT LUG MOD. Rejected by Operator

737-55-1058-R0 (ACTIVE)PRODUCTION PRR35005-136SRP 737-55-0009 (REF)

SBPRRSRP





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55-1059 SB 00 RECOMMENDED A/C HORIZONTAL STABILIZER - LOWER SKIN INSPECTION, REPAIR AND MODIFICATION Rejected by Operator

SB slpitted in three parts:

1. EO 737-55-1059-01 cover initial and repetetive inspection.2. EO 737-55-1059-02 cover LH side horiz. stab. Repair/Mod.3. EO 737-55-1059-03 cover RH side horiz. stab. Repair/Mod737-55-1059 IN 01737-55-1059 IN 02

SBSB

0000

Perform within an unlimited threshold.737-55-1059/SB Rev.00 HORIZONTAL STABILIZER - LOWER SKIN INSPECTION, REPAIR AND MODIFICATION Rejected by Operator> 737-55-1059-01/EO* Rev.00 INSP, LH AND RH HORIZONTAL STABILIZER LOWER SKIN Rejected by Operator

Reason for this StatusREJECTED BY NAS

> 737-55-1059-02/EO* Rev.00 MOD/REP, LH SIDE STABILIZER LOWER SKIN REPAIR AND MODIFICATION Rejected by OperatorReason for this StatusREJECTED BY NAS

> 737-55-1059-03/EO* Rev.00 MOD/REP, RH SIDE STABILIZER LOWER SKIN REPAIR AND MODIFICATION Rejected by OperatorReason for this StatusREJECTED BY NAS

737-55-1061 SB NOTE

RECOMMENDED A/C STAB. - INSP OF THE FASTENERS IN THE ELEVATOR HINGE PLATE Not Applicable by Serial Number

737-55-1061-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55-1091 SB 01 RECOMMENDED A/C STABILIZERS - HORIZONTAL STABILIZER - INSPECTION AND REPLACEMENT OF

THRUST BEAM CORNER FITTINGSOpen

737-SRP-55-0043 SRP 00This Document SUPERSEDES 737-55-1091/SB Rev.00Perform within an unlimited threshold.

737-55-1091/SB Rev.01 STABILIZERS - HORIZONTAL STABILIZER - INSPECTION AND REPLACEMENT OFTHRUST BEAM CORNER FITTINGS

Open

This Document SUPERSEDES 737-55-1091/SB Rev.00> 737-55-1091-01/EO* Rev.00 STABILIZERS - HORIZONTAL STABILIZER - INSPECTION OF THRUST BEAM CORNER

FITTINGSRepetitive


06.Feb.2016 77572:00/H 47651/C

Perform initially within (effective from23.May.2012) (F) 730/D or 4500/C or6000/H / Interval(F):4500/C or 730/D or6000/H


06.Feb.2014 71572:00/H 43151/C 491458, N/AWas due at: 44176/C and 23.May.2014 and4371180/H PerfRev.:'00'

> 737-55-1091-02/EO* Rev.00 STABILIZERS - HORIZONTAL STABILIZER - REPLACEMENT OF THRUST BEAMCORNER FITTINGS

On Attrition

This Document terminates 737-55-1091-01/EO Rev.00

737-55A1060 SB 01 MANDATORY A/C *AD* HORIZON. STABILIZER - INSP. FOR LOOSE/MISSING FASTENERS Not Applicable by Serial NumberThis document is applicable to LN# 2765-2980. All other LN# are NotApplicable per Boeing SB.1998-02-51 (ACTIVE)737-55A1060-R0 (REF)737-55A1060-R1 (ACTIVE)SBB 737-55A1060 (MOD-TASK)

ADSBSBTA





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55A1070 SB 03 MANDATORY A/C *AD* ELEVATOR TAB FREE-PLAY REPEAT INSPECTION Repetitive

2002-01-01 (SUPERSEDED)2006-12-23 (ACTIVE)37-SBB-55A1070-WP2 (REF)37-SBB-55A1070-WP3 (REF)37-SBB-55A1070P1+2(REPETITIVE)37-SBB-55A1070P3 (REPETITIVE)737-55A1070-R0 (REF)737-55A1070-R1 (REF)737-55A1070-R2 (REF)737-55A1070-R3 (ACTIVE)737-SL-02-002-D (REF, VIBR CH)737-SL-55-032SBB-737-55A1070 (INSPECT-TASK)

ADADTATATATASBSBSBSBSLSLTA

00

Perform within an unlimited threshold.737-55A1070/SB Rev.03 *AD* ELEVATOR TAB FREE-PLAY REPEAT INSPECTION Repetitive> 737-55A1070P1+2/EO* Rev.00 *AD* HINGE DETAIL, FREE-PLAY AND CLAMPED HINGE PUTTY INSPEC AD 2006-12-23 -

SBB 737-55A1070 PART 1, PART 2 AND PART 10Repetitive


75319:36/H 45994/CPerform initially before(F) 28394/C or52066/H / Interval(F):1500/C or 2000/H


06.Oct.2014 73319:36/H 44494/C 554152,Was due at: 44651/C and 4414320/HPerfRev.:'00'

> 737-55A1070P3/EO* Rev.00 *AD* ELEVATOR TAB CONTROL INSPECTION AD 2006-12-23 - SBB 737-55A1070, REV 2,PART 3

Repetitive








24.Oct.2014/411



737-55A1070-2 SB 03 MANDATORY A/C *AD* ELEVATOR & TAB, INITIAL INSPECTIONS & PUTTY APPLICATION Closed 10.Jul.20062002-01-01 (SUPERSEDED)2006-12-23 (ACTIVE)737-55A1070 IN 05 (REF)737-55A1070 IN 06 (REF)737-55A1070 IN 07 (REF)737-55A1070 IN 08 (REF)737-55A1070-R2 (REF)737-55A1070-R3 (ACTIVE)737-SL-27-118 (REF)AMOC LETTER 120S-06-427AMOC LETTER 120S-06-457AMOC LETTER 120S-07-476AMOC LETTER 120S-07-568SBB 737-55A1070-2 (INSP.-TASK)

ADADSBSBSBSBSBSBSLDOCRDOCRDOCRDOCRTA


10.Jul.2006 50066:00/H 26894/CPerfRev.:'NOTE' / Reason: KKM 150759ITEM: 1






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55A1070P4 SB 03 MANDATORY A/C *AD* ELEVATOR / TAB DETERMINATION OF CONFIGURATION Closed 10.Jul.2006

2006-12-23 (ACTIVE)737-55A1070-R2 (REF)737-55A1070-R3 (ACTIVE)SBB 737-55A1070P4 (INSPECTION)

ADSBSBTA

Perform BEFORE 03.Oct.2006737-55A1070P4/SB Rev.03 *AD* ELEVATOR / TAB DETERMINATION OF CONFIGURATION Closed 10.Jul.2006> 737-55A1070-2/SB* Rev.03 *AD* ELEVATOR & TAB, INITIAL INSPECTIONS & PUTTY APPLICATION Closed 10.Jul.2006


10.Jul.2006 50066:00/H 26894/CPerfRev.:'NOTE' / Reason: KKM 150759ITEM: 1






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55A1077 SB 00 MANDATORY A/C *AD* HORIZONTAL STABILIZER HINGE PIN INSP. & CORROSION PREV. Repetitive

2004-19-10 (ACTIVE)37-SBB-55A1077-P1 (REPETITIVE)37-SBB-55A1077-P2 (REPETITIVE)37-SBB-55A1077-P3 (REPETITIVE)737-55A1077 IN01 (REF)737-55A1077-RO (ACTIVE)

ADTATATASBSB

Perform within an unlimited threshold.737-55A1077/SB Rev.00 *AD* HORIZONTAL STABILIZER HINGE PIN INSP. & CORROSION PREV. Repetitive> 737-55A1077-P1/EO* Rev.00 *AD* *AD* HORIZONTAL STAB. - DET. VISUAL INSP OF HINGE PIN Not Applicable by Serial Number> 737-55A1077-P2/EO* Rev.00 *AD* HORIZONTAL STAB. - INNER & OUTER HINGE PIN INSPECTION ***

MANDATORY REPETITIVE VISUAL INSPECTION ***Repetitive


01.Nov.2016 76139:00/HPerform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D or0/H / Interval(F):1460/D or 8000/H


02.Nov.2012 68139:00/H 40570/C 273609, N/AWas due at: 23.Mar.2014 and 4132020/HPerfRev.:'00'

> 737-55A1077-P3/EO* Rev.00 *AD* HORIZONTAL STAB. - INNER & OUTER HINGE PIN INSPECTION ***MANDATORY REPETITIVE VISUAL INSPECTION ***

Repetitive


31.Oct.2020 84139:00/H



02.Nov.2012 68139:00/H 40570/C 273647, N/AWas due at: 05.Feb.2016 and 4232520/HPerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-55A1087 SB 00 MANDATORY A/C *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Repetitive

120S-04-174 (ACTIVE)2003-26-01 (ACTIVE)37-SBB-55A1087-1 (REP TASK)37-SBB-55A1087-3 (REP TASK)737-55A1087 (REF)737-55A1087 IN 01 (REF)737-55A1087 IN 02 (REF)737-55A1087 IN 03 (ACTIVE)SBB 737-55A1087 (MAINT TASK)

AMOCADTATASBSBSBSBTA

Perform BEFORE 4500/CPerform BEFORE 6000/H

737-55A1087/SB Rev.00 *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Repetitive> 737-55A1087-01/EO* Rev.00 *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Closed 10.Mar.2005




> 737-55A1087-1/EO* Rev.00 *AD* RUDDER, ACTUATOR ATTACH FITTINGS, INSP FOR LOOSE Not Applicable by Serial Number> 737-55A1087-3/EO* Rev.00 *AD* RUDDER-MAIN & AUX ACTUATOR ATTACH FITTINGS TORQUE CHECK **

STAGE 3 - REPEAT TORQUE CHECK/REWORK **Repetitive


77572:00/H 47651/CPerform initially before(F) 52130/H or28075/C / Interval(F):6000/H or 4500/C







24.Oct.2014/411


TERECOMMENDED A/C WINDOWS - NUMBER 2 SLIDING WINDOW GUIDE PIN MODIFICATION Rejected by Operator


SBPRR

737-56-1010 SB NOTE

RECOMMENDED A/C WINDOW NO.1 - LH AND RH - UPPER AFT HEAT TERMINAL - INSP. Rejected by Operator

737-56-1010-R0 (ACTIVE)737-SL-56-2 (REF)

SBSL

737-56-1013 SB 00 RECOMMENDED A/C CONTROL CABIN FIXED WINDOWS - WINDOW #3 - INSP & REPLACEMENT Not Applicable37-SBB-56-1013 (REPETITIVE)737-56-1013 IN 01 (REF)737-56-1013-R0 (ACTIVE)737-SRP-56-0010 (REF)PRODUCTION PRR 38275-11SBB 737-56-1013 (MOD-TASK)

TASBSBSRPPRRTA

737-56-1013/SB Rev.00 CONTROL CABIN FIXED WINDOWS - WINDOW #3 - INSP & REPLACEMENT Not Applicable> 737-56-1013/EO* Rev.00 WINDOW - INSP. & REPLCMT. Not Applicable by Serial Number> 737-56-1013-01/EO* Rev.00 CONTROL CABIN FIXED WINDOWS - WINDOW #3 - INSP & REPLACEMENT Not Applicable by Serial Number





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-56-1026 SB 00 MANDATORY A/C FLIGHT DECK NUMBER 2 WINDOW PANE - REPLACEMENT Rejected by Operator

NAS performs inspections per AD 2008-09-15, SB 737-56A1023. NAS hasopted not to perform scheduled replacements of No. 2 window.2008-09-15 (REF)37-SBB-56A1023 (REPETITIVE)737 FTD 56-05001 (REF)737-56-1026-R0 (ACTIVE)737-56A1023 (REF)737-SRP-56-0017 (REF)737-SRP-56-0018 (REF)PRODUCTION PRR35005-280RS

ADTAFTDSBSBSRPSRPPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-56A1023 SB 01 MANDATORY A/C *AD* FLIGHT DECK NUMBER 2, 4 AND 5 WINDOWS - INSPECTION Repetitive

2008-09-15 (ACTIVE)37-SBB-56A1023 (REPETITIVE)37-SBB-56A1023P1 (REPETITIVE)737-56-1026 (REF)737-56A1023-R0 (ACTIVE)

ADTATASBSB

Perform within an unlimited threshold.737-56A1023/SB Rev.01 *AD* FLIGHT DECK NUMBER 2, 4 AND 5 WINDOWS - INSPECTION Repetitive> 737-56A1023/EO* Rev.00 FLIGHT DECK WINDOWS NUMBER 2 REPETITIVE INSPECTION *** REPETITIVE

INSPECTION ***Repetitive


22.Jan.2017 79072:00/H



07.Feb.2014 71572:00/H 43151/C 436900, N/AWas due at: 12.Jun.2014 and 4322040/HPerfRev.:'00'

> 737-56A1023P1/EO* Rev.00 *AD* FLIGHT DECK NO. 4+5 WINDOWS INSPECTION AND REPLACEMENT ***MANDATORY REPETITIVE INSPECTION ***


737-57-1065 SB 04 RECOMMENDED A/C OUTBOARD FLAP TRACKS AFT SUPPORT INSPECTION AND MODIFICATION Not Applicable by Serial NumberApplicable to Line 1 thru 869 only (737-100/-200)2002-05-0732905737-57A1249

ADPRRSB

000102

737-57-1167 SB 03 RECOMMENDED A/C OUTB FLAP TRACK/FAIRING DOOR OPERATING LINKAGE REWORK Rejected by Operator737-57-1167-R3 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1169 SB 02 RECOMMENDED A/C BUBBLE FAIRING ATTACHMENT INSPECTION, MOD AND REPLACEMENT Not Applicable by Serial Number


SBPRR

737-57-1174 SB 01 OPTIONAL A/C LDG SUPPORT BEAMS - BEAM WEB REPAIR AND BOLT REORIENTATION Rejected by OperatorThis SB was rejected by the previous operator.737-57-1174-R0 (REF)737-57-1174-R1 (ACTIVE)

SBSB

737-57-1175 SB 05 RECOMMENDED A/C WINGS - LEADING EDGE SLATS AND FIXED LEADING EDGE UPSTOP CHANGE ANDMAIN TRACK DOWNSTOP CHANGE


NAS has no reliability issues in this area, therefore NAS does notperform this SB.PRODUCTION PRR34397PRODUCTION PRR35005-131

PRRPRR

0000

This Document SUPERSEDES 737-57-1175P1/SB Rev.04This Document SUPERSEDES 737-57-1175P2/SB Rev.04This Document SUPERSEDES 737-57-1175P3/SB Rev.04Reason for this StatusREJECTED BY PREVIOUS OPERATOR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1175P1 SB 03 RECOMMENDED A/C PART I - AUX. TRACK SUPPORT AND ROLLER/TRACK CLEARANCE INSP. Rejected by Operator

737-57-1175-R0 (REF)737-57-1175-R1 (REF)737-57-1175-R2 (REF)737-57-1175-R3 (ACTIVE)737-57-1238 (REF)737-SL-57-044 (REF)PRODL PRR 33890-84 & PRR 34397SBB 737-57-1175P1 (INSP-TASK)

SBSBSBSBSBSLPRRTA

Reason for this StatusSB REJECTED BY PREV. OPERATOR

737-57-1175P1 SB 04 RECOMMENDED A/C PART I - AUX. TRACK SUPPORT AND ROLLER/TRACK CLEARANCE INSP. Superseded (Superseded / SpecialText: Rejected by previousoperator.)

737-57-1175-R0 (REF)737-57-1175-R1 (REF)737-57-1175-R2 (REF)737-57-1175-R3 (ACTIVE)737-57-1238 (REF)737-SL-57-044 (REF)PRODL PRR 33890-84 & PRR 34397SBB 737-57-1175P1 (INSP-TASK)

SBSBSBSBSBSLPRRTA

This Document has been SUPERSEDED BY 737-57-1175/SB Rev.05Reason for this StatusSB REJECTED BY PREV. OPERATOR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1175P2 SB 03 RECOMMENDED A/C PART II - TIME-LIMITED REPAIR - AUXILIARY TRACK SUPPORT Superseded (Superseded)

737-57-1175-R0 (REF)737-57-1175-R1 (REF)737-57-1175-R2 (REF)737-57-1175-R3 (ACTIVE)737-57-1238 (REF)737-SL-57-044 (REF)PRODL PRR 33890-84 & PRR 34397SBB 737-57-1175P2 (REP-TASK)

SBSBSBSBSBSLPRRTA


737-57-1175P2 SB 04 RECOMMENDED A/C PART II - TIME-LIMITED REPAIR - AUXILIARY TRACK SUPPORT Superseded (Superseded / SpecialText: Rejected by previousoperator.)

737-57-1175-R0 (REF)737-57-1175-R1 (REF)737-57-1175-R2 (REF)737-57-1175-R3 (ACTIVE)737-57-1238 (REF)737-SL-57-044 (REF)PRODL PRR 33890-84 & PRR 34397SBB 737-57-1175P2 (REP-TASK)

SBSBSBSBSBSLPRRTA

This Document has been SUPERSEDED BY 737-57-1175/SB Rev.05This Document SUPERSEDES 737-57-1175P2/SB Rev.03





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1175P3 SB 04 RECOMMENDED A/C PART III - PREVENTIVE MODIFICATION Superseded (Superseded / Special

Text: Rejected by previousoperator.)

737-57-1175-R0 (REF)737-57-1175-R1 (REF)737-57-1175-R2 (REF)737-57-1175-R3 (ACTIVE)737-57-1238 (REF)737-SL-57-044 (REF)PRODL PRR 33890-84 & PRR 34397SBB 737-57-1175P3 (MOD-TASK)

SBSBSBSBSBSLPRRTA

This Document has been SUPERSEDED BY 737-57-1175/SB Rev.05Reason for this StatusSB REJECTED DUE TO NO SAFETY OR ECONOMIC BENEFIT

737-57-1175P3 SB 03 RECOMMENDED A/C PART III - PREVENTIVE MODIFICATION Rejected by Operator737-57-1175-R0 (REF)737-57-1175-R1 (REF)737-57-1175-R2 (REF)737-57-1175-R3 (ACTIVE)737-57-1238 (REF)737-SL-57-044 (REF)PRODL PRR 33890-84 & PRR 34397SBB 737-57-1175P3 (MOD-TASK)

SBSBSBSBSBSLPRRTA

737-57-1181 SB 06 RECOMMENDED A/C OUTB FLAPS - MAIN/SEQUENCING CARRIAGES/FITTINGS MODIFICATION Not Applicable by Serial Number737-57-1181-R6 (ACTIVE)PRODUCTION PRR34486

SBPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1181 SB 05 RECOMMENDED A/C OUTB FLAPS - MAIN/SEQUENCING CARRIAGES/FITTINGS MODIFICATION Superseded (Not Applicable by

Serial Number)737-57-1181-R6 (ACTIVE)PRODUCTION PRR34486

SBPRR


737-57-1181 SB 04 RECOMMENDED A/C OUTB FLAPS - MAIN/SEQUENCING CARRIAGES/FITTINGS MODIFICATION Superseded (Not Applicable bySerial Number)


SBPRR


737-57-1186 SB 00 RECOMMENDED A/C WING RIBS/RIB LOWER CHORD AT WBL 135.5 - INSP/REP/MOD Superseded (Superseded)This SB has been rejected by NAS, no safety or economic benefit.1998-11-04-R1 (REF-737-200)737-57-1186-R1 (ACTIVE)SBB 737-57-1186 (MOD-TASK)SIIA 737-252 (REF)

ADSBTABM


737-57-1186 SB 01 RECOMMENDED A/C WING RIBS/RIB LOWER CHORD AT WBL 135.5 - INSP/REP/MOD Rejected by OperatorThis SB has been rejected by NAS, no safety or economic benefit.1998-11-04-R1 (REF-737-200)737-57-1186-R1 (ACTIVE)SBB 737-57-1186 (MOD-TASK)SIIA 737-252 (REF)

ADSBTABM






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1187 SB 02 RECOMMENDED A/C OUTB MIDFLAP MAIN CARRIAGE SPINDLE BEARING ENCLOSURE REPL. Not Applicable by Serial Number

PRODUCTION PRR33890-61 PRR

737-57-1189 SB 02 RECOMMENDED A/C WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - END SEALS REP Rejected by Operator737-57A1189-R2 (ACTIVE)737-SL-57-34 (REF)PRODUCTION PRR 34398-R

SBSLPRR


737-57-1189 SB 01 RECOMMENDED A/C WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - END SEALS REP Superseded (Superseded)737-57A1189-R2 (ACTIVE)737-SL-57-34 (REF)PRODUCTION PRR 34398-R

SBSLPRR


737-57-1189 SB 00 RECOMMENDED A/C WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - END SEALS REP Superseded (Superseded)737-57A1189-R2 (ACTIVE)737-SL-57-34 (REF)PRODUCTION PRR 34398-R

SBSLPRR


737-57-1190 SB 00 RECOMMENDED A/C WINGS - REMOVABLE WINGTIP - ACCESS PANEL REPL. Not Applicable by Serial NumberPRODUCTION PRR34628 PRR 00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1192 SB 01 OPTIONAL A/C WINGS - FLIGHT SURFACES - SPOILER BLADE SEAL REPLACEMENT Ex Factory

737-57-1192-R0 (REF)737-57-1192-R01 IN02 (REF)737-57-1192-R01 IN03 (ACTIVE)PRR34605R (PRODUCTION)SBB 737-57-1192 (MOD-TASK)

SBSBSBPRRTA

This Document SUPERSEDES 737-57-1192/SB Rev.00Reason for this StatusPRODUCTION PRR 34605R

737-57-1192 SB 00 OPTIONAL A/C WINGS - FLIGHT SURFACES - SPOILER BLADE SEAL REPLACEMENT Superseded (Ex Factory)737-57-1192-R0 (REF)737-57-1192-R01 IN02 (REF)737-57-1192-R01 IN03 (ACTIVE)PRR34605R (PRODUCTION)SBB 737-57-1192 (MOD-TASK)

SBSBSBPRRTA

This Document has been SUPERSEDED BY 737-57-1192/SB Rev.01Reason for this StatusPRODUCTION PRR 34605R

737-57-1193 SB 00 RECOMMENDED A/C WINGS - SKIN-INBOARD-LOWER - TRAILING-EDGE PANEL REPLACEMENT Rejected by OperatorPRODUCTION PRR34668 PRR

737-57-1195 SB 00 RECOMMENDED A/C TRAILING EDGE FLAPS - OUTB AFTFLAP TRACK MOUNTING BOLT REPL Not Applicable by Serial Number

737-57-1196 SB 00 RECOMMENDED A/C TRAILING EDGE FLAPS - OUTB FLAP JACKSCREW FITTING BOLTS Not Applicable by Serial Number

737-57-1199 SB 01 RECOMMENDED A/C WINGS-WING RIBS-LEFT WING INDB RIB HOLE MODIFICATION Rejected by Operator





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1201 SB 00 RECOMMENDED A/C WINGS - TRAILING EDGE FLAPS - INBOARD AND OUTBOARD EXHAUST GATE

CHANGERejected by Operator

This modification is rejected by NAS, no safety or economic benefit.NAS has no reliability issues in this area.Reason for this StatusAUTO ASSIGNED

737-57-1201 SB 01 RECOMMENDED A/C WINGS - TRAILING EDGE FLAPS - INBOARD AND OUTBOARD EXHAUST GATECHANGE



737-57-1201 SB 02 RECOMMENDED A/C WINGS - TRAILING EDGE FLAPS - INBOARD AND OUTBOARD EXHAUST GATECHANGE







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1203 SB 05 MANDATORY A/C *AD* WINGS - TRAILING EDGE FLAP TRACK REPLACEMENT Closed 15.Jan.1995

This modification is applicable to LN# 1001-1910. The following LN#are Not Applicable due to PRR34707.

Compliance:This SB ensures compliance with AD § 2013-09-02 § (j),(k),(n) and (o).2002-05-07 (ACTIVE)2013-09-0234707 (PRODUCTION)737-57-1203 (REF)737-57-1203 R1 (REF)737-57-1203 R2 (REF)737-57-1203 R3 (REF)737-57-1203 R4 (REF)737-57-1203 R5 (ACTIVE)

ADADPRRSBSBSBSBSBSB

00


15.Jan.1995PerfRev.:'NOTE' / Reason: DELIVERYDOC.


737-57-1205 SB 00 RECOMMENDED A/C WINGS-TRAILING EDGE FLAPS-INB FLAP OUTBOARD TRACK-PANEL RPL Rejected by OperatorPRODUCTION PRR34823 PRR

737-57-1208 SB 00 RECOMMENDED A/C WINGS.OUTB FLAP OUTB TRACK SUPPORT Rejected by OperatorPRODUCTION MRR3579-644 MRR 00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1210 SB 04 MANDATORY A/C WINGS - CENTER WING BOX - FLOOR BEAM INSPECTION, MODIFICATION AND

REPAIRRejected by Operator

Compliance:This SB is complied with through Revision 03 of the revision.

EO 737-57-1210-01: Covers the preventive modification and terminatesthe repetitive inspections. Ref AD 2008-04-21 § (g) and (h).

EO 737-57-1210-02: Covers the repetitive inspection mandated by AD2008-04-21 § (f).

Revision 04 of the SB only applies if repair og modification isissued, and is rejected. If nas issues a repair, revision 04 of SBwill be used a source document.2008-04-21737-57-1210-01737-57-1210-02

ADEOEO

000200






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1210 SB 03 MANDATORY A/C WINGS - CENTER WING BOX - FLOOR BEAM INSPECTION, MODIFICATION AND

REPAIRClosed 07.Feb.2008

Compliance:This SB is complied with through


EO 737-57-1210-02: Covers the repetitive inspection mandated by AD2008-04-21 § (f).2008-04-21737-57-1210-01737-57-1210-02

ADEOEO

000200

This Document SUPERSEDES 737-57-1210/SB Rev.02Perform within an unlimited threshold.

737-57-1210/SB Rev.03 WINGS - CENTER WING BOX - FLOOR BEAM INSPECTION, MODIFICATION ANDREPAIR

Closed 07.Feb.2008

This Document SUPERSEDES 737-57-1210/SB Rev.02> 737-57-1210-01/EO* Rev.02 *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Closed 07.Feb.2008

This Document terminates 737-57-1210/EO Rev.02This Document has been SUPERSEDED BY 737-57-1210-01/EO Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-57-1210-01/EO* Rev.03 WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR See prev. DocstatusThis Document SUPERSEDES 737-57-1210-01/EO Rev.02This Document terminates 737-57-1210-02/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks07.Feb.2008 54539:00/H 30315/C PerfRev.:'NOTE'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusKKM 151394 ITEM: 1

> 737-57-1210-02/EO* Rev.00 FLOOR BEAM - CENTER WING BOX - DETAILED INSPECTION. *** MANDATORYINTERNAL REPETITIVE DVI INSPECTION ***

Not Applicable

This Document SUPERSEDES 737-57-1210/EO Rev.02This Document is terminated with implementation of 737-57-1210-01/EO Rev.03Reason for this StatusNOT APPLICABLE DUE TO TERMINATING ACTION PERF. ON EO 737-57-1210-01





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1210 SB 02 MANDATORY A/C *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Superseded (Closed 07.Feb.2008)

This SB is devided into 2 EO:


EO 737-57-1210-02: Covers the repetitive inspection mandated by AD2008-04-21 § (f).2008-04-21 (ACTIVE)37-SBB-57-1210 (REPETITIVE)737-57-1210-IN-01 (REF)737-57-1210-R0 (REF)737-57-1210-R1 (REF)737-57-1210-R2 (ACTIVE)SBB 737-57-1210 (MOD-TASK)

ADTASBSBSBSBTA

This Document has been SUPERSEDED BY 737-57-1210/SB Rev.03Perform BEFORE 48000/H

737-57-1210/SB Rev.02 *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Closed 07.Feb.2008This Document has been SUPERSEDED BY 737-57-1210/SB Rev.03

> 737-57-1210/EO* Rev.02 *AD* FLOOR BEAM - CENTER WING BOX - DETAILED INSPECTION. *** MANDATORYINTERNAL REPETITIVE DVI INSPECTION ***


This Document is terminated with implementation of 737-57-1210-01/EO Rev.02This Document has been SUPERSEDED BY 737-57-1210-02/EO Rev.00

> 737-57-1210-01/EO* Rev.02 *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Closed 07.Feb.2008This Document terminates 737-57-1210/EO Rev.02This Document has been SUPERSEDED BY 737-57-1210-01/EO Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







24.Oct.2014/411


737-57-1211 SB 00 RECOMMENDED A/C FOREFLAP SEQUENCE CARRIAGE INSPECTION AND REPLACEMENT Not Applicable by Serial Number737-57-1211-R0 (ACTIVE) SB

737-57-1214 SB 00 RECOMMENDED A/C WNG-ATTACH FITTINGS-NACELLE SKATE ANGLE FASTENER REPLACEMENT Rejected by Operator737-57-1214-R0 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1216 SB 02 MANDATORY A/C *AD* WINGS - MAIN LANDING GEAR BEAM FITTING INSP/REPLACEMENT Open

SB is split into 3 parts:PART I InspectionPART II N/A for NAS Airplane due to group config.PART III Fitting Insp and Replacement2002-02-082013-NM-131-AD737-57-1216 IN 04737-57-1216-01-L737-57-1216-01-R737-57-1216-L737-57-1216-RPRODUCTION PRR34964

ADNPRMSBEOEOSBSBPRR

0000000202020200

Perform within an unlimited threshold.737-57-1216/SB Rev.02 *AD* WINGS - MAIN LANDING GEAR BEAM FITTING INSP/REPLACEMENT Open> 737-57-1216-01-L/EO* Rev.02 MLG BEAM - L/H - FITTING INSPECTION AND REPLACEMENT Open

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document49779/C 273612

> 737-57-1216-01-R/EO* Rev.02 MLG BEAM - R/H - FITTING INSPECTION AND REPLACEMENT OpenThis Document SUPERSEDES 737-57-1216-02-R/EO Rev.02Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

49778/C 273613> 737-57-1216-L/EO* Rev.02 MLG BEAM - L/H - FITTING INSPECTION AND REPLACEMENT Repetitive




> 737-57-1216-R/EO* Rev.02 MLG BEAM - R/H - FITTING INSPECTION AND REPLACEMENT RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document





24.Oct.2014/411




737-57-1217 SB 02 OPTIONAL A/C WINGS T/E - OUTBOARD PANEL - LIGHTNING STRIKE PROTECTION Closed 21.Feb.2008737-57-1217737-57-1217PRODUCTION PRR 34987

SBSBPRR

000100




737-57-1218 SB 00 RECOMMENDED A/C WINGS TRAILING EDGE FLAPS-OUTBOARD Not Applicable by Serial Number737-57-1218 SB

737-57-1219 SB 02 RECOMMENDED A/C FLAP, T/E - INBOARD & OUTBOARD FLAP END PLATE INSTALLATION Closed 20.Feb.2008737-57-1219737-57-1219

SBSB

0002




737-57-1220 SB 00 RECOMMENDED A/C LOWER SPLICE BOLTS COMMON TO THE STRINGER PADDLE FITT INS/RP Not Applicable by Serial Number737-57-1220-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1221 SB 00 MANDATORY A/C *AD* LEADING EDGE PANEL SEALING AND DRAIN HOLE PLUGGING Closed 08.Dec.1995

This document is applicable to LN# 1001-2197,2199. All other LN# areNot Applicable per Boeing SB.1994-06-11(REF)1994-26-13 (ACTIVE)737-57-1221-R0 (REF)737-57-1221-R1 (REF)737-57-1221-R2 (ACTIVE)

ADADSBSBSB

0000


08.Dec.1995PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.


737-57-1222 SB 00 RECOMMENDED A/C WINGS-REPLACE THE INDB AND OUTB TOGGLE ON THE OUTB FLAPS Rejected by OperatorPRODUCTION PRR35120 PRR 00

737-57-1223 SB 00 RECOMMENDED A/C WINGS TRAILING EDGE INB TRACK FAIRING-SEAL PLATE HOOK REPL Rejected by OperatorPRODUCTION PRR35120 PRR 00

737-57-1224 SB 00 RECOMMENDED A/C WINGS-SKIN-CHANGE TO THE LOWER PANEL ON OUTB TRAILING EDGE Rejected by OperatorPRODUCTION PRR35155 PRR 00

737-57-1225 SB 00 RECOMMENDED A/C WINGS-LEADING EDGE ACCESS PANEL TO NACELLE STRUT - JOINT MOD Rejected by OperatorPRODUCTION PRR35005-49 PRR 00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1227 SB 00 OPTIONAL A/C FLAPS/SLATS/SPOILER REPLACE WITH SELF-LUBRICATING BEARINGS Superseded (Superseded)

737-57-1227-R0 (REF)737-57-1227-R1 (REF)737-57-1227-R2 (ACTIVE)PRODUCTION PRR35164-RSBB 737-57-1227 (MAINT TASK)

SBSBSBPRRTA

This Document has been SUPERSEDED BY 737-57-1227/SB Rev.01Reason for this StatusAUTO ASSIGNED

737-57-1227 SB 01 OPTIONAL A/C FLAPS/SLATS/SPOILER REPLACE WITH SELF-LUBRICATING BEARINGS Superseded (Superseded)737-57-1227-R0 (REF)737-57-1227-R1 (REF)737-57-1227-R2 (ACTIVE)PRODUCTION PRR35164-RSBB 737-57-1227 (MAINT TASK)

SBSBSBPRRTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1227 SB 02 OPTIONAL A/C FLAPS/SLATS/SPOILER REPLACE WITH SELF-LUBRICATING BEARINGS On Attrition

This SB is devided into 4 Groups.

Group 1: LN# 1-1792 which can have mod performed. Less AC in Group 3.Group 2: LN# 1793-3132 which can have mod performed. Less AC in Group3.Group 3: Covers scattered 737-300 with the SB performed in productionvia PRR.Group 3: Covers scattered 737-400 with the SB performed in productionvia PRR:

NAS has some Group 3 aircraft in the fleet. NAS has decided toperform the entire SB on attrition for the remaining group 1 and 2 AC.

For Group 3 AC modified per rev.:00 of the SB, NAS will perform thisrevision on an attrition basis as well.737-57-1227737-57-1227PRODUCTION PRR35164-R

SBSBPRR

0001


737-57-1228 SB 01 RECOMMENDED A/C TRAILING EDGE FLAPS-INBOARD FLAP-OUTBOARD TRACK, FAIRING CH Rejected by Operator737-57-1228737-SRP-57-0004 (REF)PRODUCTION PRR35005-61

SBSRPPRR

000000

737-57-1230 SB 00 RECOMMENDED A/C GROUND SPOILER SUPPORT FITTING BEARING INSPECTION AND REPAIR Rejected by Operator737-57A1230-R0 (ACTIVE) SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1231 SB 00 OPTIONAL A/C WINGS: MLG SUPPORT SUPPORT BEAM - STAB LINK AND FITTING REPL Rejected by Operator

Rejected by previous operator. NAS has no reliability issues withthis part of MLG system. Rejected by NAS.20-45-05, 20-50-03 (REF)51-20-4 (REF)7-11-11, 28-10-00, 32-13-21737-57-1073 (REF)PRODUCTION LINE PRR 35005-80

SOPMSRMAMMSBPRR

0000000000

Reason for this StatusREJECTED DUE TO NO RELIABILITY ISSUES.

737-57-1235 SB 01 RECOMMENDED A/C WINGS - FRONT SPAR - SLAT ACTUATOR SUPPORT FITTING - LUGINSPECTION/REPAIR/REPLACEMENT AND RUB STRIP INSTALLATION


This Document SUPERSEDES 737-57-1235/SB Rev.00Reason for this StatusNAS WILL NOT PERFORM THSI SB, NO RELIABILITY OR ECONOMIC BENEFIT.

737-57-1235 SB 00 RECOMMENDED A/C SLAT ACT. SUPPORT FITTING - LUG INSPECTION/REPAIR/REPLACE Superseded (Superseded)737-57-1140 (REF)737-57-1235-R1 (ACTIVE)

SBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1237 SB 03 OPTIONAL A/C WINGS TRAILING EDGE FLAP - SEAL BULKHEAD PLATE INSPECTION Closed 07.Feb.2008

737-57-1237737-57-1237737-57-1237PRODUCTION PRR35005-97

SBSBSBPRR

00010200




737-57-1238 SB 00 RECOMMENDED A/C LEADING EDGE SLATS/MAIN TRACK SIDE GUIDE BOLTS AND DOWNSTOP Superseded (Superseded)737-SRP-57-0056 (REF)PRR35005-131

SRPPRR 00


737-57-1238 SB 01 RECOMMENDED A/C WINGS - LEADING EDGE SLATS - MAIN TRACK SIDE GUIDE BOLT AND DOWNSTOPCHANGE


This document is applicable to LN# 1001-2798.737-57-1238 IN-01737-SRP-57-0056 (REF)PRR35005-131

SBSRPPRR

00

00This Document SUPERSEDES 737-57-1238/SB Rev.00

737-57-1240 SB 00 RECOMMENDED A/C WINGS - TRAILING EDGE FLAPS - SEAL RETAINER INSPECTION, AKATE ANGLEINSPECTION, AND OUTBOARD DEFECTION CONTROL RAMP REPLACEMENT






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1241 SB 02 RECOMMENDED A/C WINGS-FLIGHT SURFACES-TRAILING EDGE FLAPS INSPECTION, REPAIR AND

MODIFICATION OF FLAP LOWER SURFACES, AND PRELOAD PAD CHANGESRejected by Operator

737-57-1241737-57-1241PRODUCTION PRR35005-152

SBSBPRR

000100

737-57-1242 SB 01 RECOMMENDED A/C WINGS - INBOARD T/E OUTBOARD TRACKS - OUTB CARRIAGE INSP/MOD Open37-SBB-57-1242 (REPETITIVE)737-57-1242-IN-02 (REF)737-57-1242-IN-03 (REF)737-57-1242-R0 (REF)737-57-1242-R1 (ACTIVE)737-SRP-57-0062 (REF)PRODUCTION PRR35005-151SBB 737-57-1242 (MOD-TASK)

TASBSBSBSBSRPPRRTA

Perform within an unlimited threshold.737-57-1242/SB Rev.01 WINGS - INBOARD T/E OUTBOARD TRACKS - OUTB CARRIAGE INSP/MOD Open> 737-57-1242/EO* Rev.00 WINGS, INB T/E OUTB TRACKS, OUTB CARRIAGE BUMPER & FAIRING MODIFICATION Repetitive





> 737-57-1242-01/EO* Rev.00 WINGS - INBOARD T/E OUTBOARD TRACKS - OUTB CARRIAGE INSP/MOD Term.Action openThis Document terminates 737-57-1242/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





24.Oct.2014/411


TEOPTIONAL A/C WINGS - CENTER WING BOX - BUTTOCK LINE 45.57 LONGITUDINAL FL Not Applicable by Serial Number

737-57-1245 (ACTIVE)PRR 35349-R) (PRODUCTION)SBB 737-57-1245 (MAINT TASK)

SBPRRTA

737-57-1247 SB NOTE

RECOMMENDED A/C WINGS-OUTBOARD AFT FLAP-CAM TRACK DRIVE MECHANISM, REPLACEM. Not Applicable by Serial Number

737-57-1247 (MOD TASK)737-57-1247-R0 (ACTIVE)

TASB

737-57-1248 SB 00 OPTIONAL A/C WINGS - LEADING EDGE FLAPS - KRUGER FLAPS ADJUST LINK ASSEMB Rejected by Operator737-57-1248 (ACTIVE)SBB 737-57-1248 (MAINT TASK)

SBTA

737-57-1257 SB NOTE

RECOMMENDED A/C TRAILING EDGE FLAPS-SEALS REMOVE/REPLACE Rejected by Operator

737-57-1257 SB

737-57-1258 SB NOTE

OPTIONAL A/C TRAILING EDGE FLAPS - DEFLECTION CONTROL RAMP REMOVAL/REPL. Rejected by Operator

737-57-1258 IN 01 (ACTIVE)737-57-1258-R0 (ACTIVE)737-SRP-57-0070 (REF)MRR3579-1308 (REF)

SBSBSRPDOCR

737-57-1259 SB NOTE

RECOMMENDED A/C WINGS-TRAILING EDGE FLAPS-DELFLECTION Rejected by Operator

737-57-1259 SB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1261 SB 01 MANDATORY A/C *AD* CENTER WING BOX, INSP. OF SECONDARY FUEL VAPOR BARRIER Closed 07.Mar.2005

This document is applicable to LN# 311-3132.2005-13-15 (ACTIVE)737-57-1261-IN-01 (REF)737-57-1261-IN-02 (REF)737-57-1261-IN-03 (REF)737-57-1261-IN-04 (REF)737-57-1261-R0 (REF)737-57-1261-R1 (ACTIVE)

ADSBSBSBSBSBSB




737-57-1267 SB 00 MANDATORY A/C *AD* MAIN LANDING GEAR BEAM FITTING INSPECTION AND REPLACEMT Not Applicable by Serial Number2005-18-08 (ACTIVE)737-57-1216-R2 (REF737-57-1267-R0 (ACTIVE)737-57A1260-R2 (REF)

ADSBSBSB

737-57-1267-L SB 00 MANDATORY A/C L/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable2005-18-08737-57-1267

ADSB

737-57-1267-L/SB Rev.00 L/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable> 737-57-1267-L/EO* Rev.00 *AD* MLG BEAM SUPPORT FITTNG RETAINING PIN LUG FRACTURE INS Not Applicable by Serial Number

This Document is terminated with implementation of 737-57-1267-L-01/EO Rev.00> 737-57-1267-L-01/EO* Rev.00 L/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable by Serial Number

This Document terminates 737-57-1267-L/EO Rev.00





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1267-R SB 00 MANDATORY A/C R/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable

2005-18-08737-57-1267

ADSB

737-57-1267-R/SB Rev.00 R/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable> 737-57-1267-R/EO* Rev.00 *AD* MLG BEAM SUPPORT FITTNG RETAINING PIN LUG FRACTURE INS Not Applicable by Serial Number> 737-57-1267-R-01/EO* Rev.00 R/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable by Serial Number

737-57-1289 SB 00 MANDATORY A/C *AD* WEB INSPECTION - MAIN WHEEL WELL PRESSURE DECK Not Applicable by Serial NumberThis mod is applicable to LN# 2587,2594.2008-13-25 (ACTIVE)737-57-1289737-SRP-57-0199 (REF)

ADSBSRP

000000

737-57-1289-2 SB 00 RECOMMENDED A/C *AD* WEB REPLACEMENT - MAIN WHEEL WLL PRESSURE DECK Not Applicable2008-13-25737-57-1289

ADSB

737-57-1289-2/SB Rev.00 *AD* WEB REPLACEMENT - MAIN WHEEL WLL PRESSURE DECK Not Applicable> 737-57-1289-2/EO* Rev.00 WEB REPLACEMENT - MAIN WHEEL WELL PRESSURE DECK Not Applicable


> 737-57-1289-2-01/EO* Rev.00 *AD* WEB REPLACEMENT - MAIN WHEEL WLL PRESSURE DECK Not Applicable by Serial Number





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1296 SB 00 MANDATORY A/C WINGS - CENTER WING BOX - LONGITUDINAL FLOOR BEAM INSPECTION BETWEEN

BODY STATION 656 AND BODY STATION 727Repetitive

2008-05-06737-57-1296737-57-1296737-57-1296 IN 01

ADEOSBSB

00000100

Perform BEFORE 20000/C for the first timeThereafter perform in an interval of 7000/C

737-57-1296/SB Rev.00 WINGS - CENTER WING BOX - LONGITUDINAL FLOOR BEAM INSPECTION BETWEENBODY STATION 656 AND BODY STATION 727

Repetitive

> 737-57-1296/EO* Rev.00 NDT/DVI INSP. CTR. WING BOX - LONGITUDINAL FLOOR BEAM INSPECTION. **MANDATORY REPETITIVE INSP. BTW BODY STA 656 & STA 727 **

Repetitive

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document47570/C


737-57-1296 SB 01 MANDATORY A/C WINGS - CENTER WING BOX - LONGITUDINAL FLOOR BEAM INSPECTION BETWEENBODY STATION 656 AND BODY STATION 727


This revision of the SB (01) only includes revised repairinstructions for the found cracks. NAS only performs inspections.Should a repair be required, NAS will issue a repair per rev.:01 ofthe SB.2008-05-06737-57-1296737-57-1296 IN-01737-57-1296 IN-02

ADSBSBSB

00000000






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57-1318 SB 00 MANDATORY A/C WINGS - LANDING GEAR SUPPORT BEAM - REAR SPAR AND AFT SUPPORT FITTING

INSPECTIONOpen

Applicable to all B737CL.NAS only has aircraft in Group 6, Config 2 and Group 7.This SB is divided into 2 EO:737-57-1318-01: Group 6 Config 2 AC.737-57-1318-02: Group 6 Config 2 AC.737-57-1318-03: Group 7737-57-1318-04: Group 7737-57-1318-05: Group 7 AC.MSN:29072 with MLG drop May 2015.Rejected

No time limit on SB, as the time limit is differentiated, refer to EOfor time limits.120S-14-2512013-NM-131-AD2014-03-06737-57-1216737-57-1318-01737-57-1318-02737-57-1318-03737-57-1318-04737-57-1318-05

AMOCNPRMADSBEOEOEOEOEO

000000020000000000

Perform within an unlimited threshold.737-57-1318/SB Rev.00 WINGS - LANDING GEAR SUPPORT BEAM - REAR SPAR AND AFT SUPPORT FITTING

INSPECTIONOpen

> 737-57-1318-01/EO* Rev.00 MLG SUPPORT BEAM -NDT INSPECTION OF REAR SPAR AND AFT SUPPORT FITTINGSURFACE INSPECTION OF LH/RH FITTING

Open






24.Oct.2014/411


47873/CPerform initially within (effective from09.Apr.2014) (F) 4500/C /Interval(F):4500/C

> 737-57-1318-02/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTING OPENHOLE HFEC INSP 12 FASTENER HOLES

Open

This Document terminates 737-57-1318-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

61373/CPerform initially within (effective from09.Apr.2014) (F) 18000/C /Interval(F):24000/C

> 737-57-1318-03/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTINGSURFACE INSPECTION OF LH/RH FITTING


This Document is terminated with implementation of 737-57-1318-04/EO Rev.00> 737-57-1318-04/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTING OPEN

HOLE HFEC INSP 12 FASTENER HOLESNot Applicable by Serial Number

This Document terminates 737-57-1318-03/EO Rev.00> 737-57-1318-05/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTING OPEN

HOLE HFEC INSP 12 FASTENER HOLESNot Applicable by Serial Number

737-57A1079 SB 03 MANDATORY A/C *AD* WINGS - FLAP TRACK SUPPORT FITTING ATTACH BOLTS REPLCT. Superseded (Not Applicable bySerial Number)

1990-17-20737-57A1079737-57A1079 R1737-57A1079 R2737-57A1079 R3737-57A1079 R4

ADSBSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1079 SB 04 MANDATORY A/C *AD* WINGS - FLAP TRACK SUPPORT FITTING ATTACH BOLTS REPLCT. Not Applicable by Serial Number

1990-17-20737-57A1079737-57A1079 R1737-57A1079 R2737-57A1079 R3737-57A1079 R4

ADSBSBSBSBSB



1990-17-20737-57A1079737-57A1079 R1737-57A1079 R2737-57A1079 R3737-57A1079 R4

ADSBSBSBSBSB



1990-17-20737-57A1079737-57A1079 R1737-57A1079 R2737-57A1079 R3737-57A1079 R4

ADSBSBSBSBSB






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1079 SB 01 MANDATORY A/C *AD* WINGS - FLAP TRACK SUPPORT FITTING ATTACH BOLTS REPLCT. Superseded (Not Applicable by

Serial Number)1990-17-20737-57A1079737-57A1079 R1737-57A1079 R2737-57A1079 R3737-57A1079 R4

ADSBSBSBSBSB


737-57A1197 SB 00 MANDATORY A/C *AD* WINGS L.E. - LDG. LIGHT CAVITY VAPOR BARRIER SEAL INSTL Not Applicable by Serial Number1990-20-22 (ACTIVE)737-57A1197-R0 (ACTIVE)SBB 737-57A1197 (MOD-TASK)

ADSBTA

737-57A1202 SB 01 MANDATORY A/C *AD* SUPPORT FITTING ATTACH BOLT & NUT INSP./REPLACEMENT. Not Applicable by Serial Number1989-18-51 (SUPERSEDED)1990-14-04 (SUPERSEDED)1991-09-17 (ACTIVE)737-57A1202-R0 (REF)737-57A1202-R1 (ACTIVE)SBB 737-57A1202 (MOD TASK)

ADADADSBSBTA

737-57A1208 SB 00 MANDATORY A/C *AD* OUTBOARD FLAP SUPPORT FITTING ATTACH BOLTS - INSP./REPL Not Applicable by Serial NumberThis mod is applicable for LN# 1001-1762. The following LN# are Notapplicable Per MRR3579-644.1990-24-04 (ACTIVE)737-57A1208-R0 (ACTIVE)PRODUCTION MRR3579-644

ADSBPRR





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1218 SB 03 MANDATORY COMP *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFE

LIMITINGSuperseded (Superseded)

This EO controls the OH and life limit of the Flap CarriageNPRM 2002-NM-219-AD AD 00This Document has been SUPERSEDED BY 737-57A1218/SB Rev.05Affected Rotables (Part No/Serial No/Position) Status65-46481-106 / 4914WG Pos=#7 (KKM) Superseded65-46481-116 / 1783 Pos=#8 (KKM) Superseded65-46481-145 / B5121 Pos=#1 (KKM) Superseded65-46481-119 / B3554 Pos=#2 (KKM) Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1218 SB 06 MANDATORY COMP WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFE

LIMITINGOpen

This SB controls the OH and life limit of the Flap Carriag

This SB rev 06 is approved as an AMOC to SB Rev:05 referenced in AD:The Manager of the FAA Seattle Aircraft Certification Office (ACO)approves the accomplishment ofthe applicable inspections,investigative and corrective actions with the corresponding compliancetimes specified in Service Bulletin 737-57A1218 Revision 6 as an AMOCto the accomplishment of the applicable inspections, investigativeand corrective actions with the corresponding compliance timesspecified in Service Bulletin 737-57A1218 Revision 5 required byparagraphs (i), (k), (l), (o), (p), (q), (r), and (s) of AD2010-15-08 . When this service bulletin specifies contacting Boeingfor repair instruction, the repair instructions must be approved bythe FAA in accordance with paragraph (t) of the AD. Allprovisions of AD 2010-15-08 that are not specifically referenced inthis paragraph remain fully applicable and must be complied with.2014-05-12NPRM 2002-NM-219-AD

ADAD

0000


737-57A1218/SB Rev.06 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFELIMITING

Open

This Document SUPERSEDES 737-57A1218/SB Rev.05> 737-57A1218-01/EO* Rev.00 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL Open


65-46481-116 / 1783 Pos=#8 (KKM)Repetitive / Next Due:11.Jan.2022 38297/C/ Last Performed:13.Jan.2014 0/CRefDocument:FAA 8130-3 026010 Rev.00

65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due:14.May.2021 22077/C





24.Oct.2014/411


65-46481-119 / B3554 Pos=#2 (KKM)

Repetitive / Next Due:05.Oct.2020 22073/C/ Last Performed:07.Oct.2012 0/CRefDocument:FAA 8130-3 024128-2Rev.00

65-46481-106 / 4914WG Pos=#7 (KKM)

Repetitive / Next Due:05.Feb.2019 37305/C/ Last Performed:07.Feb.2011 35283:00/H25305/C RefDocument:EASA F1001282424 Rev.00

> 737-57A1218-02/EO* Rev.01 WINGS- TE OUTB FLAP CARRIAGE SPINDELS LIFE LIMIT FOR FLAP CARRIAGES WITHDOCUMENTED HISTORY

Open

This Document SUPERSEDES 737-57A1218-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-46481-119 / B3554 Pos=#2 (KKM) Open / Next Due: 40000/C65-46481-106 / 4914WG Pos=#7 (KKM) Open / Next Due: 40000/C65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due: 40000/C65-46481-116 / 1783 Pos=#8 (KKM) Open / Next Due: 40000/C

> 737-57A1218-03/EO* Rev.00 WINGS- TE OUTB FLAP CARRIAGE SPINDELS LIFE LIMIT FOR FLAP CARRIAGES WITHUN-DOCUMENTED HISTORY

Not Applicable / Special Text: Thiscomp.is Not Applicable due toKNOWN history,ref EO737-57A1218-02


65-46481-116 / 1783 Pos=#8 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: THISCOMP.IS NOT APPLICABLE DUE TOKNOWN HISTORY,REF EO737-57A1218-02





24.Oct.2014/411


65-46481-145 / B5121 Pos=#1 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: EO737-57A1218-02 COVER CARRIAGESWITH KNOWN HISTORY

65-46481-119 / B3554 Pos=#2 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: NA DUETO KNOWN HISTORY, REFER TO EO737-57A1218-02

65-46481-106 / 4914WG Pos=#7 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: NOTAPPLICABLE SINCE HISTORY ISKNOWN, REF EO 737-57A1218-02

737-57A1218 SB 00 MANDATORY COMP *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFELIMITING


This EO controls the OH and life limit of the Flap CarriageNPRM 2002-NM-219-AD AD 00This Document has been SUPERSEDED BY 737-57A1218/SB Rev.05Affected Rotables (Part No/Serial No/Position) Status65-46481-145 / B5121 Pos=#1 (KKM) Superseded65-46481-119 / B3554 Pos=#2 (KKM) Superseded65-46481-106 / 4914WG Pos=#7 (KKM) Superseded65-46481-116 / 1783 Pos=#8 (KKM) Superseded





24.Oct.2014/411



This EO controls the OH and life limit of the Flap CarriageNPRM 2002-NM-219-AD AD 00This Document has been SUPERSEDED BY 737-57A1218/SB Rev.05Affected Rotables (Part No/Serial No/Position) Status65-46481-119 / B3554 Pos=#2 (KKM) Superseded65-46481-116 / 1783 Pos=#8 (KKM) Superseded65-46481-145 / B5121 Pos=#1 (KKM) Superseded65-46481-106 / 4914WG Pos=#7 (KKM) Superseded

737-57A1218 SB 04 MANDATORY COMP *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFELIMITING


This EO controls the OH and life limit of the Flap CarriageNPRM 2002-NM-219-AD AD 00This Document has been SUPERSEDED BY 737-57A1218/SB Rev.05Affected Rotables (Part No/Serial No/Position) Status65-46481-145 / B5121 Pos=#1 (KKM) Superseded65-46481-116 / 1783 Pos=#8 (KKM) Superseded65-46481-119 / B3554 Pos=#2 (KKM) Superseded65-46481-106 / 4914WG Pos=#7 (KKM) Superseded





24.Oct.2014/411



This EO controls the OH and life limit of the Flap CarriageNPRM 2002-NM-219-AD AD 00This Document has been SUPERSEDED BY 737-57A1218/SB Rev.05Affected Rotables (Part No/Serial No/Position) Status65-46481-145 / B5121 Pos=#1 (KKM) Superseded65-46481-119 / B3554 Pos=#2 (KKM) Superseded65-46481-116 / 1783 Pos=#8 (KKM) Superseded65-46481-106 / 4914WG Pos=#7 (KKM) Superseded

737-57A1218 SB 05 MANDATORY COMP WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFELIMITING


This SB controls the OH and life limit of the Flap CarriageNPRM 2002-NM-219-AD AD 00This Document SUPERSEDES 737-57A1218/SB Rev.00This Document SUPERSEDES 737-57A1218/SB Rev.01This Document SUPERSEDES 737-57A1218/SB Rev.02This Document SUPERSEDES 737-57A1218/SB Rev.03This Document SUPERSEDES 737-57A1218/SB Rev.04This Document has been SUPERSEDED BY 737-57A1218/SB Rev.06Affected Rotables (Part No/Serial No/Position) Status65-46481-119 / B3554 Pos=#2 (KKM) Superseded65-46481-145 / B5121 Pos=#1 (KKM) Superseded65-46481-116 / 1783 Pos=#8 (KKM) Superseded65-46481-106 / 4914WG Pos=#7 (KKM) Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1249 SB 02 MANDATORY A/C *AD* OUTB. FLAP, INBOARD TRACK INSP/OH/REPLACEMENT WBL 254 Cancelled (Cancelled)

2002-05-07737-57A1249-R2 (REPLACED)737-57A1271-R1 (ACTIVE)

ADSBSB

00

This Document has been CANCELLED BY 737-57A1271/SB Rev.01

737-57A1260 SB 02 MANDATORY A/C MLG SUPPORT BEAM RETAINING PIN - BOLT & NUT REPLACEMENT Closed 30.Mar.20012002-02-08737-57A1260737-57A1260 R1737-57A1260 R2

ADSBSBSB








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1266 SB 02 MANDATORY A/C WINGS - ATTACH FITTINGS - LANDING GEAR ATTACH FITTINGS, MLG BEAM

OUTBOARD STABILIZING FITTING REPLACEMENTOpen

All NAS AC are group 8 AC.Therefore only Part II and repetitive 10 year inspections areapplicable. This per AD § (g).11-1072 (MSN 27285 ONLY)2008-08-10 (ACTIVE)737-57A1266737-57A1266737-57A1266737-57A1266 AMOC-01737-57A1266 IN-01737-57A1266-01PRODUCTION PRR35005-234RS

TDADSBEOSBSBSBEOPRR

0000000101OO000200

This Document SUPERSEDES 737-57A1266/SB Rev.01Perform BEFORE 18.May.2011

737-57A1266/SB Rev.02 WINGS - ATTACH FITTINGS - LANDING GEAR ATTACH FITTINGS, MLG BEAMOUTBOARD STABILIZING FITTING REPLACEMENT

Open

This Document SUPERSEDES 737-57A1266/SB Rev.01> 11-1072/TD* Rev.00 INSTALLATION OF FREEZEPLUG IN REAR SPAR, MSN 27285 FINAL REPAIR OF ONE

HOLE WHILE PERFORMING SB 737-57A1266Not Applicable by Serial Number

> 737-57A1266/EO* Rev.01 *AD* VISUAL INSP. OF THE OUTB STABILIZING FITTING, WALKING B HANGER, ANDREAR SPAR ATTACH FITTING

Cancelled


> 737-57A1266-01/EO* Rev.02 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT See prev. DocstatusThis Document SUPERSEDES 737-57A1266-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks11.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusKKM 150397 ITEM: 1

> 737-57A1266-02/EO* Rev.00 VISUAL INSP. OF THE OUTB STABILIZING FITTING, WALKING B HANGER, AND REARSPAR ATTACH FITTING

Open


11.Mar.2015 489501Perform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D /Interval(F):3650/D





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1266 SB 01 MANDATORY A/C *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Superseded (Cancelled)

2008-08-10 (ACTIVE)37-SBB-57A1266 (REP TASK)737-57A1266-IN-01 (REF)737-57A1266-R0 (REF)737-57A1266-R1 (ACTIVE)PRODUCTION PRR35005-234RSSBB 737-57A1266 (MAINT TASK)

ADTASBSBSBPRRTA

This Document SUPERSEDES 737-57A1266/SB Rev.00This Document has been SUPERSEDED BY 737-57A1266/SB Rev.02Perform BEFORE 18.May.2011

737-57A1266/SB Rev.01 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT CancelledThis Document SUPERSEDES 737-57A1266/SB Rev.00This Document has been SUPERSEDED BY 737-57A1266/SB Rev.02


Cancelled


> 737-57A1266-01/EO* Rev.01 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT SupersededThis Document SUPERSEDES 737-57A1266-01/EO Rev.00This Document has been SUPERSEDED BY 737-57A1266-01/EO Rev.02





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1266 SB 00 MANDATORY A/C *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Superseded (Closed 11.Mar.2005)

2008-08-10 (ACTIVE)37-SBB-57A1266 (REP TASK)737-57A1266-IN-01 (REF)737-57A1266-R0 (REF)737-57A1266-R1 (ACTIVE)PRODUCTION PRR35005-234RSSBB 737-57A1266 (MAINT TASK)

ADTASBSBSBPRRTA

This Document has been SUPERSEDED BY 737-57A1266/SB Rev.01Perform BEFORE 18.May.2011

737-57A1266/SB Rev.00 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Closed 11.Mar.2005This Document has been SUPERSEDED BY 737-57A1266/SB Rev.01


Cancelled


> 737-57A1266-01/EO* Rev.00 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Closed 11.Mar.2005This Document has been SUPERSEDED BY 737-57A1266-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

11.Mar.2005 46130:00/H 23575/CKKM 150397ITEM: 1





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1269 SB 00 MANDATORY A/C *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Superseded (Superseded)

2005-20-01 (ACTIVE)37-SBB-57A1269P1 (REPETITIVE)737-57A1269 IN 01 (REF)737-57A1269 IN 02 (REF)737-57A1269-R0 (REF)737-57A1269-R1 (ACTIVE)SBB 737-57A1269 (MOD TASK)

ADTASBSBSBSBTA






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1269 SB 01 MANDATORY A/C *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Open

SB 737-57A1269 IN-03 introduces SB 737-47-1007 as an AMOC to AD2005-20-01. SB 737-47-1007 is rejected due to cost.2005-20-01 (ACTIVE)737-47-1007737-57A1269737-57A1269 IN-01737-57A1269 IN-02737-57A1269 IN-03737-57A1269-01737-57A1269P1

ADSBSBSBSBSBEOEO

0000000000000101


737-57A1269/SB Rev.01 *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. OpenThis Document SUPERSEDES 737-57A1269/SB Rev.00

> 737-57A1269-01/EO* Rev.01 *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Term.Action openDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMITPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Apr.2006 49193:00/H 26146/C PerfRev.:'NOTE'

> 737-57A1269P1/EO* Rev.01 *AD* WINGS CNTR SECT. REAR SPAR. STIFFNER L/H & R/H BBL 6.1 *** MANDATORYREPETITIVE INSPECTION ***

Repetitive








24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1271 SB 03 MANDATORY COMP WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - TRAILING EDGE FLAPS

OUTBOARD FLAP, INBOARD TRACK INSPECTION/OVERHAUL/REPLACEMENTRepetitive

EO 737-57A1271-1 covers the repetitive inspections of the flap tracksat given interval.

EO 737-57A1271-2 covers the replacement of flap tracks at giveninterval.

RELATED AD ONLY:Federal Aviation Administration Airworthiness Directive (AD)78-13-07, Amendment 39-3253; AD 2000-25-07, Amendment 39-1204; AD2002-05-07, Amendment 39-12675; and AD 90-06-02, Amendment 39-6489are related to this service bulletin.

Compliance to current AD 2013-09-02:This SB and its EOs ensures complaince with AD § (n),(p),(q),(r),(s),(t) and (u).2013-09-02737-57A1271737-57A1271737-57A1271737-57A1271-1737-57A1271-2737-SRP-57-0131 (REF)PRODUCTION PRR35005-238RS

ADSBSBSBEOEOSRPPRR

0000010201010000


737-57A1271/SB Rev.03 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - TRAILING EDGE FLAPSOUTBOARD FLAP, INBOARD TRACK INSPECTION/OVERHAUL/REPLACEMENT

Repetitive






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-57A1271-1/EO* Rev.01 OUTB. TRAILING EDGE FLAPS, INB. TRACK INSPECTION AT WB 254 INSTR FOR VISUAL

AND EDDY CURRENT INSP. FLAP TRACKS (APP TO #2&#7)Repetitive


65C34812-6 / E-2487 Pos=#2 (KKM)

Repetitive / Next Due:22.Jan.2018 10000/C/ Last Performed:22.Jan.2014RefDocument:FORM 8130-3 026156Rev.01

65C34812-6 / E-3004 Pos=#7 (KKM)Repetitive / Next Due:21.Jan.2018 10000/C/ Last Performed:22.Jan.2014RefDocument:N/A Rev.01

> 737-57A1271-2/EO* Rev.01 OUTB TRAILING EDGE FLAPS, INB TRACK,OVERHAUL/REPLM. AT WBL 254 RepetitiveAffected Rotables (Part No/Serial No/Position) Status

65C34812-6 / E-2487 Pos=#2 (KKM)

Repetitive / Next Due:20.Jan.2022 20000/C/ Last Performed:22.Jan.2014 0/CRefDocument:FORM 8130-3 026156Rev.01

65C34812-6 / E-3004 Pos=#7 (KKM)Repetitive / Next Due:21.Jan.2022 20000/C/ Last Performed:22.Jan.2014 0/CRefDocument:FAA FORM 026155 Rev.01

> 737-57A1271-3/EO* Rev.00 OUTB. TRAILING EDGE FLAPS, INB. TRACK INSPECTION AT WB 254 INSTR FOR VISUALAND EDDY CURRENT INSP. FLAP TRACKS (APP TO #2&#7)

Not Applicable


65C34812-6 / E-3004 Pos=#7 (KKM)

Not Applicable / Reason: AD §(Q)ALLOWS FOR LATE INITIALINSPECTION, NAS USECONSERVATIVE §(U)

65C34812-6 / E-2487 Pos=#2 (KKM)

Not Applicable / Reason: AD §(Q)ALLOWS FOR LATE INITIALINSPECTION, NAS USECONSERVATIVE §(U)





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1271 SB 01 MANDATORY COMP OUTB. FLAP, INBOARD TRACK INSP/OH/REPLACEMENT WBL 254 Superseded (Superseded)


EO 737-57A1271-2 covers the replacement of flap tracks at giveninterval.1978-13-07 (SUPERSEDED)2002-05-07 (ACTIVE)737-57A1271-IN-01 (REF)737-57A1271-R0 (REF)737-57A1271-R1 (ACTIVE)737-SRP-57-0131 (REF)PRODUCTION PRR35005-238RS

ADADSBSBSBSRPPRR

This Document CANCELS 737-57A1249/SB Rev.02This Document has been SUPERSEDED BY 737-57A1271/SB Rev.02Affected Rotables (Part No/Serial No/Position) Status65C34812-6 / E-3004 Pos=#7 (KKM) Superseded65C34812-6 / E-2487 Pos=#2 (KKM) Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1271 SB 02 MANDATORY COMP WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - TRAILING EDGE FLAPS

OUTBOARD FLAP, INBOARD TRACK INSPECTION/OVERHAUL/REPLACEMENTSuperseded (Superseded)


EO 737-57A1271-2 covers the replacement of flap tracks at giveninterval.

RELATED AD ONLY:Federal Aviation Administration Airworthiness Directive (AD)78-13-07, Amendment 39-3253; AD 2000-25-07, Amendment 39-1204; AD2002-05-07, Amendment 39-12675; and AD 90-06-02, Amendment 39-6489are related to this service bulletin.737-57A1271737-57A1271737-57A1271-1737-57A1271-2737-57A1271-IN-01 (REF)737-SRP-57-0131 (REF)PRODUCTION PRR35005-238RS

SBSBEOEOSBSRPPRR

00010101000000

This Document SUPERSEDES 737-57A1271/SB Rev.01This Document has been SUPERSEDED BY 737-57A1271/SB Rev.03Affected Rotables (Part No/Serial No/Position) Status65C34812-6 / E-2487 Pos=#2 (KKM) Superseded65C34812-6 / E-3004 Pos=#7 (KKM) Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1277 SB 03 MANDATORY A/C WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP CARRIAGE SPINDLE - INSPECTION

FOR CRACKINGOpen

Inspection per Revision 01 is mandated by AD 2010-15-08.This SB is Rejected until new AD arrives.

This inspection is divided into two EO.EO 737-57A1277-01 covers the repetitive NDT inspection.EO 737-57A1277-02 covers the repetitive Gap Check inspection.2010-15-08737-57A1277-01737-57A1277-02

ADEOEO

000000

This Document SUPERSEDES 737-57A1277/SB Rev.01This Document SUPERSEDES 737-57A1277/SB Rev.02Perform within an unlimited threshold.

737-57A1277/SB Rev.03 WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP CARRIAGE SPINDLE - INSPECTIONFOR CRACKING

Open

This Document SUPERSEDES 737-57A1277/SB Rev.01This Document SUPERSEDES 737-57A1277/SB Rev.02

> 737-57A1277-01/EO* Rev.01 NDT OF TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. OpenThis Document SUPERSEDES 737-57A1277-01/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status

65-46481-106 / 4914WG Pos=#7 (KKM)Repetitive / Next Due:05.Apr.2015 33501/C/ Last Performed:07.Oct.2014 44068:36/H32001/C W/O:15483811 Rev.01

65-46481-116 / 1783 Pos=#8 (KKM)Repetitive / Next Due: 29297/C / LastPerformed:13.Jan.2014 0/CRefDocument:FAA 8130-3 026010 Rev.00

65-46481-119 / B3554 Pos=#2 (KKM)Repetitive / Next Due:04.Apr.2015 15497/C/ Last Performed:06.Oct.2014 5180:36/H13997/C W/O:15483875 Rev.01

65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due: 13077/C





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status> 737-57A1277-02/EO* Rev.01 WINGS- TE OUTB FLAP GAP CHECK & CARRIAGE SPINDELS INSP FOR CRACKS. Repetitive

This Document SUPERSEDES 737-57A1277-02/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

21.Oct.2014 44634/CPerform initially before(F) 140/C /Interval(L):140/C or 14/D


07.Oct.2014 73319:36/H 44494/C 15665000,Was due at: 44533/C and 26.Sep.2014PerfRev.:'01'

> 737-57A1277-03/EO* Rev.00 NDT OF TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. Not ApplicableAffected Rotables (Part No/Serial No/Position) Status

65-46481-145 / B5121 Pos=#1 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

65-46481-119 / B3554 Pos=#2 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

65-46481-106 / 4914WG Pos=#7 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

65-46481-116 / 1783 Pos=#8 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

737-57A1277 SB 00 MANDATORY A/C *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAPCHECK







24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1277 SB 02 MANDATORY A/C WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP CARRIAGE SPINDLE - INSPECTION

FOR CRACKINGSuperseded (Superseded)

This SB is Rejected until new AD arrives.

This inspection is divided into two EO.EO 737-57A1277-01 covers the repetitive NDT inspection.EO 737-57A1277-02 covers the repetitive Gap Check inspection.737-57A1277 IN-03 SB 00This Document has been SUPERSEDED BY 737-57A1277/SB Rev.03Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1277 SB 01 MANDATORY A/C WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAP CHECK Superseded (Superseded)

This inspection is divided into two EO.EO 737-57A1277-01 covers the repetitive NDT inspection.EO 737-57A1277-02 covers the repetitive Gap Check inspection.2010-15-08737-57A1277-01737-57A1277-02

ADEOEO

000000


737-57A1277/SB Rev.01 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAP CHECK SupersededThis Document SUPERSEDES 737-57A1277/SB Rev.00This Document has been SUPERSEDED BY 737-57A1277/SB Rev.03

> 737-57A1277-01/EO* Rev.00 NDT OF TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. SupersededThis Document has been SUPERSEDED BY 737-57A1277-01/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status

65-46481-145 / B5121 Pos=#1 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

65-46481-119 / B3554 Pos=#2 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

65-46481-116 / 1783 Pos=#8 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

65-46481-106 / 4914WG Pos=#7 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

> 737-57A1277-02/EO* Rev.00 WINGS- TE OUTB FLAP GAP CHECK & CARRIAGE SPINDELS INSP FOR CRACKS. SupersededThis Document has been SUPERSEDED BY 737-57A1277-02/EO Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1301 SB 03 MANDATORY A/C WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - MAIN TRACK DOWNSTOP

ASSEMBLY INSPECTION AND MODIFICATIONOpen

2008-06-292011-NM-071-AD737-57A1301737-57A1301737-57A1301737-57A1301 IN-01737-57A1301-01737-57A1301-02737-57A1301-03

ADADSBSBSBSBEOEOEO

000000010200010000


737-57A1301/SB Rev.03 WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - MAIN TRACK DOWNSTOPASSEMBLY INSPECTION AND MODIFICATION

Open

This Document SUPERSEDES 737-57A1301/SB Rev.02> 737-57A1301-01/EO* Rev.01 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY MODIFICATION Open

This Document SUPERSEDES 737-57A1301-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

19.Sep.2019 57386/CPerform initially within (effective from20.Sep.2013) (F) 15000/C or 2190/D

> 737-57A1301-02/EO* Rev.00 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION RepetitiveThis Document SUPERSEDES 737-57A1301/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> 737-57A1301-03/EO* Rev.00 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY DET INSPECTION FOR FOD Closed 01.Nov.2012 W/O:273638Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status01.Nov.2012 68139:00/H 40570/C 273638, N/A Was due at: 31.Jul.2013 PerfRev.:'00'

737-57A1301 SB 01 MANDATORY A/C *AD* LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION Superseded (Superseded)2008-06-29 (ACTIVE)737-57A1301737-57A1301 IN-01737-57A1301-R0 (SUPERSEEDED)

ADSBSBSB

00010000






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1301 SB 02 MANDATORY A/C WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - MAIN TRACK DOWNSTOP

ASSEMBLY INSPECTION AND MODIFICATIONSuperseded (Repetitive)

2008-06-29 (ACTIVE)737-57A1301737-57A1301 IN-01737-57A1301-R0 (SUPERSEEDED)

ADSBSBSB

00010000


737-57A1301/SB Rev.02 WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - MAIN TRACK DOWNSTOPASSEMBLY INSPECTION AND MODIFICATION

Repetitive


> 737-57A1301/EO* Rev.00 *AD* LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION CancelledThis Document has been SUPERSEDED BY 737-57A1301-02/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks27.Jun.2011 64534:00/H 37798/C 205184, N/A Was due at: 39508/C PerfRev.:'00'Reason for this StatusManually deassigned after Document Cancelled/Superseeded

> 737-57A1301-01/EO* Rev.00 *AD* LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION SupersededThis Document has been SUPERSEDED BY 737-57A1301-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Apr.2008 54936:00/H 30624/CPerfRev.:'NOTE' / Reason: IN MAINTPROG


> 737-57A1301-02/EO* Rev.00 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION RepetitiveThis Document SUPERSEDES 737-57A1301/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Feb.2014 71572:00/H 43151/C 489494, N/A Was due at: 45070/C PerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1304 SB 01 MANDATORY A/C OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Closed 05.Jun.2008

Perform within an unlimited threshold.737-57A1304/SB Rev.01 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Closed 05.Jun.2008> 737-57A1304-01/EO* Rev.00 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Closed 05.Jun.2008


05.Jun.2008 47535:00/H 31034/CACCOMPLISHED ONWO:151472

PerfRev.:'00'

> 737-57A1304-02/EO* Rev.00 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Not Applicable / Special Text: ThisCarriage is Not Applicable by PN/SN.


65C27409-27 / B3554 Pos=#2 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN.

65C27409-23 / 4914WG Pos=#7 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-25 / 1783 Pos=#8 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-33 / B5121 Pos=#1 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

> 737-57A1304-03/EO* Rev.00 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Not Applicable / Special Text: ThisCarriage is Not Applicable by PN/SN.


65C27409-27 / B3554 Pos=#2 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN.

65C27409-25 / 1783 Pos=#8 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED





24.Oct.2014/411


65C27409-23 / 4914WG Pos=#7 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-33 / B5121 Pos=#1 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

737-57A1319 SB 00 RECOMMENDED COMP WINGS - INSPECTION FOR CORROSION - OUTBOARD FLAP, CARRIAGE SPINDLE Superseded (Not Applicable by LineNumber)

Due to more reports of failed HVOF coatings, all HVOF coated carraigespindles must be inspected within 90 days, repeat insp. every 180days.

SB allows for a document review to determine which carriage spindlesto inspect. NAS treats this SB as a component SB as we have track ofall sub ASSY PN.This Document has been SUPERSEDED BY 737-57A1319/SB Rev.01Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-57A1319 SB 01 MANDATORY COMP WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP, CARRIAGE SPINDLE - INSPECTION

FOR CORROSIONNot Applicable

Due to more reports of failed HVOF coatings, all HVOF coated carraigespindles must be inspected within 90 days, repeat insp. every 180days.

SB allows for a document review to determine which carriage spindlesto inspect. NAS treats this SB as a component SB as we have track ofall sub ASSY PN.2012-13-07737-57A1319-01737-57A1319-02

ADEOEO

000000


737-57A1319/SB Rev.01 WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP, CARRIAGE SPINDLE - INSPECTIONFOR CORROSION

Not Applicable

This Document SUPERSEDES 737-57A1319/SB Rev.00> 737-57A1319-01/EO* Rev.00 WINGS - INSPECTION FOR CORROSION - OUTBOARD FLAP, CARRIAGE SPINDLE Not Applicable

This Document is terminated with implementation of 737-57A1319-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

> 737-57A1319-02/EO* Rev.00 WINGS - REPLACEMENT OF OUTBOARD FLAP, CARRIAGE SPINDLE Not ApplicableThis Document terminates 737-57A1319-01/EO Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

737-71-1149 SB 02 RECOMMENDED A/C THRUST REVERSER HINGE FITTING ISOLATORS Not Applicable by Serial Number737-71-1149-R0PRODUCTION PRR33944-02R

SBPRR





24.Oct.2014/411


TERECOMMENDED A/C ENGINE REPLACEMENT CFM56-3-B1 WITH CFM56-3B-2 ENGINES Not Applicable by Serial Number

737-71-1171MC7200MK3008

SBPRR

737-71-1176 SB NOTE

RECOMMENDED A/C POWER PLANT-GENERAL-INTERMIX OF ONE Rejected by Operator

737-71-1176 SB

737-71-1233 SB NOTE

RECOMMENDED A/C INTERMIX OF ENG/SUBST. OF ENG OR CHANGE TO Rejected by Operator

737-71-1233 SB

737-71-1238 SB NOTE

RECOMMENDED A/C POWER PLANT-GENERAL-ENGINE BLEED DUCT Rejected by Operator

737-71-1238 SB

737-71-1269 SB NOTE

RECOMMENDED A/C POWER PLANT-GENERAL-INTERMIX OF ONE Rejected by Operator

737-71-1269 SB

737-71-1270 SB 00 RECOMMENDED A/C POWER PLANT-COWLING-FAN COWL Rejected by Operator737-71-1270 SB





24.Oct.2014/411


TERECOMMENDED A/C INST.OF 45% N1 PLACARD WITH REPLACEMENT OF Closed 10.May.1993

1989-25-02 (REF)737-71-1273-R0 (ACTIVE)PRODUCTION PRR34633-10

ADSBPRR


10.May.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-71-1285 SB NOTE

RECOMMENDED A/C ELECTRIAL HARNESS CONNECTOR DISCONNECT Closed 09.Dec.1992




737-71-1288 SB NOTE

RECOMMENDED A/C POWER PLANT-GENERAL- Rejected by Operator

737-71-1288 SB

737-71-1336 SB NOTE

RECOMMENDED A/C RUBSTRIP INSTALLATION AT FAN COWL SUPPORT Rejected by Operator

737-71-1336 SB





24.Oct.2014/411


TEOPTIONAL A/C REV. OF CERTIFIED TAKEOFF AND LANDING ALT. LIM. FOR CFM56 Rejected by Operator

737-71-1475-R0 (ACTIVE)CFM56-3/3B/3C S/B 72-0982CFM56-3/3B/3C S/B 72-1000MC7200MK3615 (BOEING-ECM)

SBCFSBCFSBDOCR

737-71-1523 SB NOTE

OPTIONAL A/C CERTIFIED TAKEOFF AND LANDING ALTITUDE LIMITATION FOR CFM56 Rejected by Operator

737-71-1523-R0 (ACTIVE)CFM56-3/3B/3C S/B 72-1031MC7200MK3586 (BOEING-ECM)

SBCFSBDOCR

737-71-1608 SB 00 OPTIONAL COMP INSP. & REP.OF THE ENG. BUILD UP BRACKETS TO PREVENT DAMAGE Not Applicable by Line Number737-71-1608-R0 SBAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

737-71-1625 SB 00 OPTIONAL A/C POWER PLANT - POWER PLANT - CHANGE THE OPERATIONAL THRUST RATING OFCFM56-7B ENGINES FROM CFM56-7B24 TO CFM56-7B26/B2 THRUST RATING

Not Applicable

737-700 Airplanes. Refer to Paragraph 1.A.1., Airplanes for the listof affected airplanes.71-1625 SB 00Reason for this StatusAUTO ASSIGNED





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-71A1208 SB 02 MANDATORY A/C *AD* POWER PLANT GEN. - NACELLE HW & FUEL LINE INTERFERENCE Not Applicable by Serial Number

1992-24-05 (ACTIVE)737-71A1208 (REF)737-71A1208 R1 (REF)737-71A1208 R2 (ACTIVE)SBB 737-71A1208 (MAINT TASK)

ADSBSBSBTA

737-71A1287 SB NOTE

RECOMMENDED A/C POWER PLANT-ENGINE COWLING Closed 01.Oct.1992

737-71A1287 SB 00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

01.Oct.1992PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


737-74-1008 SB NOTE

OPTIONAL A/C PROV INST/ALTERNATE DISPATCH WITH RIGHT SIDE ENGINE IGNITION Not Applicable by Serial Number

737-74-1008-R0MC7400MK3008 MASTERCHANGE

SB

DOCR

737-74-1012 SB NOTE

OPTIONAL A/C PROV INST/ALTERNATE DISPATCH WITH RIGHT SIDE ENGINE IGNITION Not Applicable by Serial Number

737-74-1012-R0MC7400MK3008 MASTERCHANGE

SB

DOCR





24.Oct.2014/411


TEOPTIONAL A/C HIGH PRESS TURBINE CLEARANCE CONTROL TIMER RETROFIT-CFM56-3B Rejected by Operator


SBPRR

737-75-1012 SB NOTE

OPTIONAL A/C AIR- GENERAL - NINTH STAGE BLEED DUCT BAND CLAMP REPLACEMENT Rejected by Operator


SBPRR

737-76-1019 SB NOTE

RECOMMENDED A/C NUMBER TWO ENGINE THROTTLE CABLE CLEARANCE HOLE MODIFICATION Rejected by Operator


SBPRR

737-76-1023 SB 00 RECOMMENDED A/C ENGINE CONTROL SYSTEM - REPLACEMENT OF ENGINE THROTTLE CONTROLCABLES

Not Applicable

737-76-1023/SB Rev.00 ENGINE CONTROL SYSTEM - REPLACEMENT OF ENGINE THROTTLE CONTROLCABLES

Not Applicable

> 737-76-1023/SB* Rev.NOTE *AD* ENG.CONT.SYSTEM-REPL. OF ENG. THROTTLE. CTRL. CABLES Closed 28.Feb.1992Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Feb.1992 PerfRev.:'NOTE' / Reason: MALEV DOC.Reason for this StatusMALEV DOC.





24.Oct.2014/411


TEMANDATORY A/C *AD* ENG.CONT.SYSTEM-REPL. OF ENG. THROTTLE. CTRL. CABLES Closed 28.Feb.1992

1991-21-13 (ACTIVE)737-76-1023 (ACTIVE)PRODUCTION PRR 34969SBB 737-76-1023 (MOD TASK)

ADSBPRRTA

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Feb.1992 PerfRev.:'NOTE' / Reason: MALEV DOC.Reason for this StatusMALEV DOC.

737-77-1011 SB NOTE

OPTIONAL A/C AIRBORNE VIBRATION MONITORING (AVM) SYSTEM MOD. Ex Factory

737-77-1011-RO (ACTIVE)737-77-1070-R0 (REF)737-77-1070-R1 (REF)PRODUCTION LINE PRR 33887

SBSBSBPRR

Reason for this StatusPRODUCTION LINE PRR 33887

737-77-1024 SB NOTE

RECOMMENDED A/C ENGINE IDLE SPEED INDICATION RETROFIT INSTALLATION Not Applicable by Serial Number

737-SL-22-24 (REF)MC7710MK3013 PRR34633-01RSBB 737-77-1024-R1 (ACTIVE)

SLDOCRSB

737-77-1027 SB NOTE

RECOMMENDED A/C ENG INSTRUMENT SYSTEM DISPLAYS REPL FOR EXTENDED TWIN ENG OP Rejected by Operator

PRODUCTION PRR34769SBB 737-77-1027-R0 (ACTIVE)

PRRSB





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-77-1031 SB 00 MANDATORY A/C *AD* MOD FOR INCREASED CAPABILITY IN HAIL, RAIN AND SLEET Closed 03.Jan.1994

1993-05-05 (ACTIVE)PRODUCTION PRR34633-10SBB 737-77-1031-R1 (ACTIVE)

ADPRRSB


03.Jan.1994PerfRev.:'NOTE' / Reason: SUNEXPRESSEO: 737-77-1031

Reason for this StatusSUNEXPRESS EO: 737-77-1031

737-77-1055 SB 00 OPTIONAL A/C AIRBORNE VIBRATION MONITORING (AVM) SYSTEM REPL. Rejected by Operator737-77-1055-R0 (ACTIVE)PRODUCTION PRR38380-3

SBPRR

737-77-1066 SB NOTE

OPTIONAL A/C AIRBORNE VIBRATION MONITORING (AVM) SYSTEM REPL. Rejected by Operator

37-SL-77-015-D (REF)737-77-10660-R0 (ACTIVE)PRR35441-R

SLSBPRR

737-77-1069 SB 02 OPTIONAL COMP AVM SYSTEM - REPLACE CONDITIONER UNIT FOR CFM56-7B ENGINES Not Applicable by Line Number737-77-1069737-SL-77-018PRODUCTION PRR38698

SBSLPRR

02LAST

Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-77-1070 SB 01 OPTIONAL A/C AIRBORNE VIBRATION MONITORING (AVM) SYSTEM REPL. On Attrition

The service bulletin 737-77-1011, original issue must be done beforeor at the same time as this service bulletin for airplanes withAirborne Vibration Monitor (AVM) Signal Conditioner Unit (SCU) PartNumber S332T304-16 originally installed.737-77-1011 SB NOTEReason for this StatusAUTO ASSIGNED

737-77A1026 SB 04 MANDATORY A/C *AD* ENGINE INDICATING - POWER - WIRING MODIFICATION Not Applicable by Serial NumberThis document is applicable to LN# 1001-1780, the following LN# areNot Applicable due to PRR 34633-8.1989-25-02737-77A1026-R0 (REF)737-77A1026-R1 (REF)737-77A1026-R2 (REF)737-77A1026-R3 (REF)737-77A1026-R4 (ACTIVE)PRODUCTION PRR34633-8

ADSBSBSBSBSBPRR

00

737-78-1048 SB NOTE

MANDATORY A/C *AD* PREVENT THRUST REVERSER TRANSLATING SLEEVE SEPARATION Ex Factory

1991-25-06737-78-1048-R8EASA 2004-7858 (REF)PRODUCTION LINE PRR34553

ADSBADPRR






24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-78-1053 SB 06 MANDATORY A/C *AD* TRUST REVERSER SYNC LOCK INSTALLATION - CFM56 ENGINES Repetitive

This document is applicable to LN# 1001-2401, the following LN# areNot Applicable due to PRR 35105.1994-21-05 (SUPERSEDED)1994-21-05-R1 (ACTIVE)737-78-1053-R0 (REF)737-78-1053-R1 (REF)737-78-1053-R2 (REF)737-78-1053-R3 (REF)737-78-1053-R4 (REF)737-78-1053-R5 (REF)737-78-1053-R6 (ACTIVE)PRODUCTION PRR35105

ADADSBSBSBSBSBSBSBPRR


12.Apr.1997PerfRev.:'NOTE' / Reason: DELIVERYDOC.


737-78-1057 SB 00 RECOMMENDED A/C THRUST REVERSER CASCADE SEGMENT INSPECTION/REPLACEMENT Rejected by Operator737-78-1057-R0 (ACTIVE)737-SL-78-27 (REF)PRODUCTION LINE PRR35005-56R

SBSLPRR





24.Oct.2014/411


TEMANDATORY A/C THRUST REVERSER SYNC LOCK WIRING CHANGES - CFM56 ENGINES Not Applicable by Serial Number

1994-21-05 R1737-78-1058737-78-1058 R1737-78-1058 R2737-78-1058 R3737-78-1058 R4

ADSBSBSBSBSB

737-78-1060 SB 00 OPTIONAL A/C THRUST REVERSER - THRUST REVERSER CASCADE SUPPORT RING MODIFICATION Rejected by OperatorNo compliance time is given.20-20-0220-41-0220-43-0378-31-0178-31-02

DOCRDOCRDOCRAMMAMM

LASTLASTLASTLASTLAST


737-78-1064 SB NOTE

OPTIONAL A/C CFM56-3 FAN DUCT COWL AND THRUST REVERSER- INNER WALL CHANGE Rejected by Operator

737-78-1064-R1 (ACTIVE)737-SRP-78-0032 (REF)

SBSRP

737-78-1065 SB NOTE

RECOMMENDED A/C EXHAUST-THRUST REVERSER Rejected by Operator

737-78-1065 SB





24.Oct.2014/411


TERECOMMENDED A/C EXHAUST-THRUST REVERSER Rejected by Operator

737-87-1066 SB

737-78-1081 SB 00 RECOMMENDED A/C J20 JUNCTION BOX - INSP. AND PROTECT. OF THE WIRE BUNDLES Closed 01.Nov.2012 W/O:273621COMPLIANCEBoeing recommends that the change given in this service bulletin bedone within 60 months after the date on this service bulletin

The service bulletin 737-78-1053, Revision 1, 2, 3, 4, and 6 must bedone before or at the same time with this service bulletin.12-31-1120-00-1120-10-1120-10-1220-10-1320-10-1820-50-1220-60-0324-22-0029-15-0032-00-01737-78-105378-31-00

AMMSWPMSWPMSWPMSWPMSWPMSOPMAMMAMMAMMAMMSBAMM

LASTLASTLASTLASTLASTLASTLASTLASTLASTLASTLAST06LAST

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Nov.2012 68139:00/H 40570/C 273621, N/A Was due at: 26.Mar.2013 PerfRev.:'00'





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject Status737-78A1048 SB 08 MANDATORY A/C *AD* PREVENT THRUST REVERSER TRANSLATING SLEEVE SEPARATION Not Applicable by Serial Number

737-78A1048 (REF)737-78A1048 R1 (REF)737-78A1048 R2 (REF)737-78A1048 R3 (REF)737-78A1048 R4 (REF)737-78A1048 R5 (REF)737-78A1048 R6 (REF)737-78A1048 R7 (REF)737-78A1048 R8 (ACTIVE)PRODUCTION LINE PRR34553

SBSBSBSBSBSBSBSBSBPRR 00

737-78A1055 SB 00 MANDATORY A/C *AD* T/R CTRL SYSTEM - MOD. OF TEE & RESTRICT. FITTING ON TR Closed 26.Oct.19931992-24-04 (ACTIVE)737-78A1055-R0 (REF)737-78A1055-R1 (REF)737-78A1055-R2 (REF)737-78A1055-R3 (ACTIVE)SBB 737-78A1055 (MOD TASK)

ADSBSBSBSBTA

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks26.Oct.1993 PerfRev.:'NOTE' / Reason: MALEVReason for this StatusMALEV

737-78A1056 SB 01 MANDATORY A/C *AD* THRUST REVERSER - APPL. OF A TOPCOAT TO THE T/R FIREWAL Not Applicable by Serial Number1995-09-01 (ACTIVE)737-78A1056-R0 (REF)737-78A1056-R1 (ACTIVE)

ADSBSB





24.Oct.2014/411


TEOPTIONAL A/C ENG STARTING SYSTEM-STARTER PROTECTION CIRCUIT MODIFICATION Rejected by Operator

737-80-1056-R0 (ACTIVE) SB

737-80-1059 SB NOTE

MANDATORY A/C *AD* TO PREVENT UNDETECTED PROLONGED ENG. STARTER OPERATION Rejected by Operator

1983-01-05-R2 (ACTIVE)737-80-1059-R0 (ACTIVE)PRODUCTION MC7700MK3005

ADSBPRR


737-80-1060 SB NOTE

OPTIONAL A/C ENG STARTING SYSTEM - N2 TACH RELAY - SUPPRESSION DIODE INST Rejected by Operator

737-80-1060-R0 (ACTIVE) SB

A001-25-92 SB 00 MANDATORY A/C *AD* CAPTAIN & F/O CREW SEATS - INSPECTION/MODIFICATION Closed 12.Dec.19971997-19-03 (ACTIVE)IPECO SB A001-25-74 R2 (REF)IPECO SB A001-25-92 R1 (REF)SB A001-25-92 (MOD-TASK)

ADSBSBTA


12.Dec.1997PerfRev.:'NOTE' / Reason: MALEVENGINEERING DOC.

Reason for this StatusMALEV ENGINEERING DOC.





24.Oct.2014/411

Document-Number Type Rev Compliance A|C Subject StatusB221001-52-03 SB 03 MANDATORY COMP *AD* COCKPIT DOOR ASSY. PRESSURE RELIEF LATCH REPLACEMENT Not Applicable

2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12SUB4 (ACTIVE)B221001-52-03-R0 (REF)B221001-52-03-R3 (ACTIVE)SB B221001-52-03 (MOD TASK)

ADADADSBSBTA

This Document SUPERSEDES B221001-52-03/SB Rev.02Affected Rotables (Part No/Serial No/Position) Status

B221200BM631 / 810571 Pos=#1 (KKM)Not Applicable / Reason: N/AACCORDING TO SB

B221001-52-03 SB 02 MANDATORY COMP *AD* COCKPIT DOOR ASSY. PRESSURE RELIEF LATCH REPLACEMENT Superseded (Superseded)2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12SUB4 (ACTIVE)B221001-52-03-R0 (REF)B221001-52-03-R3 (ACTIVE)SB B221001-52-03 (MOD TASK)

ADADADSBSBTA

This Document has been SUPERSEDED BY B221001-52-03/SB Rev.03Affected Rotables (Part No/Serial No/Position) StatusB221200BM631 / 810571 Pos=#1 (KKM) Superseded





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Document-Number Type Rev Compliance A|C Subject StatusB221200-52-01 SB 01 MANDATORY COMP *AD* COCKPIT DOOR ASSY. DEADBOLT ARMOUR PLATE INSTALLATION Not Applicable

2005-12-05 (SUPERSEDED)2007-10-12SUB4 (ACTIVE)B221200-52-01-R0 (REF)B221200-52-01-R1 (ACTIVE)SB B221200-52-01 (MOD TASK)

ADADSBSBTA


B221200BM631 / 810571 Pos=#1 (KKM)Not Applicable / Reason: IMPLEMENTEDBEFORE INSTALL.





24.Oct.2014/411

Modification Control Report 13237 24. · PDF file737-11-1040 sb 00 recommended a/c alternate...

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Transcript of Modification Control Report 13237 24. · PDF file737-11-1040 sb 00 recommended a/c alternate...