TECHNICAL DATA Aircraft Type : Saab 340 Effective Date : · PDF file ·...

Aircraft Type : Saab 340 Effective Date : 9/12/2007Serial # : 340A-057Date of Manufacture : 1986Aircraft Total Time : 37240.4Aircraft Total Cycles : 41340Hours Since Major Inspection/ Overhaul :

Left Hand Engine :

Type : G.E. CT7-5A2 Serial # : GE-E-367499

TSN : -23401.8 TCSN : -17280.0 AD2002-01-03 due at 28849TSO : -34797.3 TCSO : N/A ECMP

Time Since Hot Section Inspection : N/A ECMPPGB SN: UDAG0074Right Hand Engine :

Type : G.E. CT7-5A2 Serial # : GE-E-367275

TSN : -13800.6 TCSN : -14557.0TSO : -33078.3 TCSO : N/A ECMP

Time Since Hot Section Inspection : N/A ECMPPGB SN: UDAG0349

Optrs / Mfrs

Limits

Optrs / Mfrs

TECHNICAL DATA

ENGINE DATA

Limits

Aircraft Registration # : C-GQXF

LEFT ENGINE : GE-E-367499

DESCRIPTIONPART

NUMBER

SERIAL

NUMBER

LIFE LIMIT

(Cycles)LAST

DONE

NEXT

DUEREMAINING

Stage 1 Blade-Disk 6044T38G07 GLHK5FMJ 25200 38129 63329 21989Spacer Ring (Stages 1, 2) 5051T47P02 PAMRG03Y 34000 38129 72129 30789Stage 2 Blade-Disk 6061T05P02 GLHG8436 34100 27280 61380 20040Stages 3 and 4 Blade-Disk 6044T41P08 GLHK5EV1 24200 33679 57876 16536Spacer Ring (Stages 2, 3) 5051T48P02 PAMS2468 34000 38129 72129 30789Stage 5 Blade-Disk 6044T42P10 GLHJ5897 40000 33435 73435 32095Centrifugal Impeller 6071T67P01 GLHK5FCT 17000 38129 55129 13789Compressor Tie Rod 5043T04P03 GATEN541 33000 25784 58784 17444Rear Shaft 5086T82P01 GATCTF9P 32600 38129 70729 29389

Stage 1 Turbine Fwd Cooling Plate 6064T08P01 GFFR81AA 15000 38129 53129 11789Stage 1 Turbine Aft Cooling Plate 6064T09P01 GFFR81P4 15000 38129 53129 11789Stage 2 Turbine Fwd Cooling Plate 4106T80P01 GFFR5652 13200 38129 51329 9989Stage 2 Turbine Aft Cooling Plate 6064T07P02 GFFR3457 12000 38129 50129 8789Stage 1 Turbine Disk 6064T06P01 GATCV8W0 15000 38129 53129 11789Stage 2 Turbine Disk 6064T12P01 GATCV34T 15000 38129 53129 11789GG Turbine Shaft 6068T44P01 FIAA4163 28200 27280 55480 14140

Power Turbine Drive Shaft Assy 5121T01G01 GAT0435B 30000 26663 56663 15323Stage 3 Turbine Disk 6055T98P01 GATEP351 22800 26861 49661 8321Stage 4 Turbine Disk 6038T34P05 GATBWR72 24000 38129 62129 20789Output Shaft 6032T89P04 ALFP4173 NA N/A N/A #VALUE!

LIFE LIMITED PARTS REPORT

COMPRESSOR ROTOR PARTS

GAS GENERATOR TURBINE ROTOR

POWER TURBINE ROTOR AND POWER TURBINE ROTOR DRIVE SHAFT

Aircraft Registration # : C-GQXF

RIGHT ENGINE : GE-E-367275

DESCRIPTIONPART

NUMBER

SERIAL

NUMBER

LIFE LIMIT

(Cycles)LAST

DONE

NEXT

DUEREMAINING

Stage 1 Blade-Disk 6044T38G07 GLHD2274 25200 48405 7065Spacer Ring (Stages 1, 2) 5051T47P02 PAMH6055 34000 57205 15865Stage 2 Blade-Disk 6061T05P02 GLHJ5145 34100 68095 26755Stages 3 and 4 Blade-Disk 6044T41P08 GLHJ4872 24200 58195 16855Spacer Ring (Stages 2, 3) 5051T48P02 GATCM239 34000 50725 9385Stage 5 Blade-Disk 6044T42P10 GLHJ4088 40000 73995 32655Centrifugal Impeller 6071T67P01 GLHJ0367 17000 50995 9655Compressor Tie Rod 5043T04P03 GATBW918 33000 49725 8385Rear Shaft 5086T82P02 FIAAEC3E 32600 66595 25255

Stage 1 Turbine Fwd Cooling Plate 6064T08P01 GFFN2557 15000 50731 9391Stage 1 Turbine Aft Cooling Plate 6064T09P01 GFFR6225 15000 53635 12295Stage 2 Turbine Fwd Cooling Plate 4106T80P01 GFFR5644 13200 51835 10495Stage 2 Turbine Aft Cooling Plate 6064T07P02 GFFP0963 12000 45750 4410Stage 1 Turbine Disk 6064T06P01 GATCTMRG 15000 53635 12295Stage 2 Turbine Disk 6064T12P01 GAT7365R 15000 50731 9391GG Turbine Shaft 6068T44P11 FIAAEC3E 28200 61297 19957

Power Turbine Drive Shaft Assy 5121T01G01 GATCTEEH 30000 68718 27378Stage 3 Turbine Disk 6055T98P01 GATBFW88 22800 61518 20178Stage 4 Turbine Disk 6038T34P05 PUN12692 24000 62718 21378Output Shaft 6032T89P04 N/A NA N/A #VALUE!

LIFE LIMITED PARTS REPORT

COMPRESSOR ROTOR PARTS

GAS GENERATOR TURBINE ROTOR

POWER TURBINE ROTOR AND POWER TURBINE ROTOR DRIVE SHAFT

Manufacter : Dowty/Rotol Model : R.389/4-123-F/25

Left Serial # : DRG/1513/86

TSN : 33966.2 TSO :Overhaul Date : 10/06/2000 Limit :

Serial Number Operator's Limit Mfg's Limit Last done Next due Remaining

Hub CW1298 7500 HR 7500 Hours 29587.4 37457 216.6 EXTDate of Overhaul : 5 Y 5 Years 10/06/2000 10/06/2005

Blade #1 SF340-132/183 7500 HR 7500 Hours 29587.4 37457 216.6 EXTDate of Overhaul : 5 Y 5 Years 10/06/2000 10/06/2005




Right Serial # : DRG/8689/86

TSN : 28688.5 TSO :Overhaul Date : 08/01/2004 Limit :

Serial Number Operator's Limit Mfg's Limit Last done Next due Remaining

Hub AW785 7500 HR 7500 Hours 31021.5 38521.5 1281.1Date of Overhaul : 5 Y 5 Years 08/01/2004 10/11/2006

Blade #1 SF340-132/463 7500 HR 7500 Hours 31021.5 38521.5 1281.1Date of Overhaul : 5 Y 5 Years 08/01/2004 10/11/2006




PROPELLERS

7658.47500 Hours5 Years

6218.97500 Hours5 Years

Aircraft Total Time : 0Aircraft Total Cycles : 0Effective Date : 9/12/2007

Aircraft Type : Saab 340A Registration : C-GQXF Serial # : 340A.057

All "due" times are referenced to aircraft total time and total cycles.

Item S/N Position Life Last Done Next Due Remaining

Chapter 5 Time Limits/Maintenance Checks

LC1 Check 057 N/A 48 FH na na LC1LC2 Check 057 N/A 7 days na na LC2AB1-AB10 (400-800FHs) 057 N/A 400 FH 36926.9 37326.9 86.51200 FH Inspections 057 N/A 1200 FH 36161.2 37361.2 120.84000 FH Inspections 057 N/A 4000 FH 33158.7 37158.7 -81.75000 FH Inspections 057 N/A 5000 FH 32535.4 37535.4 2958000 FH Inspections 057 N/A 8000 FH 36213.6 44213.6 6973.212 Month Inspections 057 N/A 1 Y 05/2004 05/200524 Month Inspections 057 N/A 2 Y 05/2003 07/20053000FL 057 N/A 3000FL 38853 41853 5136000FL 057 N/A 6000FL 35938 41938 59812000FL 057 N/A 12000FL 29663 41963 6232Y Zonals 057 N/A 2 Y 06/2004 06/20064Y Zonals 057 N/A 4 Y 06/2004 06/20084Y SSI`s 057 N/A 4 Y 06/2004 06/2008Weight & Balance 057 N/A 5 Y 05/2003 05/2008

Chapter 21 Air Conditioning

Brush and bearing replacement on fan motor.212101

057 N/A 900 FH N/A N/A #VALUE!

Vacuum clean filter, p/n471749212102

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Filter replacement, smoking212103


AIRFRAME AIRWORTHINESS LIMITATIONS

Filter replacement, non-smoking, p/n 471749212104


Filter replacement, p/n QB 0441. Non-smoking212106

057 N/A 4000 FH 33158.7 37158.7 -81.7

Brush and bearing replacement on fan motor.212201


Vacuum clean filter, p/n471750212202

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Filter replacement212203


Filter replacement, p/n471750212204

057 N/A 1800 FH 36244.5 38044.5 804.1

Perform operational check of cabin air shut-off valve.212206


Filter replacement. P/n QB0443212207

057 N/A 2400 FH pn 471750 na #VALUE!

Brush and bearing replacement on fan motor.PRE MOD 1125212301

057 N/A 1500 FH NA NA #VALUE!

Brush and bearing replacement on fan motor.212302 Post MOD 1125

78 N/A 2500 FH 35650.6 37815.2 574.8

Vacuum clean filter and inlet screen. P/n 471754212303

057 N/A 800 FH 36926.9 37626.9 386.5AB Even

Filter replacement - smoking212304


Filter replacement. P/n 471754212305

057 N/A 1800 FH 36244.5 38044.5 804.1

Filter replacement. P/n QB 0442212307

057 N/A 2400 FH pn471754 NA #VALUE!

213002 inspect tubing for general condition 057 4000 FH 33158.7 37158.7 -81.7

Inspect and clean electropneumatic outflow valve (primary) andpneumatic outflow valve (secondary) including poppet valveseat.213003

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of dump system.213004

057 N/A 4000 FH 33158.7 37158.7 -81.7

Drainage of water traps.213005

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of manual pressurization control system.213006

057 N/A 8000 FH 36213.6 44213.6 6973.2

Replace electropneumatic outflow valve (primary) filter.213007

057 N/A 6000 FH 34653.8 40653.8 3413.4

Drain and refill ACM oil.215002

057 N/A 400 FH 36926.9 37326.9 86.5AB

Check for leakage, block and spray nozzle filter contamination.215004

057 N/A 4000 FH 33158.7 37158.7 -81.7

920133 RH 6000 FH 31936.9 37936.9 696.5870516 LH 6000 FH 33312.6 39312.6 2072.2

216001 bench ck o/temp sw 057 N/A 4000 FH 33158.7 37158.7 -81.7Bench check of supply duct overtemperature switch.216004

057 N/A 4000 FH 33158.7 37158.7 -81.7

215181 Overhaul of ACM

Operational check of air ventilation tailcone shutoff valve.217001

057 N/A 4000 FH 33158.7 37158.7 -81.7

Chapter 22 Auto Flight

Functional test of the servo slip clutches.221001

057 N/A 4000 FH 33158.7 37158.7 -81.7

Visual check of servo and servo mount mechanical installationincluding capstan cables for condition and security and checkfor proper spool off angle.221002

057 N/A 4000 FH 33158.7 37158.7 -81.7

Functional check of capstan cable tension.221004

057 N/A 4000 FH 33158.7 37158.7 -81.7

Chapter 23 Communications

Inspect HF antenna installation for cracks and generalcondition.231201

N/A N/A 800 FH N/A N/A #VALUE!

Check Emergency Call function.233001

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of REU emergency function.235001

057 N/A 4000 FH 33158.7 37158.7 -81.7

Overhaul CVR according to vendor Overhaul manual.237001

57946 N/A 9000 FH 32962.7 41962.7 4722.3

237001QS CVR intel 057 N/A 1Y 05/2004 05/2005

Test for four channel operations including audio levels andsound quality.237002

52254 N/A 4000 FH 33158.7 37158.7 -81.7

Chapter 24 Electrical Power

Check generator for damage, loose connections, wiringinsulation wear, and re-torque mounting clamp.242101

057 N/A 800 FH 36926.9 37626.9 386.5

AB EVEN

A.C. Generator overhaul according to vendor overhaul manual.242102

1290 Left 2000 FH 35542.4 37542.4 302

A.C. Generator overhaul according to vendor overhaul manual.242102

148 Right 2000 FH 36991.8 38991.8 1751.4

Operational check of 26VAC from STBY inverter.242401

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of inverters 1 and 2.242402

057 N/A 4000 FH 33158.7 37158.7 -81.7

Brush replacement; check Generator for damage, looseconnections, wiring insulation wear.243101

057 N/A 800 FH 36926.9 37626.9 386.5

AB EVEN

6756 Left 1600 FH 37093.6 38693.6 1453.2991117 Right 1600 FH 36599.1 38199.1 958.7

3442 Left 1200 FH 33164.3 na #VALUE!3449 Right 1200 FH 33164.3 na #VALUE!

A02051 Left 300 FH 37180.1 37480.1 239.7J02129 Right 300 FH 37180.1 37480.1 239.7

A02051 Left 12 M 10/2004 10/2005J02129 Right 12 M 10/2004 10/2005

Functional check of BAT HOT/NO BAT start alert.243404

057 N/A 4000 FH 33158.7 37158.7 -81.7

243501 Emer batt volt chk 057 N/A 1200 FH 36161.2 37361.1 120.7

Emergency Battery Discharge Check243502

057 N/A 12 M 05/2004 05/2005

D.C. Generator overhaul in accordance with vendor overhaulmanual.

D.C. Generator overhaul in accordance with vendor overhaulmanual.243104

Battery Service243401

DC Battery Overhaul243402

Chapter 25 Equipment

Visual inspection and ops.I check of Pilot/Co-pilot and observerseat.251101

057 N/A 4000 FH 34045.4 38045.4 805

057 N/A 800 FH N/A N/A #VALUE!N/A 4000 FH 33158.7 37158.7 -81.7

251110QS Emer equip chk 057 N/A 400 FH 36926.9 37326.9 86.5 AB

251111QS Seat breakover chk 057 N/A 400 FH 36926.9 37326.9 86.5 AB

Visual inspection and operational check of flight attendant seat.252101

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of restraint system.252202

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of seat folding mechanism and seat foldingstops.252204

057 N/A 4000 FH 33158.7 37158.7 -81.7

Inspect galley paper and linen waste receptacle enclosureaccess and disposal doors for proper operation, fit, sealing andlatching for the containment of possible trash fires.253001

057 N/A 6000 FH 35547.4 41547.4 4307

Inspect lavatory paper and linen waste receptacle enclosureaccess and disposal doors for proper operation, fit, sealing andlatching for the containment of possible trash fires.254001

057 N/A 6000 FH 33158.7 39158.7 1918.3

ELT RecertificationSTD 625 254002QS

057 N/A 12 M 05/2004 05/2005

Check net webbing, fittings, and all wall and floor attachments.255001

057 N/A 1200 FH 36161.2 37361.1 120.7

Detailed inspection of the Pilot/Co-pilot seat back structure.POST-MOD SB 25-223

Check liner, mounts, panels and channels for general conditionand security.255002

057 N/A 1200 FH 36161.2 37361.1 120.7

ELT Battery Ops Check256001

057 N/A 1 Y 05/2004 5/2005

Replace ELT batteryType : MARCO ELT 10256002

C10688 N/A 2 Y 05/2003 05/2005

Functional test of ULB & cleaning of water switch256003

057 CVR 1 Y 05/2004 05/2005

Battery date of underwater locater beacon (ULD)Type : DK120256005

28575 CVR 6 Y 10/2000 10/2006

DV0843 FDR 6 Y 07/2001 07/2007Chapter 26 Fire Protection

057 L/H 6000 FH 36563.2 42563.2 5322.8R/H 36563.2 42563.2 5322.8

057 Avionics 800 FH 36926.9 37626.9 386.5 AB EVENLav. 800 FH 36926.9 37626.9 386.5 AB EVEN

Cargo 800 FH na na #VALUE!

057 Avionics 9000 FH na na #VALUE!Lav. 9000 FH na na #VALUE!

620 Cargo 9000 FH 34213.7 43213.7 5973.3

Check container pressure gauge reading vs. temperature262101

057 N/A 400 FH 36926.9 37326.9 86.5

AB

97937EJ Left 4000 FH 33158.7 37158.7 -81.771656EK Right 4000 FH 33158.7 37158.7 -81.7

262103 vis insp extinghiser Left 4000 FH 33158.7 37158.7 -81.7manifold ans ass components Right 4000 FH 33158.7 37158.7 -81.7

Spot detectors bench check261201

Visual inspection and cleaning - Detector photo optics andconnectors (Avionics, lavatory and cargo smokedetectors).fenwall

Visual inspection and cleaning - Detector photo optics andconnectors (Avionics, lavatory and cargo smokedetectors).cerberus

Engine Fire ExtinguisherWeight check 262102

Functional check crossover check valve.262104

057 N/A 4000 FH 33158.7 37158.7 -81.7

Functional check extinguishing circuit excluding cartridges.262105

057 N/A 4000 FH 33158.7 37158.7 -81.7

na LH Fwd 5 Y NA NAna LH Aft 5 Y NA NAna RH Fwd 5 Y NA NAna RH Aft 5 Y NA NA

71656EK Left 5 Y 05/2004 05/2009371EL Right 5 Y 02/13/03 02/13/08

00463 LH Fwd 10 Y 03/2000 10/201000319 LH Aft 10 Y 10/2000 10/20100298 RH Fwd 10 Y 05/98 05/20080002 RH Aft 10 Y 03/98 03/2008

Electrical circuit functional check262201

057 N/A 5000 FH 33158.7 38158.7 918.3

Replace cartridge262202

072WK Cargo 7 Y 11/98 11/2005

Container weight check262203

072WK Cargo 3 Y 10/2002 10/2005

Fire Bottle Hydrostatic262204

1198101 Cargo 5 Y 03/2001 03/2006

Visual check gauge, Trash bin fire extinguisher.262205

057 Trash 400 FH 36926.9 37326.9 86.5AB

Fire extinguisher life limit.262206

8552 Trash 10 Y 09/1996 09/2006

Weight check of lavatory fire extinguisher. P/N A800100-2262207

Trash 1 Y NA by PN NA

Change extinguisher cartridges per service life limit.262106

Engine Fire Ext. (Hydrostat)262107

Replace and discard extinguisher cartridges per service lifelimits.-01262108

Visual check gauge or indicator disc of cabin and cockpitportable fire extinguishers.262301

400 FH 36926.9 37326.9 86.5

AB

V-498006 Cabin 1 Y 05/2004 05/2005V-451440 Cockpit 05/2004 05/2005V-451423 Galley 05/2004 05/2005

V-498006 CABIN 12 Y 12/1995 12/2007V-451440 COCKPIT 03/1996 03/2008

V-451423 CABIN 03/1996 03/2008V-498006 Cabin 10 Y N/A N/AV-451440 CockpitV-451423 Galley

Chapter 27 Flight Controls

Inspect control system in wing for security and generalcondition.271101

057 N/A 4000 FH 33158.7 37158.7 -81.7

Inspect cable tension regulators, aileron hinges and blots forsecurity and general condition.271102

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of cable tension regulators.271103

057 N/A 4000 FH 33158.7 37158.7 -81.7

Check cable tension.271104

057 N/A 4000 FH 33158.7 37158.7 -81.7

Lubrication of bearings of aileron hinges.271107

057 N/A 800 FH 36431.7 37231.7 -8.7AB ODD

Control cable inspection and lubrication271109

057 N/A 5000 FH 32535.4 37535.4 295

Lubrication of aileron and flap greasable bell cranks and partsof the aileron centering mechanism. If installed. (POST-MOD2509, SB 27-069).271112

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Port. Fire Extinguisher weinght check262302

Hydrostatic check of cabin and cockpit portable fireextinguishers.

Port. Fire Extinguisher Life Limit 10 Y from D.O.M.262304

Operational check of the individual switches of standby trimswitch.271202

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of standby trim from alternate power source(RH BAT BUS)271203

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of standby trim from normal power source(LH BAT BUS)271204

057 N/A 4000 FH 33158.7 37158.7 -81.7

Check backlash of LH and RH aileron trim tab mechanism271206

057 N/A 4000 FH 33158.7 37158.7 -81.7

Aileron trim inspection271207

057 N/A 5000 FH 32535.4 37535.4 295

Aileron trim tab travel check271208

057 N/A 5000 FH 32535.4 37535.4 295

Actuator movement check271209

057 N/A 5000 FH 32535.4 37535.4 295

Lubricate aileron trim tab hinges fitted with grease nipples.271210

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Check standby trim indication from alternate power source (RHBAT BUS)271301

057 N/A 4000 FH 33158.7 37158.7 -81.7

Aileron spring unit function check271401

057 N/A 8000 FH 36213.6 44213.6 6973.2

Functional check of disconnect unit.271402

057 N/A 4000 FH 33158.7 37158.7 -81.7

272101 insp control system and cable tension device forsecurity and general condition

057 N/A 5000 FH 32535.4 37535.4 295


057 N/A 4000 FH 33158.7 37158.7 -81.7

272103 insp cable sliding surfaces for wear and security 057 N/A 5000 FH 32535.4 37535.4 295

Visual inspection of spring tab mechanism including stops forgeneral condition and security272107

057 N/A 4000 FH 33158.7 37158.7 -81.7

Lubricate rudder hinges fitted with greas nipples272108

057 N/A 4000 FH 33158.7 37158.7 -81.7

272110 insp of rudder hinges and bolts for security and generalcondition

057 N/A 4000 FH 33158.7 37158.7 -81.7

Rudder control cables, inspect and lube272112

057 N/A 5000 FH 32535.4 37535.4 295

Operational check of the individual switches of standby trimswitch.272201

057 N/A 4000 FH 33158.7 37158.7 -81.7

Rudder trim travel check272203

057 N/A 5000 FH 32535.4 37535.4 295

Visually inspect trim tab and associated linkage for generalcondition and security.272204

057 N/A 4000 FH 33158.7 37158.7 -81.7

Visually inspect rudder tab damper for general condition andsecurity.272205

057 N/A 4000 FH 33158.7 37158.7 -81.7

Perform functional check of rudder spring tab mechanism anddamper.272206

057 N/A 4000 FH 33158.7 37158.7 -81.7

Check fill level indicator on damper.272207

057 N/A 4000 FH 33158.7 37158.7 -81.7

Lubricate rudder trim tab hinges fitted with grease nipples.272208

057 N/A 800 FH 36926.9 37626.9 386.5

AB EVEN

Rudder limiter self test272401

057 N/A 400 FH 36926.9 37326.9 86.5AB

272402 insp operating actuators and limiter mech linkage forgeneral security and condition

057 N/A 4000 FH 33158.7 37158.7 -81.7

273101 insp elevator bearings and fittings for security andgeneral cond.

057 N/A 4000 FH 33158.7 37158.7 -81.7

273102 inspect cable tension regulators for security andgeneral condition

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of cable tension regulators.273103

057 N/A 4000 FH 33158.7 37158.7 -81.7


057 N/A 4000 FH 33158.7 37158.7 -81.7

Lubricate elevator bearings273107

057 N/A 4000 FH 33158.7 37158.7 -81.7

Elevator control cables: inspect and lube273110

057 N/A 5000 FH 32535.4 37535.4 295

Operational check of the individual normal pitch trim switches(both pilots).273201

057 N/A 400 FH 36926.9 37326.9 86.5

AB

Check backlash of LH and RH elevator trim tab mechanism273204

057 N/A 4000 FH 33158.7 37158.7 -81.7

Elevator trim inspection273205

057 N/A 5000 FH 32535.4 37535.4 295

Check time for LH and RH tab travel from zero to fullydeflected position in both directions. Functional check of LHand RH trim actuator limit switches. Check simultaneously forfreedom of movement and abnormal sound.273206

057 N/A 4000 FH 33158.7 37158.7 -81.7

Elevator trim actuator check273207

057 N/A 5000 FH 32535.4 37535.4 295

Standby pitch trim switches ops check273208

057 N/A 400 FH 36926.9 37326.9 86.5AB

Lubricate elevator trim tab hinges fitted with grease nipples.273209

057 N/A 800 FH 36926.9 37626.9 386.5

AB EVEN

Operational check of the trim syncFHonization.273210

057 N/A 400 FH 36926.9 37326.9 86.5AB

273401 insp. Of disconnect unit for security and general cond. 057 N/A 5000 FH 32535.4 37535.4 295

Disconnect unit function check273404

057 N/A 8000 FH 36213.6 44213.6 6973.2

Functional check of override function of disconnect unit.273405

057 N/A 4000 FH 33158.7 37158.7 -81.7

Visually inspect Angle of Attack (AOA) vanes for condition andcheck for freedom of movement.273501

057 N/A 25 FH LC1 LC1 #VALUE!

Pusher disarm ops check273503


AOA transmitter ops check273504


Operational check of failure signals from stall warningcomputers to CWP.273505

057 N/A 400 FH 36926.9 37326.9 86.5

AB

Functional check of stall warning and ident sustem with AOArelated to different flap positions (overriden WOW switches).273506

057 N/A 4000 FH 33158.7 37158.7 -81.7

Servo actuator, cables, visual inspection273507

057 N/A 5000 FH 32535.4 37535.4 295

Operational check of pusher disarm. Non US operators only.273508


Flap control test275101

057 N/A 400 FH 36926.9 37326.9 86.5AB

Replace flap actuator p/n TP1000-9275109

057 N/A 10000 FL N/A N/A #VALUE!

174 N/A 58162 FL LH 21532 65224 23884099 RH 23209 65460 24120

Replace flap actuator p/n 70837 & 70837-1275111

N/A N/A 39600 FL N/A N/A #VALUE!

Flap interconnect inspection275201

057 N/A 4000 FH 33158.7 37158.7 -81.7

277101 insp. Gust lock installation for security and generalcondition

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operate gust lock and associated controls and check lockmechanism.277102

057 N/A 4000 FH 33158.7 37158.7 -81.7

Rudder gust lock warming, ops check277201

057 N/A 5000 FH 32535.4 37535.4 295

277202 insp. Of parts and rigging included in rudder gust lockassy

057 N/A 4000 FH 33158.7 37158.7 -81.7

Chapter 28 Fuel

281102 fuel sumping 057 na LC1 LC1 LC1

Replace flap actuator p/n TP1000-10275110

Inspect overwing filler caps for condition and ops check281104

057 N/A 4000 FH 33158.7 37158.7 -81.7

Float switch ops. Check284101

057 N/A 6Y/4Y 06/2004 06/2008

Chapter 29 Hydraulics

Main hydraulic system functional check.291002


291001 CK DIFF IND. 057 NA LC1 LC1 LC1Replace pressure and return filter elements and inspect returnfilter element291005

057 N/A 4000 FH 37158.7 37158.7 -81.7

Pump motor brushes inspection (if regular use of prop brake).291007


Pump motor brushes inspection291007

AH93388 N/A 3000 FH 34932.3 37932.3 691.9

AH93388 N/A 3600 FH N/A N/A6000 FH 34932.3 40932.3 3691.9

Main hydraulic system functional check. Non US operatorsonly.291011

0-57 N/A 50 FH LC1 LC1 #VALUE!

Replace the hydraulic reservoir P/N 70841If installed291012

0-57 N/A 63000 FL N/A N/A #VALUE!

Replace the hydraulic reservoir P/N 70841-2If installed291013

0-57 N/A 72000 FL N/A N/A #VALUE!

292001 hydr. Leakage ck 057 na LC2 LC2 LC2Operational check of the system with all tFHee-selector valvepositions.292005

0-57 N/A 4000 FH 33158.7 37158.7 -81.7

292002 ck of fluid level 057 NA LC2 LC2 LC2

Pump motor bearings replace (if regular use of prope brake).Replace bearings

292003 insp. For leakage of hydraulic fluid 057 N/A 800 FH 36431.7 37231.7 -8.7 AB ODD

Visual check of vent and breathing valve for cleanliness andgeneral condition.292006

0-57 N/A 4000 FH 33158.7 37158.7 -81.7

Operational chek of mechanical indicator and check of cockpitindicator response.293101

0-57 N/A 4000 FH 33158.7 37158.7 -81.7

Chapter 30 Deice

Visual inspection of Deicer Boots for general condition andsecurity.301001

057 N/A 400 FH 36926.9 37326.9 86.5

AB

057 N/A 6000 FH 33164.3 39164.3 1923.933164.3 39164.3 1923.9

Over temp circuit ops check301003

057 N/A 8000 FH 36213.6 44213.6 6973.2

301004 ops airfoil de-ice 057 NA AT ENG CHGPerform functional check of distribution valve heater blanketsand check deicer tube drain hole for obstruction.301006

057 N/A 1 Y 05/2004 05/2005

301005 drain stab water trap 057 NA LC2 LC2 LC2R-apply "Icex" (or equivalent) to de-icer boots if icing conditionsare expected during operation of aircraft.301008


301007 visual stab de-icer 057 NA LC2 LC2 LC2

Inspect that Control Unit Display fault indicator lights are out(not illuminated).COX air intake only302003

N/A N/A 800 FH N/A LUCAS N/A #VALUE!

Detailed inspection of wiper blade and arm assembly forcondition and securityAD115304302

057 N/A 4000 FH 33164.3 37164.3 -76.1

306001visual prop boots 057 NA LC2 LC2 LC2

Temp sensors bench check301002

Inspection of Dowty propeller brush blocks, brackets and sliprings for general condition and wear.306002

057 N/A 400 FH 36926.9 37326.9 86.5

AB

Inspection of Hamilton Standard propeller brush blocks,brackets and slip rings for general condition and wear. (340Bonly)306003


Chapter 31 Recording

Overhaul Flight Data Recorder according to vendor CMM.313002

N/A 1 Y OC OC

313002QS FDR head clean 057 na 1Y OC OC

Parameter check buy copy recorder of flight line tester.313003

N/A 1 Y 05/2004 05/2005

313003QS FDR acc test 057 na 1Y 05/2003 05/2004

Visual inspection of aileron potentiometer for security ofinstallation and obvious damage: ditto for security of two-aluminium shear rivets which attach the lever/crank arm to theaileron.313005

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of configuration warning.315101

057 N/A 4000 FH 33158.7 37158.7 -81.7

315102 LAMP TEST 057 NA LC1 LC1 LC1Chapter 32 Landing Gear

057 N/A 400 FH 36926.9 37326.9 86.5 AB057 36926.9 37326.9 86.5 AB

321103-322103 insp LDG trunion attach points for security andgeneral condition

057 N/A 800 FH 36431.7 37231.7 -8.7AB ODD

321104-322104 Insp LDG cylinders, piston, axle fittings andtorque links for security and general condition

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Lube torque link bearings.321102

321105-322105 insp LDG drag brace, links and downlockmechanism attach points for security and general condition

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

322106 insp NWS components attachments 057 N/A 800 FH 36431.7 37231.7 -8.7 AB ODD

057 N/A 2000 FH 36591.4 38591.4 1351057 36591.4 38591.4 1351

Functional check of nose wheel centering at extension of nosewheel strut.322108

057 N/A 4000 FH 33158.7 37158.7 -81.7

Overhaul of NLG Shock Strut321109

LK8802036 NLG 12000 FL 39822 51822 10482

LK8905154 L/H 12000 FL 39643 51643 10303LK8302131 R/H 32344 44344 3004

OH of NLG Drag Brace321109

LK8306042 NLG 12000 FL 39822 51822 10482

LK8504013 L/H 12000 FL 39870 51870 10530LK8902357 R/H 39639 51639 10299

Overhaul of Steering Imput Assembly.322110

LK8503424 N/A 12000 FL 39822 51822 10482

057 L/H 4000 FH 33158.7 37158.7 -81.7R/H 33158.7 37158.7 -81.7NLG 33158.7 37158.7 -81.7

Discard landing gear life limited parts.321116322116

057 N/A

Inspect landing gear doors for security and general condition.321201322201

057 N/A 400 FH 36926.9 37326.9 86.5

AB

323101 insp of retraction actuator bearings 057 N/A 800 FH 36431.7 37231.7 -8.7 AB ODD

Check landing gear shock strut hydraulic fluid quantity andnitrogen pressure.

Overhaul of MLG Shock Strut322109

Overhaul of MLG Drag Brace322109

Inspection of MLG and NLG axle fitting/piston tube interfacesealant for damage and/or deterioration.321114

SEE FOLLOWING

323102 insp. Assistor spring for security and general condition 057 N/A 800 FH 36431.7 37231.7 -8.7AB ODD

323105 insp. Emergency uplock valve, handle and control valve 057 N/A 4000 FH 33158.7 37158.7 -81.7

Functional check of emergency extension of landing gear.323106

057 N/A 5000 FH 32535.4 37535.4 295

323107 vis insp. Of separation bolt and wiring for damage,corrosion and general condition

057 N/A 4000 FH 33158.7 37158.7 -81.7

Continuity check of separation bolt dual bridge wire circuitry323108

057 N/A 5000 FH 33158.7 38158.7 918.3

2908 L/H 10 Y 06/2001 06/20111442 R/H 06/1995 06/2005

LK8606055 L/H 24000 FL 23934 51293 9953LK8808546 R/H 36846 60846 19506LK9104653 NLG 19496 42516 1176

323201 insp. Uplock and release mech. For security andgeneral

057 N/A 800 FH 36926.9 37626.9 386.5AB EVEN

L/H 20000 FL N/A N/A #VALUE!R/H N/A N/A #VALUE!NLG N/A N/A #VALUE!

323301 insp. Downlock mech. Including actuator andassociated installation

057 N/A 800 FH 36926.9 37626.9 386.5AB EVEN

323401 insp. LG door linkages for security and condition 057 N/A 800 FH 36926.9 37626.9 386.5AB EVEN

324101 TIRE PRESSURE 57 NA LC1 LC1 LC1

Inspect MLG brake swivels for leakage324202

057 N/A 400 FH 36926.9 37326.9 86.5AB

Discard separation bolts.NOTE: Interval from date of manufacture.

Overhaul of main and nose landing gear retract actuators.323110

Discard landing gear uplock actuator(s) P/N 67110-1323203

324204 insp. Brake valves for leakage 057 N/A 800 FH 36926.9 37626.9 386.5 AB EVEN

324206 insp. Parking brake valve for leakage 057 N/A 800 FH 36926.9 37626.9 386.5 AB EVEN

Inspect mechanical connection between outbd. and inbd. Brakevalves for cracks.324208

057 N/A 4000 FH 33158.7 37158.7 -81.7

324305 insp anti-skid control valves for leakage 057 N/A 4000 FH 33158.7 37158.7 -81.7

Lubricate all bearings of output linkage system and outerbearing of steering collar. Pre-mod 2192325001

057 N/A 800 FH 36926.9 37626.9 386.5

AB EVEN

325002 insp. Steering collar, collar gear cover torque links andoutput linkage

057 N/A 800 FH 36926.9 37626.9 386.5AB EVEN

Functional check of ground handling lock out switch.325003

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of servo pressurization control.325004

057 N/A 4000 FH 33158.7 37158.7 -81.7

325008 insp NWS control transfer and feedback mechanismfor security and general condition

057 N/A 4000 FH 33158.7 37158.7 -81.7

Functional check of steering brake.325010

057 N/A 4000 FH 33158.7 37158.7 -81.7

Lubricate cavity between strut bearing in steering collar.325012

057 N/A 4000 FH 33158.7 37158.7 -81.7

326102 insp. Downlock position indicator switches 057 N/A 800 FH 36926.9 37626.9 386.5 AB EVEN

GEARS SAFE LIFE LIMITSTOTAL LIFE MLG Strut NLG strut MLG Drag NLG Drag

Brace Brace90000FL AIR83022 AIR83522 AIR84310 AIR84306

AIR83562 AIR8431171162FL AIR83064 AIR84334

AIR84335

68659FL AIR83564 AIR84350AIR83566

Retaining BoltP/N AIR 123816

N/A NLG 54793 FL N/A N/A #VALUE!

Trunion pin PN air 127284, 134492, 127286 N/A NLG 66357 N/A N/A #VALUE!

Trunnion PinP/n AIR 123342, 123344


Torque Arm PinAIR 123350


Torque arm pin AIR127288 N/A NLG 75067 FL N/A N/A #VALUE!

CylinderAIR 123300


Retract Actuator PinAIR 123346, 127298


Trunnion Bolt retainingP/N AIR 123816

395 NLG 54793 FL 39822 94615 53275

Trunnion Pin InnerP/N AIR 124284, 134492, 127286

NE10-009 NLG 66357 FL 39822 55898 14558


TRA14 NLG 75067 FL 39822 114889 73549


TRA15 NLG 75067 FL 39822 114889 73549

CylinderP/N AIR 123300

BEL0160 NLG 79822 FL 39822 119644 78304

Retract PinP/N AIR 123346

LK8705162 NLG 17323 FL N/A N/A #VALUE!

NLG SHOCK STRUT P/N AIR 83522

NLG SHOCK STRUT P/N AIR 83562-6 S/N LK8802036 CSN 25,799


WO37100556 NLG 75067 FL 39822 82236 40896

Trunnion BoltP/N AIR 123816


Trunnion PinP/N AIR 124284, 134492, 127286








Trunnion BoltP/N AIR 123816


Trunnion PinP/N AIR 124284, 127286, 134492








NLG DRAGBRACE ASSEMBLY P/N AIR 84306-8S/N LK84306/8 CSN 30010Trunnion PinP/N AIR 127290, 127292

1807 NLG 66357 FL 39822 59905 18565

63 NLG 66357 FL 39822 59905 18565Trunion pin AIR 123514, 123516 N/A NLG 26033 NA NA #VALUE!



Downlock RollerP/N AIR 126706

GIN6745 NLG 12000 FL 39822 51822 10482

Roller PinP/N AIR 124544

AF01902 NLG 12000 FL 39822 51822 10482

ScrewP/N AIR 123540

MAN226 NLG 12000 FL 39822 51822 10482

Shear Bolt or ARD4312/3P/N AIR 124050

FF2063 NLG 24000 FL 39822 63822 22482

NLG DRAGBRACE ASSEMBLY P/N AIR 84350

Downlock RollerP/N AIR 126076


Roller PinP/N AIR 124544


ScrewP/N AIR 123540


Shear BoltP/N AIR 124050


Trunnion PinP/N AIR 127290, 127292


MLG SHOCK STRUT ASSEMBLY P/N AIR 83022-12Strut Life SN LK8905154 LH 90000 FL 39643 106483 65143Trunnion Pin (Inner)P/N AIR 127280

W26157 LH 79879 FL 39643 119522 78182

Trunion pin (inner) AIR 125342 NSN LH 7672 NA NA #VALUE!

Trunnion Pin (Outer)P/N AIR 127278

528 LH 83729 FL 39643 123372 82032

AIR 123442 NSN LH 3777 FL NA NA #VALUE!

Torque Arm PinAIR 127282, 123450

SDE460 LH 87097 FL 39643 126740 85400

SDE465 LH 87097 FL 39643 126740 85400Axle AdaptorAIR 127308

44 LH 80022 FL 39643 119665 78325

AIR 123402 LH 2953 FL NA NA #VALUE!

Piston TubeP/N AIR 123410

N/A LH 21206 FL N/A NA #VALUE!

PistonP/N AIR 130230

23 LH 74553 FL 39643 114196 72856

Brake FlangeP/N AIR 127312

TPE6711 LH 36706 FL 39643 76349 35009

DowelP/N AIR 123688

N/A LH 2000 FL N/A N/A #VALUE!

Dowel Pin or ARD6076P/N AIR 130236

FFU355 LH 58979 FL 39643 98622 57282

AIR127314 NSN LH 29878 FL N/A N/A #VALUE!


381 LH 54394 FL 39643 94037 52697

Gas HeadP/N AIR 127304, 123430

FFV352 LH 87097 FL 39643 126740 85400

Lock TabP/N AIR 124052

FFV353 LH 83829 FL 39643 123472 82132

Bearing HousingP/N AIR 125436

FFV354 LH 56838 FL 39643 96481 55141

BoltP/N AIR 127322

FFV386to 391 LH 87097 FL 39643 126740 85400

MLG LOCK STRUT ASSEMBLY P/N AIR 83064

Trunnion PinP/N AIR 127278


AIR 127280 N/A LH 59362 FL N/A N/A #VALUE!



Axle AdaptorAIR 130238






Dowel PinP/N AIR 130236




Gas HeadP/N AIR 127304






BoltP/N AIR 127322


Pivot PinP/N AIR 123738


MLG DRAGBRACE ASSEMBLY P/N AIR 84310-8S/N LK8504013 CSN: 38425Trunnion PinP/N AIR 127294

PK579C21 LH 83729 FL 39870 71420 30080

AIR123740 N/A LH 12030 FL N/A NA #VALUE!Trunnion PinP/N AIR 129662

TPE9212 LH 56980 FL 39870 96850 55510

AIR 12418 N/A LH 46653 FL N/A NA #VALUE!Upper LinkP/N AIR 129692

PIP155 LH 62694 FL 39870 64139 22799

AIR125162 N/A LH 14098 FL N/A NA #VALUE!

MLG DRAGBRACE ASSEMBLY P/N AIR 84311


N/A LH 83729 N/A NA #VALUE!

AIR 123740 N/A LH 12030 FL N/A NA #VALUE!Trunnion PinP/N AIR 129662

N/A LH 56980 N/A NA #VALUE!

AIR 124218 N/A LH 46653 FL N/A NA #VALUE!Upper LinkP/N AIR 125163


AIR 129693 N/A LH 62694 FL N/A NA #VALUE!




AIR 129662 N/A LH 47034 FL N/A N/A #VALUE!Upper LinkP/N AIR 130246







AIR 129662 N/A LH 47034 FL N/A N/A #VALUE!Upper LinkP/N AIR 130247




MLG SHOCK STRUT ASSEMBLY P/N AIR 83022-12

Trunnion Pin (Inner)P/N AIR 127280

LK8302131 RH 79879 FL 32344 67316 25976

Trunion pin (inner) AIR 125342 LK8302131 RH 7672 FL NA NA #VALUE!

Trunnion Pin (Outer)P/N AIR 127278, 123442

LK8302131 RH 83729 FL 32344 71166 29826

Torque Arm PinAIR 127282, 123450

LK8302131 RH 87097 FL 32344 74534 33194

Axle AdaptorAIR 127308, 123402

LK8302131 RH 80022 FL 32344 67459 26119

Piston TubeP/N AIR 123410

N/A RH 21206 FL N/A N/A #VALUE!


LK8302131 RH 74553 FL 32344 62030 20690


TPE-2506 RH 36706 FL 32344 68283 26943

DowelP/N AIR 123688


Dowel Pin or ARD6076P/N AIR 130236, 127314

LK8302131 RH 58979 FL 32344 46416 5076


LK8302131 RH 54394 FL 32344 54394 13054

Gas HeadP/N AIR 123430, 123430

LK0312131 RH 87097 FL 32344 74534 33194


LK0312131 RH 83829 FL 32344 71266 29926


LK0312131 RH 56838 FL 32344 89182 47842

BoltP/N AIR 127322

LK0312131 RH 87097 FL 32344 74534 33194

MLG SHOCK STRUT ASSEMBLY P/N AIR 83064

Trunnion PinP/N AIR 127278, 127280




Axle AdaptorAIR 130238






Dowel PinP/N AIR 130236




Gas HeadP/N AIR 127304






BoltP/N AIR 127322







AIR 127294 NA RH 83729 FL N/A N/A #VALUE!Trunion pin AIR 129662 NA RH 56980 FL N/A N/A #VALUE!AIR 124218 NA RH 46653 FL N/A N/A #VALUE!Upper LinkP/N AIR 125162


AIR 129692 NA RH 62694 FL N/A N/A #VALUE!MLG DRAGBRACE ASSEMBLY P/N AIR 84311-7S/N LK8902357Trunnion PinP/N AIR 127294

427 RH 83729 FL 39639 78120 36780

AIR 123740 N/A RH 12030 FL N/A N/A #VALUE!


PT254A RH 56980 FL 39639 51371 10031


Upper LinkP/N AIR 129693

PIP182 RH 62694 FL 39639 57085 15745





AIR 129662 N/A RH 47034 N/A N/A #VALUE!








AIR 129662 NA RH 47034 FL N/A N/A #VALUE!





Chapter 33 Lighting

Operational test of Emergency Light System (International andExternal) including floor proximity escape signs. Pre-mod 2523335001

057 N/A 400 FH 36926.9 37326.9 86.5

AB

057 #1 1 Y 05/2004 05/2005#2 05/2004 05/2005#3 05/2004 05/2005#4 05/2004 05/2005#5 05/2004 05/2005

Operational test of Emergency Light System (International andExternal) including floor proximity escape signs. post-mod 2523335003

057 N/A 6 M N/A N/A

Functional test of Emergency battery pack capacity. Post mod2523335004

057 N/A 6 M N/A N/A

Chapter 34 Navigation

4660 L/H 2 Y 05/2003 05/20052087 R/H 05/2003 05/20052512 Stby 05/2003 05/2005

Isolation and leak test of shut off valves341102

057 N/A 2 Y 05/2003 05/2005

Visual check of LH, RH and standby water traps for wateraccumulation. Drain if required.341103

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Inspect total pressure drain hole for blockage.341104

057 N/A 800 FH 36431.7 37231.7 -8.7AB ODD

Leak test of AIR DATA COMPUTER and Functional test ofADC Overspeed Warning.341201

057 N/A 2 Y 05/2003 05/2005

Functional check of Altimeter, ASI, VSI, Stby Altimeter & StbyASI during leak test.341301

057 N/A 2 Y 05/2003 05/2005

Bench Inspection and Charge Test of Emergency Light PowerSupplies Pre mod 2523335002

Leak test of static/dynamic line (LH, RH and STBY SYST).341101

Functional test of ASI overspeed warning, during leak test.341302

057 N/A 2 Y 05/2003 05/2005

Functional test of Altimeter & Stby Altimeter vibrator function341303

057 N/A 2 Y 05/2003 05/2005

057 #1 2 Y 05/2003 05/2005#2 05/2003 05/2005

Operational check of Go-Around mode (EADI).342201

057 N/A 4000 FH 33157.8 37157.8 -82.6

Operational check (during flight) of Loss of Approach Mode(NOTE: A functional check may be performed if consideredpractical).342202


Operational check (during flight) of Loss of Approach Mode(NOTE: A functional check may be performed if consideredpractical).342203

057 N/A 2500 FH 35328.9 37828.9 588.5

Perform Stby compass swing.342301

057 N/A 1 Y MCM na

Operational check of ADI/HSI reversionary mode.342401

057 N/A 4000 FH 33157.8 37158.7 -81.7

Ops check of DRIVE XFR/XSIDE data mode.342402

057 N/A 4000 FH 33157.8 37158.7 -81.7

Bench test of computer.344001

4511 N/A 7000 FH 33164.3 40164.3 2923.9

Operational check ot test inhibit function.344101

057 N/A 4000 FH 33157.8 37157.8 -82.6

344201 insp grease ant 057 N/A 800 FH 36431.7 37231.7 -8.7 AB ODD057 N/A 2 Y 05/2003 05/2005

05/2003 05/2005

Functional check of AFH Air Speed inputs.342102

Functional check of ATC Transponder345401

Chapter 35 Oxygen

Inspection and hydrostatic test of oxygen cylinder.351105

ALT279-2500 N/A 3 Y 05/2003 05/2006

442 co-pilot 3 Y 05/2003 05/2006483 captain 06/2003 06/20061731 observer 09/08/03 09/08/06

Restoration of regulator assy.351107

2378 MAIN 02 6 Y 01/2000 01/2006

ALT279-2500 N/A 15 Y 12/1990 12/2005NA NA NANA N/A 15 Y NA NA

Discard Oxygen bottle.P/N 803358-01NOTE: Interval from date of manufacture.351109

N/A N/A 15 Y N/A N/A

Functional check of oxygen pressure switch. Non-US operators351203

057 N/A 3 Y 04/28/2003 04/28/2006

Functional check of oxygen pressure switch. US Operators.351204

N/A N/A 8000 FH na na #VALUE!

Operation of toggle valve and check of oxygen supply to alloutlets. If drop down system not installed.352001

N/A N/A 4000 FH 33158.7 37158.7 -81.7

General visual check of passenger masks. If drop down systemnot installed.352002

057 N/A 4000 FH 33158.7 37158.7 -81.7

Functional check of pressure switch. P/N:36136. If drop outsystem installed.352004

N/A N/A 3 Y N/A N/A

Inspection and test of crew mask.351106

Discard Oxygen bottle.P/N 89506050P/N 803207-01

Operational check of passenger oxygen drop out system. Ifdrop out system installed.352005

N/A N/A 3 Y N/A N/A

General visual check of passenger oxygen drop out maskx. Ifdrop out system installed.352006

N/A N/A 3 Y N/A N/A

Open "ON-OFF" valve and check with connected mask thatoxygen is available tFHough mask.353003

057 N/A 4000 FH 33164.3 37164.3 -76.1

Inspection and test of smoke mask353004

8515 N/A 3 Y 12/2003 12/2006

106613 1st

AIDPORT.

5 Y 10/2000 10/2005

187438 LARGE 5/2003 5/2008151024 LWR PORT 5/2003 5/2008103786 1st AID

PORT.

5 Y 10/2000 10/2005

104807 5/2003 5/2008K10050 LWR PORT 5/2003 5/2008

Inspection of PBE354001

N/A 4000 FH 33157.8 37158.7 -81.7

E000027 N/A 10 Y 07/2000 07/2010E004284 12/2000 12/2010E9548678 11/1995 11/2005

CHAPTER 36 PneumaticInspect Peri-Seals for security, condition and signs ofleakage.Bleed air leak361108

057 N/A 600 FH 37180.1 37780.1 539.7

Operational check of valve shut-off ejector precooler andinspection of ejector nozzle for cleanliness.361202

057 N/A 4000 FH 33157.8 37158.7 -81.7

Bench check of bleed air high pressure switch, bleed air hightemperature switch and continuity check of harness.362201

057 N/A 8000 FH 36213.6 44213.6 6973.2

Inspection and hydrostatic test of oxygen cylinder.353005

Overhaul of regulator assembly - Inspection and test lowpressure assembly for leakage.353006

Discard PBE354002

362301 inspect exposed leak detection sensing element in flapcove areas WS48.00 to WS127 for security, damage andalignment

057 NA 800 FH 36926.9 37626.9 386.5

AB EVEN

362302 inspect leak detection sensing elements in nacelleareas and in wing/fuselage area for damage, security alignment

057 N/A 4000 FH 33157.8 37158.7 -81.7

Operational check of high stage bleed valve manual control361101

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of X-valve manual contro.361102

057 N/A 4000 FH 33158.7 37158.7 -81.7

Remove and inspect mid stage bleed air check valve forgeneral condition.361104

057 N/A 12000 FH 25247.1 37247.1 6.7

Chapter 52 Doors

Inspect door main hinge, stabilizing rod arm and secondaryhinge arm pivoting points for sign of wear. Operate door.521301

057 N/A 4000 FH 33158.7 37158.7 -81.7

Inspect door seal and door way sealing strip nib for wear anddamage.521401

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Operational check of pilot escape hatch.522101

057 N/A 4000 FH 33158.7 37158.7 -81.7

Visual inspection of pilot escape hatch seal for generalcondition.522102

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operation check of FWD emergency door from both inside andoutside.522201

057 N/A 4000 FH 33158.7 37158.7 -81.7

Operational check of overwing emergency exit doors type IIIfrom both inside and outside.522301

057 N/A 4000 FH 33158.7 37158.7 -81.7

Treat counter balance springs with corrosion inhibitor.523301

057 N/A 4000 FH 33158.7 37158.7 -81.7

Visual inspection and operational check of entrance stair.526001

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

Chapter 53 Fuselage

Lubricate wing to fuselage attachment link bolts at greasefittings.534101

057 N/A 4000 FH 33158.7 37158.7 -81.7

Chapter 56 Windows

Discard windshield/side window attachment bolts.561003

057 N/A 24000 FL 23934 47934 6594

Chapter 61 Propellers

PROPELLER (HAMILTON STANDARD)611001 visual prop na na LC1 LC1 LC1Visually inspect propeller blade retention area for security andgeneral condition. (340B Only)611002


N/A L/H 6500 FH N/A N/A #VALUE!N/A R/H 6500 FH N/A N/A #VALUE!

N/A L/H 800 FH N/A N/A #VALUE!N/A R/H N/A N/A #VALUE!


Remove propeller for major inspection. (340B Only)611004

Propeller hub oil level check. (340B only)611005

Perform torque check of the primary ballscrew quill. (340BOnly)

PROPELLER (DOWTY AEROSPACE)611001 VISUAL PROP 057 NA LC1 LC1 LC1Visually inspect blade surfaces for signs of damage anddelamination.611002

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

057 L/H 4000 FH 33157.8 37157.8 -82.6R/H 33157.8 37157.8 -82.6

L/H Hub 7500 FH or5 Y*

SEEPROPS

SEEPROPS

#1 Blade 7500 FH or5 Y*

THISSECTION




R/H Hub 7500 FH or5 Y*

SEEPROPS

SEEPROPS


THISSECTION




Check the propeller blades for excessive movement of theblade tips.611007

057 N/A 800 FH 36431.7 37231.7 -8.7

AB ODD

057 L/H 400 FH 36926.9 37326.9 86.5 ABR/H 36926.9 37326.9 86.5 AB

Perform PCU power level spring check on aircraft. (Dowty)612005

057 N/A 4000 FH 33157.8 37157.8 -82.6

Visually inspect propeller assembly including the hub assy, de-icing boots, slip rings and spinner assy for general condition and

Remove propeller for overhaul. *Réf. Dowty SB 61-996 latestrev. For calendar limit.611005

Remove propeller for overhaul. *Réf. Dowty SB 61-996 latestrev. For calendar limit.611005

Perform propeller overspeed test.612004

057 L/H 400 FH 36926.9 37326.9 86.5 ABR/H 36926.9 37326.9 86.5 AB

612302 Check aux motor and pump, connectors and harness ifhamilton prop installed B model

NA LH/RH 3000 FH N/A N/A #VALUE!

N/A N/A #VALUE!N/A L/H 300 FH N/A N/A #VALUE!N/A R/H N/A N/A #VALUE!

Perform autocoarsen system test. (340A Only) PRE-MOD2198 (SB61-026). Interval only applicable if task 612503 isperformed.612502


Perform autocoarsen system test. POST-MOD 2198 (SB 61-026)612502

N/A N/A 200 FH LC2 LC2 #VALUE!

Perform autocoarsen system test. POST-MOD 2198 (SB61-026). Interval only applicable if task 612503 is performed.612502


Perform P3-switch test. POST-MOD 2198 (SB61-026). NOTrequired if task 612502 is performed at interval 200 FH.612503


Operational test of propeller brake lock valves. NOT applicableif Prop Brake system disabled613004






Perform propeller pitch change test.612301

Perform autocoarsen system test. (340B Only) PRE-MOD2198 (SB61-026). Interval only applicable if task 612503 is

Operational system test.613005

Inspect brake pads and disc for degradation.613007

Penetrant or magnaflux inspect propeller brake disc.613008

Inspect propeller brake assembly for oil contamination.613009

N/A L/H 22000 FL N/A N/A #VALUE!N/A R/H N/A N/A #VALUE!

Chapter 71 Powerplant

711001 visual 057 LC2 LC2 LC2

Visual inspection: Aft mounts for condition and security.712001

057 N/A 500 FH 36844.6 37344.6 104.2

Visual inspection: Prop gear box side mounts for condition andsecurity. PRE-MOD 2020 (SB 71-32).712002

057 N/A 1200 FH na by SB NA #VALUE!

4005 LH Bottom 5000 FH 36575.2 41575.2 4334.8346 RH bottom 33159.6 38159.6 919.2038 LH IB 5000 FH 36575.2 41575.2 4334.8032 LH OB 5000 FH 36575.2 41575.2 4334.8235 RH IB 5000 FH 36144.9 41144.9 3904.5

328 RH OB 5000 FH 33159.6 38159.6 919.2Visual inspection: Aft mounts, prop gear box bottom and sidemounts for condition and security.712004

057 N/A At enginechange

AT ENGINE CHANGE

Discard prop gear box bottom mount molded assemblies (P/N:00-12193-01)712005


Discard prop gear box bottom mount bonded canister (P/N:00-13226-01) if installed. (POST-MOD 1777 (SB 71-023). PRE-MOD 2659 (SB 71-047)712006


Discard prop gear box bottom mount bonded canister (P/N:00-13226-01) if installed. (PRE-MOD 1777 (SB 71-023) 340A.712007


Discard prop gear box bottom mount bonded canister. (P/N: 00-13226-03)712008


Discard propeller brake control assembly P/N HP1410100-3 ifinstalled

Remove prop gear box bottom and side mounts for overhaul.712003

15082 LH Fwd 5000 FH 36278.7 41278.7 4038.315083 LH Aft 36278.7 41278.7 4038.315431 36844.6 41844.6 4604.215432 36844.6 41844.6 4604.2

Visual inspection and cleaning of thermocouple harnessconnector and mating connector.715003

057 N/A 4000 FH 33157.8 37157.8 -82.6

717101 drain collector tank 057 NA 150FH LC2 LC2Chapter 72 Engine

057 L/H 150 FH LC2 LC2 #VALUE!057 R/H LC2 LC2 #VALUE!

720000pg701 eng wash 057 N/A 250 FH 37076.8 37326.8 86.4720003 Csump seals 367499 LH 1500FH 36244.5 37744.5 504.1

367275 RH 1500FH 36844.6 38344.6 1104.2367499 L/H 1000 FH 36244.5 37244.5 4.1367275 R/H 36982.6 37982.6 742.2

721003 visual PGB prop 57 NA at prop inst.367499 L/H At power unit 34797.3 @ CHG367275 R/H change/ At

PGB change33078.3 @ CHG

723101 discard output shaft 57 NA see life limit367499 L/H 4000 FH 33157.8 37157.8 -82.6367275 R/H 33157.8 37157.8 -82.6

367237 L/H 800 FH 36431.7 37231.7 -8.7 AB ODD367275 R/H 36431.7 37231.7 -8.7 AB ODD

367499 L/H Per G.E MM367275 R/H SEI 576

367499 L/H 4000 FH 34797.3 38797.3 1556.9367275 R/H 33078.3 37078.3 -162.1

367499 L/H 400 FH 36926.9 37326.9 86.5 AB367275 R/H 36926.9 37326.9 86.5 AB

367499 L/H 800 FH 36926.9 37626.9 386.5 AB EVEN367275 R/H 800 FH 36926.9 37626.9 386.5 AB EVEN

367499 L/H 800 FH 36926.9 37626.9 386.5 AB EVEN

Discard aft engine mounts712009

Monitor propeller gearbox chip detector for metallic particles bymeasurement on external chip detector harness.

Remove, inspect and clean PGB chip detector.721004

Visual inspection of PGB drive shaft for general condition andsecurity.723202

Manually actuate linkage assembly and visually inspectcompressor stator, linkage assembly, actuating rings, levers

Inspect power unit stage 4 bleed air boss, and fitting oncompressor casing for condition, security and leakage. 340A

Discard rotating components at published life limits. NOTE:Rotating Parts Life Management Program to monitor part

See Life Limit SectionPages 1 & 2

Borescope inspection of stage 1 and 5 compressor rotorblades, rotor lands/coatings, stage 1 and 5 vanes, IGV's, and

Visual inspection of the stage 1 blades and IGV's tFHough theinlet using a bright light.

Borescope inspection of power unit combustion liner, stages 1and 2 turbine nozzles, stages 1 and 2 turbine rotor blades,

Inspect power unit stage 4 bleed air boss, and fitting on

367275 R/H 36926.9 37626.9 386.5 AB EVEN

N/A L/H 800 FH N/A N/A #VALUE!N/A R/H 800 FH N/A N/A #VALUE!

367499 L/H 800 FH 36926.9 37626.9 386.5 AB EVEN367275 R/H 800 FH 36926.9 37626.9 386.5 AB EVEN

367499 L/H Per G.E MM367275 R/H SEI 576

367499 L/H Per G.E MM367275 R/H SEI 576

367499 L/H Per G.E MM367275 R/H SEI 576

726101 ck common drain 57 NA LC1 LC1 LC1367499 L/H 2400 FH 35447.4 37847.4 607367275 R/H 36844.6 39244.6 2004.2

Chapter 73 Engine Fuel

731001 visual o/board drai 057 NA LC2 LC2 LC2367499 L/H 600 FH 37180.1 37780.1 539.7367275 R/H 37180.1 37780.1 539.7

367499 L/H 3000 FH 34797.3 37797.3 556.9367275 R/H 36844.6 39144.9 1904.5

367499 L/H 400 FH 36926.9 37326.9 86.5 AB367275 R/H 36926.9 37326.9 86.5 AB

367499 L/H 4000 FH 33159.6 37159.6 -80.8367275 R/H 33159.6 37159.6 -80.8

367499 L/H 1600 FH 36406.4 38006.4 766367275 R/H 36844.6 38444.6 1204.2

Chapter 74 Engine controls

367499 L/H LC2 LC2 NA #VALUE!367275 R/H LC2 NA #VALUE!

367499 L/H 400 FH 36926.9 37326.9 86.5 AB

compressor casing for condition, security and leakage. 340A

Borescope inspection of power unit combustion liner, stages 1and 2 turbine nozzles, stages 1 and 2 turbine rotor blades, and

Borescope inspection of stage 3 power turbine blades andexposed portions of stage 3 nozzle.

Discard rotor disks and cooling plates at published life limits.724404


Discard power turbine shaft at published life limits.725301


Discard power turbine attaching hardware when replacingpower turbine engine shaft and/or power turbine rotor disks.

COMPLIED WITH BYGE AT LAST VISIT

Inspection of power unit radial drive shaft for general conditionand for spline wear.

Visual inspection and cleaning of the tFHee fuel injectorslocated at clock positions of 12, 1, and 2 viewed from aft

Visual inspection and cleaning of the nine fuel injectors locatedat clock position 3 tFHu 11 viewed from aft looking forward.

Perform operational check of engine overspeed protectionsystem ("A" and "B" separately, then "A" and "B" together).

Functional check: Fuel filter impending bypass circuit.733301

Replace power unit fuel filter element.733302

Inspect ignitor plugs. PRE-MOD 1414 (SB 74-004).742001

Inspect ignitor plugs.post mod 1414

367275 R/H 36926.9 37326.9 86.5 AB

Chapter 76 Engine Electronics

N/A L/H 2 Y N/A BY P/N -12FN/A R/H N/A N/A

N/A L/H 6000 FL N/A BY P/N -12F #VALUE!N/A R/H N/A N/A #VALUE!

057 L/H 4000 FH 33157.5 37157.5 -82.9057 R/H 33157.5 37157.5 -82.9

057 L/H 8000 FH 36213.6 44213.6 6973.2057 R/H 36213.6 44213.6 6973.2

057 L/H 4000 FH 33157.8 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

057 L/H 4000 FH 33157.8 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

057 L/H 4000 FH 33157.8 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

057 L/H 8000 FH 36213.6 44213.6 6973.2057 R/H 36213.6 44213.6 6973.2

057 L/H 4000 FH 33157.8 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

057 L/H 300 FH N/A N/A #VALUE!057 R/H N/A N/A #VALUE!

057 L/H 4000 FH 33157,8/ 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

057 L/H 4000 FH 33157.8 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

057 L/H 1600 FH 36144.9 37744.9 504.5057 R/H 36844.6 38444.6 1204.2

742002

Replace control quadrant P/N 53082-7.761001

Replace control quadrant. P/N 53170.761002

Lubricate inner rod of power control cables at wing/fuselageinterface.

Purge control cables with nitrogen and replace O-rings in sealfitting of control cables at wing/fuselage interface.

Inspect the two-pin joint of the control cables for axial play atthe HMU, the wheelwell, and the wing/fuselage interface. PRE-

Perform control cable tension check761108

Lubricate inner rod of condition lever control cables atwing/fuselage interface.

Purge control cables with nitrogen and replace O_rings in sealfitting of control cables at wing/fuselage interface.

Perform control cable tension check761207

Perform Automatic Power Reserve (APR) system test. (340Bonly)

Operational check of the FI stop override function POST-MOD2558 (SB 76-032 & 76-038)

Operational check of the "FI STOP OPEN" indication POST-MOD 2558 (SB 76-032 & 76-038)

Operational check of emergency shutdown system.762001

Chapter 77 Engine Electronics

057 L/H 4000 FH 33157.8 37157.8 -82.6057 R/H 33157.8 37157.8 -82.6

Chapter 79 Engine Oil

367499 L/H 2400 FH 34797.3 37197.3 -43.1367275 R/H 36844.5 39244.5 2004.1

791101 check oil level 57 NA LC1 LC1 LC1367499 L/H 4000 FH 33157.8 37157.8 -82.6367275 R/H 33157.8 37157.8 -82.6

791102 drain exhaust pipes 57 NA LC1 LC1 LC1367499 L/H LC2/800FH 35557.8 na #VALUE!367275 R/H 33809.1 NA #VALUE!

367499 L/H 4000 FH 33158.7 37158.7 -81.7367275 R/H 33158.7 37158.7 -81.7

367499 L/H 4000 FH 33158.7 37158.7 -81.7367275 R/H 33158.7 37158.7 -81.7

367499 L/H 800 FH 36431.7 37231.7 -8.7 AB ODD367275 R/H 36431.7 37231.7 -8.7 AB ODD

367499 L/H 800 FH 36926.9 37626.9 386.5 AB EVEN367275 R/H 36926.9 37626.9 386.5 AB EVEN

791201 PGB bypass 57 NA LC1 LC1 LC1367499 L/H 4000 FH 33158.7 37158.7 -81.7367275 R/H 33158.7 37158.7 -81.7

791202PGBoil level 57 NA LC2 LC2 LC2367499 L/H 400 FH 36926.9 37326.9 86.5 AB367275 R/H 36926.9 37326.9 86.5 AB

367499 L/H 800 FH 36926.9 37626.9 386.5 AB EVEN367275 R/H 36926.9 37626.9 386.5 AB EVEN

367499 L/H 800 FH NA NA #VALUE!367275 R/H NA NA #VALUE!

Functional check of ITT-Indication and ENG HOT light by useof ITT Test Set.

Replace power unit lube filter element.791103

Remove power unit electrical chip detector and check thefunction by performing electrical check of circuit.

Remove, inspect and clean power unit electrical chip detector.NOTE: First LC" after new/overhauled engine installation.

Remove, inspect and clean power unit scavenge screens.791107

Visual inspection of oil cooler impending leakage inspectionhole at the 12 o'clock position on oil cooler. If oil cooler with

Remove, inspect and clean power unit B-sump scavengescreen and delta P reference tube.

Operational check of the low oil pressure switch.180UP793201

Visual inspection and cleaning of 7:30 o'clock exhaust strut oilsupply tube drain hole.

Change the propeller gearbox oil and filter.791206

Visual inspection: Oil cooler inlet and exhaust ducts forblockage.

Operational check of the low oil pressure switch.793101

Fig & Item Description

InitialInspection

(hrs)

Reinspection

(hrs)

Last Done

(hrs)

Due Next

(hrs)

Remaining

(hrs)

5210-813-01I Inspect main entrance door guide pins and door stops forcracks. Detailed

27000 FL 12000 FL 38923 50923 9583

5210-813-80I Inspect main entrance door guide pins and door stops forcorrosion.

6 Y 2 Y 06/2004 06/2006

5220-815-01E5220-816-01E Inspect rear emergency doorwindow frames, at the edge of the

cut-out, for cracks.

30000 FL 12000 FL 29963 41963 623

5311-113-01I Inspect forward pressure bulkead lower left hand part STA-145at stiffener BL. 21 for cracks. A/C 004-018

28000 FL 6000 FL N/A N/A #VALUE!

5311-115-01I5311-116-01I Inspect nose gear well side wall stiffeners for cracks.

30000 FL 6000 FL 35938 41938 598

5311-115-02I5211-116-02I Inspect center floor beam in forward fuselage for cracks.

30000 FL 6000 FL 35938 41938 598

5311-145-01I Inspect web at BL 0, cabin pressure bulkhead STA401 forcracks.

30000 FL 6000 FL 35938 41938 598

5311-151-01I5311-152-01I

Inspect cabin pressurebulkhead STA 401, including all stiffeners for cracks.

30000 FL 12000 FL 29663 41963 623

5311-145-02I5311-146-01I5311-151-02I5311-152-02I5311-161-01I5311-162-01I

Inspect cabin pressurebulkhead, webs at STA 401 &STA 475.5 for cracks.

30000 FL 12000 FL 29963 41963 623

5311-151-03I5311-152-03I Inspect cabin pressure bulkheads at STA 475.5 and STA 401,

upper flanges in bend radius, for cracks.

22000 FL 6000 FL N/A by SB N/A #VALUE!

STRUCTURAL INSPECTIONS



26000 FL 12000 FL 36069 48069 6729



26000 FL 12000 FL 34948 46948 5608

5311-210-01I Inspect fwd fuselage pressure bulkhead upper flange aroundBL 23.35 and RBL 23.35 for cracks. Detailed A/C 004-048

30000 FL 12000 FL 29963 41963 623

5311-317-01I5311-318-01I Inspect rear pressure bulkhead, STA 853, vertical beams to

skin attachments, BL 4.29 & RBL 4.29 for cracks.

30000 FL 12000 FL 29963 41963 623

5312-181-01I Inspect frame STA 630.112 inner flange from lower sill to SL1524 for cracks. Detailed ALL 30.000 fl/6.000

30000 FL 6000 FL 35938 41938 598

5312-210-01I Inspect windshield lower sill support frame at BL.29 and RBL29, aft of STA 160, for cracks.

30000 FL 12000 FL 29963 41963 623

5312-225-01I Inspect main door frame, STA 258, inner flange from WL 126.5to WL 137.5 for cracks.

30000 FL 12000 FL 29963 41963 623

5312-225-02I Inspect main door frame, STA 258, inner flange, including boxarea at bottom guide for cracks.

30000 FL 12000 FL 29963 41963 623

5312-225-03I Inspect fwd emergency exit frame, STA 272, inner flange forcracks.

30000 FL 12000 FL 29963 41963 623

5312-225-04I Inspect main door frame, STA 288, inner flange from WL 75.5to WL 82.0 especially upper and lower ends of gusset plate atbottom guide for cracks.

30000 FL 6000 FL 35938 41938 598

5312-225-05I Inspect main door frame, STA 288, inner flange below WL122.0 for cracks.

30000 FL 12000 FL 29963 41963 623

5312-225-06I Inspect support bracket for fwd top guide pin at main entrancedoorway for cracks.

30000 FL 12000 FL 29963 41963 623

5312-225-07I Inspect support bracket for aft top guide pin at main entrancedoorway for cracks.

30000 FL 12000 FL 29963 41963 623

5312-225-08I Inspect inboard flange of the upper sill at the upper fwd cornerof the main entrance doorway for cracks. 340A

26000 FL 9000 FL 34948 43948 2608

5312-225-09I Inspect forward Emergency Exit door frame STA 294, innerflange for cracks.

30000 FL 12000 FL 29963 41963 623

5312-241-01I5312-242-01I Inspect rear emergency exits, frame below WL 100.0 for

cracks.

30000 FL 12000 FL 29963 41963 623

5312-241-02I5312-242-02I Inspect fwd wing support frame below WL 100.0 for cracks.

30000 FL 12000 FL 29963 41963 623

5312-241-04I5312-242-04I Inspect frame STA 401.0 between WL 71 and WL 76 for

cracks.

30000 FL 12000 FL 29963 41963 623

5312-241-05I5312-242-05I Inspect angle at frame STA 435.5 at WL 73.5 for cracks.

30000 FL 12000 FL 29963 41963 623

5312-241-06I5312-242-06I Inspect angle at frame STA 439.5 at WL 73.5 for cracks.

30000 FL 12000 FL 29963 41963 623

5312-251-01I5312-251-01I Inspect rear wing support frame below WL 100.0 for cracks.

30000 FL 12000 FL 29963 41963 623


cracks. 340A

16000 FL 6000 FL 35938 41938 598


cracks. 340A

30000 FL 12000 FL 35938 41963 623


cracks. 340B

30000 FL 12000 FL 29963 41963 623

5312-251-06I5312-251-06I Inspect rear emergency door frame STA 461.5, inner flange,

for cracks.

30000 FL 12000 FL 29963 41963 623

5312-271-01E Inspect cargo door reinforcement edge at frame STA 630.112 30000 FL 6000 FL 35938 41938 598

5312-271-01I Inspect frame STA 630.112 inner flange from SL 1504 to lowersill for cracks.

30000 FL 6000 FL 35938 41938 598

5312-271-02E Inspect cargo door reinforcement edge at frame STA 686.888for cracks.

30000 FL 6000 FL 35938 41938 598

5312-271-02I Inspect frame STA 686.888, inner flange from SL 1504 tolower sill for cracks.

30000 FL 6000 FL 35938 41938 598

5312-310-01I Inspect machined web at stabilizer and fin attachments, STA758 and STA 781, for cracks. Detailed 340B

20000 FL 12000 FL N/A N/A #VALUE!

5313-181-01E Inspect lower sill cargo door reinforcement edge at door cut outfrom STA 630.112 to STA 686.888 for cracks.

30000 FL 6000 FL 35938 41938 598

5313-181-01I Inspect lower sill cap joints at STA 630.112 for cracks. 30000 FL 6000 FL 35938 41938 598

5313-181-02I Inspect lower sill cap joints at STA 686.888 for cracks. 30000 FL 6000 FL 35938 41938 598

5313-200-01E Inspect all cabin window frames at the edge of the cut-outs forcracks.

30000 FL 6000 FL 35938 41938 598

5313-210-01E Inspect windshield lower sill external doublers (gussets) at rearpost, side post and center post for cracks.

30000 FL 3000 FL 38853 41853 513

5313-210-01I Inspect windshield lower sill inner flange gusset at side post forcracks.

30000 FL 6000 FL 35938 41938 598

5313-210-02E Inspect windshield upper sill, external gussets ans skin panelsat rear post, side post and center post for cracks.

30000 FL 3000 FL 38853 41853 513

5313-210-02I Inspect windshield upper sill inner flange gusset at side post forcracks.

30000 FL 6000 FL 35938 41938 598

5313-210-03I Inspect lower sill windshield frame lugs for cracks. 30000 FL 12000 FL 29963 41963 623

5313-210-04I Inspect upper sill windshield frame lugs for cracks. 30000 FL 12000 FL 29963 41963 623

5313-210-05I Inspect windshield, lower sill inner flange gusset at center post,inner flange and outer flange for cracks.

30000 FL 12000 FL 29963 41963 623

5313-210-06I Inspect windshields upper sill inner flange gusset at center post,inner flange and outer flange for cracks.

30000 FL 12000 FL 29963 41963 623

5313-271-01E Inspect upper sill cargo door reinforcement edge at door cut outfrom STA 630.112 to STA 686.888 for cracks.

30000 FL 6000 FL 35938 41938 598

5313-271-01I Inspect upper sill joint plate at STA 630.112 for cracks. 30000 FL 12000 FL 29963 41963 623

5313-271-02I Inspect upper sill joint plate at STA 686.888 for cracks. 30000 FL 12000 FL 29963 41963 623

5315-271-01I Inspect center post, windshield attachment lugs for cracks. 30000 FL 12000 FL 29963 41963 623

5315-271-02I Inspect side post windshield attachment lugs for cracks. 30000 FL 12000 FL 29963 41963 623

5315-271-03I Inspect windshield center post below WL 109, center post,inner flanges and center post outer flanges for cracks.

30000 FL 12000 FL 29963 41963 623

5315-271-04I Inspect side posts, inner and outer flanges for cracks. 30000 FL 12000 FL 29963 41963 623

5315-271-05I Inspect rear posts inner flange splice at upper sill, inner andouter flanges for cracks.

30000 FL 12000 FL 29963 41963 623

5331-122-01I5331-174-01I Inspect skin panel around toilet service installation cut out for

cracks.

30000 FL 12000 FL 29963 41963 623

5331-317-01E5331-318-01E Inspect tail cone skin panels between frames STA 793 ans

STA 853, between BL 10 & RBL 10 for cracks.

30000 FL 12000 FL 29963 41963 623

5332-181-01E Inspect lower corners of cargo door reinforcement for cracks. 30000 FL 3000 FL 38853 41853 513

5332-181-01I Inspect cargo door reinforcement lower splice at STA 655 forcracks.

30000 FL 12000 FL 29963 41963 623

5332-181-02E Inspect skin panel around cargo door for cracks. 30000 FL 6000 FL 35938 41938 598

5332-191-01I5332-192-01I Inspect skin panels around wing cut out, skin and doubler at

forward corner for cracks.

30000 FL 12000 FL 29963 41963 623

5332-210-01E Inspect skin panel around the pitot tubes cut outs for cracks. 30000 FL 12000 FL 29963 41963 623

5332-225-01E Inspect skin panels around main entrance door, upper fwdcorner from STA 258 to STA 264.5 and from WL 135 to WL139.8 for cracks. Special detailed.

30000 FL 12000 FL 29963 41963 623

5332-225-02E Inspect skin panel around main entrance door, lower rearcorner from STA 284 to STA 288 and from WL 70.1 to WL 76for cracks.

30000 FL 12000 FL 29963 41963 623

5332-225-03E Inspect skin panel around main entrance door, skin and doublerat edge of cut out for cracks.

30000 FL 12000 FL 29963 41963 623

5332-225-04E Inspect skin panel around fwd emergency door, skin anddoubler at edge of cut out for cracks.

30000 FL 12000 FL 29963 41963 623

5332-241-01E5332-242-01E Inspect rear emergency exits, skin and doubler at lower rear

corner for cracks.

30000 FL 6000 FL 35938 41938 598

5332-241-02E5332-242-02E Inspect rear emergency exits, skin and doubler at upper

forward corner for cracks.

30000 FL 12000 FL 35938 47938 6598

5332-271-01E Inspect upper fwd corner of cargo door reinforcement forcracks.

30000 FL 3000 FL 38853 41853 513

5332-271-01I Inspect cargo door reinforcement, splice at STA 655 for cracks.Special detailed.

30000 FL 12000 FL 29963 41963 623

5332-271-02E Inspectskin panel around cargo door for cracks. 30000 FL 6000 FL 35938 41938 598

5332-271-03E Inspect cargo door cut out, upper rear corner from STA 681 toSTA 685.7 and from WL 122.2 to WL 125.5 for cracks. Specialdetailed A/C 004-068

30000 FL 6000 FL 35938 41938 598

5332-271-04E Inspect cargo door cut out, upper rear corner from STA 681 toSTA 685.7 and from WL 122.2 to WL 125.5 for cracks. Specialdetailed A/C 069 & up.

30000 FL 12000 FL 29963 41963 623

5332-313-01I5332-314-01I Inspect skin cut outs at stabilizer and fin spars for cracks.

30000 FL 3000 FL 38853 41853 513

5341-151-01I Inspect fwd and rear wing/fuselage drag links, bolt hole sleevefor cracks.

30000 FL 12000 FL 29963 41963 623

5341-191-01I5341-192-01I Inspect wing/fuselage attachments, frame lugs for cracks.

30000 FL 6000 FL 35938 41938 598

5411-453-02I5411-463-02I Inspect upper longeron nacelle splice at NS 287 for cracks.

Detailed. 340A

30000 FL 12000 FL 29963 41963 623


Detailed. 340B

30000 FL 12000 FL N/A N/A #VALUE!


Detailed. 340B

28000 FL 6000 FL N/A N/A #VALUE!

5411-453-06I5411-463-06I Inspect upper RH longeron between NS 257 and NS 277.5 for

cracks. NDT

30000 FL 12000 FL 29963 41963 623

5412-453-01E5412-463-01E Inspect frame NS 203 outer flange, inboard and outboard at

WL 96.22 for cracks.

30000 FL 12000 FL 29963 41963 623

5412-453-01I5412-463-01I Inspect forward frame at NS 197 for cracks. Special NDT

30000 FL 12000 FL 29963 41963 623

5412-453-02I5412-463-02I Inspect forward frame at NS 203 for cracks. Special detailed

NDT

30000 FL 12000 FL 29963 41963 623

5413-453-01I5413-463-01I Inspect the nacelle fire deck angle, between frame STA 203

and firedeck, for cracks.

30000 FL 12000 FL 29963 41963 623

5442-453-01I5442-463-01I Inspect the lower engine mount fittings for cracks or broken

fitting.

30000 FL 12000 FL 29963 41963 623

5442-453-02I5442-463-02I Inspect the fixed side engine mounts for cracks or broken

mount.

30000 FL 12000 FL 29963 41963 623

5442-453-03I5442-463-03I Inspect the removable side engine mount fittings for cracks or

broken fittings.

30000 FL 12000 FL 29963 41963 623

5511-332-01E5511-342-01E Inspect upper horiz. stab skin common to spar caps inbd of

HSS 60.0 for cracks.

30000 FL 6000 FL 35938 41938 598

5512-332-01I5512-342-01I Inspect horiz. stab forward spar, upper cap at HSS 27.2 for

cracks. NDT 340A

30000 FL 12000 FL 29963 41963 623


cracks. NDT 340B

30000 FL 12000 FL N/A N/A #VALUE!


cracks. NDT 340A

30000 FL 12000 FL 29963 41963 623


cracks. NDT 340B

30000 FL 12000 FL N/A N/A #VALUE!

5512-332-05I5512-342-05I Inspect horiz. stab rear spar, upper cap at HSS 22.0 for cracks.

NDT 340A

30000 FL 12000 FL 29963 41963 623


NDT 340B

30000 FL 12000 FL N/A N/A #VALUE!


NDT 340A

30000 FL 12000 FL 29963 41963 623


NDT 340B

30000 FL 12000 FL N/A N/A #VALUE!

5512-332-09I5512-342-09I Inspect horiz. stab forward spar, upper cap inboard of HSS

42.0 for cracks.

30000 FL 12000 FL 29963 41963 623

5512-332-10I5512-342-10I Inspect horiz. stab rear spar, upper cap inboard of HSS 37.0

for cracks.

30000 FL 12000 FL 29963 41963 623

5512-332-80I5512-342-80I Inspect horiz stab forward spar caps for corrosion.

6 Y 4 Y 06/2004 06/2008

5512-332-81I5512-342-81I Inspect horiz stab rear spar caps for corrosion.

6 Y 4 Y 06/2004 06/2008

5513-332-01E5513-342-01E Inspect elevator coves for delamination of the anti-static

aluminium foil. Detailed A/C 004-260 pre mod sb 51-012 alt 2

800 HR 800 HR na cw 6-11-95 express #VALUE!

5532-323-80I Inspect vert stab upper front spar caps for corrosion. 6 Y 4 Y 06/2004 06/2008

5551-332-01I5551-342-01I Inspect horiz stab upper front spar finger splice attach to

fuselage frame for cracks. NDT 340A

30000 FL 12000 FL 29963 41963 623

5551-332-02I5551-342-02I Inspect horiz stab upper rear spar finger splice attach to

fuselage frame for cracks. NDT 340A

30000 FL 12000 FL 29963 41963 623

5551-332-03I5551-342-03I Inspect horiz stab upper front spar finger splice attach to

fuselage frame for cracks. NDT 340B

30000 FL 12000 FL N/A N/A #VALUE!

5551-332-04I5551-342-04I Inspect horiz stab upper rear spar finger splice attach to

fuselage frame for cracks. NDT 340B

30000 FL 12000 FL N/A N/A #VALUE!

5551-332-80I5551-342-80I Inspect horiz stab finger splice at front spar for corrosion.

6 Y 4 Y 06/2004 06/2008

5551-332-81I5551-342-81I Inspect horiz stab finger splice at rear spar for corrosion.

6 Y 4 Y 06/2004 06/2008

5552-332-01E5552-342-01E Inspect outboard elevator hinge assembly (stab) at attaching

structure and hinge assy for cracks.

30000 FL 6000 FL 35938 41938 598

5552-332-01I5552-342-01I Inspect inboard elevator hinge assy (stab) at attaching structure

for cracks.

30000 FL 12000 FL 29963 41963 623

5552-333-01E5552-343-01E Inspect inboard elevator hinge fitting (elev) at attaching

structure for cracks.

30000 FL 6000 FL 35938 41938 598

5552-333-02E5552-343-02E Inspect outboard elevator hinge fitting (elev) at attaching


30000 FL 6000 FL 35938 41938 598

5553-333-01I5553-343-01I Inspect the elev cont fitting for accidental damage.

8000 FH 8000 FH 36213.6 44213.6 6973.2

5553-334-01I5553-344-01I Inspect the elev tab act fitting for accidental damage.

8000 FH 8000 FH 36213.6 44213.6 6973.2

5553-334-02I5553-344-02I Inspect the elev tab act support fitting for accidental damage.

8000 FH 8000 FH 36213.6 44213.6 6973.2

5554-323-01I Inspect vert stab finger plate interface angles for cracks.Special NDT

30000 FL 12000 FL 29963 41963 623

5554-323-02I Inspect vert stab rear spar fuselage interface fitting for cracks.Special NDT

30000 FL 12000 FL 29963 41963 623

5554-323-03I Inspect vert stab front spar fuselage interface fitting for cracks.Special NDT

30000 FL 12000 FL 29963 41963 623

5555-323-01E Inspect the vert stabilizer, lower rudder hinge fitting assy andattaching structure for cracks.

30000 FL 12000 FL 29963 41963 623

5555-323-02E Inspect the vert stabilizer, upper rudder hinge fitting assy andattaching structure for cracks.

30000 FL 12000 FL 29963 41963 623

5555-323-03E Inspect the vert stabilizer, upper rudder triangular hinge andattaching structure for cracks.

30000 FL 12000 FL 29963 41963 623

5555-324-01E Inspect the lower rudder hinge fitting and attaching structure forcracks.

30000 FL 12000 FL 29963 41963 623

5555-324-02E Inspect the upper rudder hinge fitting and attaching structure forcracks.

30000 FL 12000 FL 29963 41963 623

5555-325-01I Inspect rudder nose rib for cracks. Detailed A/C 004-369premod 2569

800 FH 800 FH na by mod N/A #VALUE!

3000 FH or 3000 FH or 35001.2 38001.2 760.818 M 18 M 02/2004 08/2005

5610-210-02E Inspect outer frames, front and side windshields for cracks. 4000 FH 4000 FH 33157.8 37157.8 -82.6

1 Y or 1 Y or 04/18/2004 04/18/20052500 FH 2500 FH 35447.4 37947.4 707

5711-501-01E5711-601-01E Inspect rear spar web splice at W.S. 21.15, fastener holes

common to web and spar cap for cracks. Special detailed NDTA/C 004-078

30000 FL 12000 FL 29963 41963 623

5711-501-01I5711-601-01I Inspect front spar web splice at W.S. 21.15, fastener holes

common to lower spar cap and splice plate for cracks. Specialdetailed NDT A/C 004-078

30000 FL 12000 FL 29963 41963 623

5610-210-01E Inspect front and side windshield for cracks, scratches andchipping, and inspect windshield moisture seals.

5610-210-03E Inspect cabin windows for cracks. NOTE: Interval wichever isreached first.

5711-501-02E5711-601-02E Inspect rear spar web splice at W.S. 164, fastener holes

common to web and spar cap for cracks. Special detailed NDTA/C 079 & up.

30000 FL 12000 FL N/A BY S/N N/A BY S/N #VALUE!

5711-501-02I5711-601-02I Inspect lower forward splice fitting BL 0.0 for cracks. Special

NDT

30000 FL 12000 FL 29963 41963 623

5711-501-03I5711-601-03I Inspect lower mid splice fitting at BL 0.0 for cracks. Special

NDT

30000 FL 12000 FL 29963 41963 623

5711-501-04I5711-601-04I Inspect lower aft splice fitting at BL 0.0 for cracks. Special NDT

30000 FL 12000 FL 29963 41963 623

5711-501-05I5711-601-05I Inspect lower forward cap splice angle fittings for cracks.

30000 FL 12000 FL 29963 41963 623

5711-501-06I5711-601-06I Inspect lower aft cap splice fittings for cracks.

30000 FL 12000 FL 29963 41963 623

5711-501-07I5711-601-07I Inspect lower stringer splice fittings for cracks.

30000 FL 12000 FL 29963 41963 623

5711-501-08I5711-601-08I Inspect front spar web splice at WS 158 at fasteners holes

common to lower spar cap and splice plate for cracks. Specialdetailed NDT A/C 079 & up.

30000 FL 12000 FL N/A BY S/N N/A BY S/N #VALUE!

5711-501-80I5711-601-80I Inspect machined rib at BL 0.0 for corrosion.

6 Y 4 Y 06/2004 06/2008

5711-521-80I5711-621-80I Inspect upper spar cap inboard of WS 132 for corrosion.

6 Y 4 Y 06/2004 06/2008

5711-522-80I5711-622-80I Inspect machined ribs at BL 120 and BL 144 for corrosion.

6 Y 4 Y 06/2004 06/2008

5711-523-01I5711-623-01I Inspect lower front spar section at skin inboard of WS 297 for

cracks.

30000 FL 12000 FL 29963 41963 623

5711-523-80I5711-623-80I Inspect upper spar cap outboard of WS 132 for corrosion.

6 Y 4 Y 06/2004 06/2008

5711-523-81I5711-623-81I Inspect lower front spar cap inboard of WS 297 for corrosion.

6 Y 4 Y 06/2004 06/2008

5711-524-80I5711-624-80I Inspect lower front spar cap outboard of WS 297 for corrosion.

6 Y 4 Y 06/2004 06/2008

5711-531-01I5711-631-01I Inspect lower rear spar section at skin, web and spar cap for

cracks.

30000 FL 12000 FL 29963 41963 623

5711-531-80I5711-631-80I Inspect lower rear spar cap for corrosion.

6 Y 4 Y 06/2004 06/2008

5723-523-01E5723-524-01E Inspect aileron coves for delamination of the anti-static

aluminium foil. Detailed Eff. A/C 004-260 pre mod sb51-012 alt2

800 FH 800 FH na by sb na #VALUE!

5732-520-01E5732-620-01E Inspect lower skin at rib stations WS 42 and WS 210 at

fastener holes for cracks.

30000 FL 12000 FL 29963 41963 623

5732-521-80E5732-621-80E5732-523-80E5732-623-80E5732-524-80E5732-624-80E Inspect complete lower skin along the stringers from BL 0 to

WS 415.2 for corrosion. Detailed Eff. A/C 182, A/C 186 LH,A/C 198 LH, A/C 203 LH, A/C 206 LH, A/C 210 LH, A/C 212LH, A/C 214 LH

6 Y 4 Y N/A BY S/N N/A BY S/N

5732-521-80I5732-621-80I5732-523-80I5732-623-80I

5732-524-80I5732-624-80I Inspect complete lower skin around and between stringers from

BL 0 to WS 415.2 for corrosion. Detailed Eff. A/C 182, A/C 186LH, A/C 198 LH, A/C 203 LH, A/C 206 LH, A/C 210 LH, A/C212 LH, A/C 214 LH

6 Y 4 Y N/A BY S/N N/A BY S/N

5732-522-01IInspect lower skin and stringer plugs in nacelle area for cracks.Special NDT A/C 012

5000 FH 11000 FL N/A BY S/N N/A BY S/N

5732-523-01IInspect lower skin and stringer plugs in fuel tank area forcracks. Special Detailed NDT A/C 027

5000 FH 19000 FL N/A BY S/N N/A BY S/N

5741-501-01I5741-601-01I Inspect inboard forward wing attach fitting at lug area for

cracks.

30000 FL 12000 FL 29963 41963 623

5741-501-02I5741-601-02I Inspect outboard forward wing attach fitting at lug area for

cracks.

30000 FL 12000 FL 29963 41963 623

5741-501-03I5741-601-03I Inspect inboard rear wing attach fitting at lug area for cracks.

30000 FL 12000 FL 29963 41963 623

5741-501-04I5741-601-04I Inspect outboard rear wing attach fitting at lug area for cracks.

30000 FL 12000 FL 29963 41963 623

5741-501-80I5741-601-80I Inspect drag support assy for corrosion.

6 Y 4 Y 06/2004 06/2008

5742-524-01E5742-624-01E Inspect inboard aileron hinge strap support and fitting at attach


30000 FL 12000 FL 29963 41963 623

5742-524-02E5742-624-02E Inspect outboard aileron hinge support strap and fittings at

attach structure for cracks.

30000 FL 12000 FL 29963 41963 623

5742-524-80E5742-624-80E Inspect inboard aileron hinge support and fitting for corrosion.

6 Y 4 Y 06/2004 06/2008

5742-524-81E5742-624-81E Inspect outboard aileron hinge support and fitting for corrosion.

6 Y 4 Y 06/2004 06/2008

5744-457-01E5744-467-01E Inspect MLG drag brace support fitting for accidental damage.

Detailed

4000 FH 4000 FH 33157.8 37157.8 -82.6

5744-457-02E5744-467-02E Inspect MLG trunnion fitting for accidental damage. Detailed

4000 FH 4000 FH 33157.8 37157.8 -82.6

5744-457-03E5744-467-03E Inspect MLG trunnion link fittings for accidental damage.

Detailed

4000 FH 4000 FH 33157.8 37157.8 -82.6

5744-457-04E5744-467-04E Inspect torque of MLG supports attach bolts. NOTE: One-time

inspection. 340A

25000 FL N/A NA

5744-457-05E5744-467-05E Inspect torque of MLG supports attach bolts. NOTE: One-time

inspection. 340B

12000 FL N/A N/A N/A #VALUE!

5752-541-01E5752-641-01E Inspect flap upper skin for cracks. Detailed

16000 FL 6000 FL 35938 41938 598

5752-541-01I5752-641-01I Inspect flap forward and rear spar assy at skin, spar and rib

sections for cracks. Detailed

16000 FL 6000 FL 35938 41938 598

5752-541-02E5752-641-02E Inspect flap lower skin for cracks. Detailed

16000 FL 6000 FL 35938 41938 598

250001QS insulation blankets inspection 12000 FL 12000 FL 29963 41963 623

CWA 5-18-0336069 TAS

InitialInspection

(hrs)

Reinspection

(hrs)

Last Done

(hrs)

Due Next

(hrs)

Remaining

(hrs)

ZONE 100 - LOWER HALF OF FUSELAGE (below cabin floor)

0600-100-02E General visual inspection 4000 FH 4000 FH 33158.7 37158.7 -81.7

ZONE 111 - RADOME

0600-111-01I General visual inspection 4000 FH 4000 FH 33158.7 37158.7 -81.7

ZONE 112 - NOSE GEAR WELL

0600-112-01E General visual inspection 800 FH 800 FH 36431.7 37231.7 -8.7 AB ODD

ZONE 113/114 - HYDRAULIC COMPARTMENT LH/RH

0600-113-01I0600-114-01I

General visual inspection 800 FH 800 FH 36926.9 37626.9 386.5AB EVEN

ZONE 115/116 - FWD FLIGHT DECK UNDERFLOOR LH/RH

0600-115-01I0600-116-01I

General visual inspection 4000 FH 4000 FH 33158.7 37158.7 -81.7

0600-115-02I0600-116-02I

General visual inspection 6 Ys 4 Ys 06/2004 06/2008

ZONE 117/118 - REAR FLIGHT DECK UNDERFLOOR LH/RH

0600-117-01I0600-118-01I


0600-117-02I0600-118-02I

General visual inspection 6 Ys 4 Ys 06/2004 06/2008

ZONE 121/122 - FORWARD CABIN UNDERFLOOR - FWD LH/RH

ZONAL INSPECTIONS

Zone TitleTask Description

0600-121-01I0600-122-01I


0600-121-02I0600-122-02I

General visual inspectionNOTE: If galley or forward toilet isinstalled.

4 Y 2Y 06/2004 06/2006

0600-121-03I0600-122-03I

General visual inspectionNOTE: If galley or forward toilet is notinstalled.

6 Ys 4 Ys 06/2004 06/2008

ZONE 131/132 - FORWARD CABIN UNDERFLOOR - MID LH/RH

0600-131-01I0600-132-01I


0600-131-02I0600-132-02I

General visual inspection 6Y 4Y 06/2004 06/2008 2359.6

ZONE 141/142 - FORWARD CABIN UNDERFLOOR - REAR LH/RH

0600-141-01I0600-142-01I


0600-141-02I0600-142-02I

General visual inspection 6 Y 4 Y 06/2004 06/2008


0600-143-01I0600-144-01I


0600-143-02I0600-144-02I



0600-145-01I0600-146-01I


0600-145-02I0600-146-02I


ZONE 151/152 - MID CABIN UNDERFLOOR LH/RH

0600-151-01I0600-152-01I


0600-151-02I0600-152-02I


ZONE 161/162 - REAR CABIN UNDERFLOOR - FWD LH/RH

0600-161-01I0600-162-01I


0600-161-02I0600-162-02I


ZONE 163/164 - REAR CABIN UNDERFLOOR - FWD LH/RH

0600-163-01I0600-164-01I


0600-163-02I0600-164-02I


ZONE 171/172 - REAR CABIN UNDERFLOOR - REAR LH/RH

0600-171-01I0600-172-01I


0600-171-02I0600-172-02I


ZONE 173/174 - REAR CABIN UNDERFLOOR - REAR LH/RH

0600-173-01I0600-174-01I


0600-173-02I0600-174-02I

General visual inspectionNOTE: If rear toilet is installed.

4 Y 2 Y 06/2004 06/2006

0600-173-03I0600-174-03I

General visual inspectionNOTE: If rear toilet is not installed.

6 Y 4 Y NA NA

ZONE 181/182 - CARGO COMPARTMENT UNDERFLOOR - FWD LH/RH

0600-181-01I0600-182-01I


0600-181-02I0600-182-02I


ZONE 183/184 - CARGO COMPARTMENT UNDERFLOOR - REAR LH/RH

0600-183-01I0600-184-01I


0600-183-02I0600-184-02I


ZONE 191/192 - AREA IN WING FAIRING

0600-191-01I0600-192-01I

General visual inspection 6Y 4 Y 06/2004 06/2008

ZONE 193/194 - AREA IN WING FAIRING (ECS COMPARTMENT)

0600-193-01I0600-194-01I


0600-193-03I0600-194-03I


ZONE 195/196 - AREA IN WING FAIRING (BATTERY AND ELECTRIC COMP)

0600-195-01I0600-196-01I


0600-195-02I0600-196-02I


ZONE 197/198 - AREA IN HYDRAULIC TUBING FAIRING LH/RH

0600-197-01I0600-198-01I


ZONE 200 - UPPER HALF OF FUSELAGE


ZONE 210 - FLIGHT COMPARTMENT


0600-210-02I General visual inspection 6 Y 4 Y 06/2004 06/2008

ZONE 221 - AVIONICS RACK

0600-221-01I General visual inspection 8000 FH 8000 FH 36213.6 44213.6 6973.2


ZONE 222 - FWD CABIN RH



ZONE 223 - GALLEY AND AIRSTAIR STOWAGE AREA



ZONE 225 - FWD ENTRANCE AREA



ZONE 226 - FWD TOILET AREA (if installed)


ZONE 231/232 - FWD CABIN LH/RH

0600-231-01I0600-232-01I


0600-231-80I0600-232-80I


ZONE 241/242 - CENTER CABIN LH/RH

0600-241-01I0600-242-01I


0600-241-02I0600-242-02I


ZONE 251/252 - CENTER CABIN LH/RH

0600-251-01I0600-252-01I


0600-251-02I0600-252-02I


ZONE 261/262 - AFT CABIN LH/RH

0600-261-01I0600-262-01I


0600-261-80I0600-262-80I


ZONE 271/272 - CARGO COMPARTMENT LH/RH

0600-271-01I0600-272-01I


0600-271-02I0600-272-02I


ZONE 274 - REAR TOILET AREA (if installed)



ZONE 300 - EMPENNAGE AND FUSELAGE TAIL SECTION FROM AFT FACE OF CARGO COMPARTMENT

ZONE 311/312 - FWD SECTION OF FUSELAGE TAIL LH/RH

0600-311-01I0600-312-01I


ZONE 313/314 - HORIZONTAL AND VERTICAL STABILIZER ATTACHMENT AREA ABOVE WL 110

0600-313-01I0600-314-01I


ZONE 315/316 - HORIZONTAL AND VERTICAL STABILIZER ATTACHMENT AREA BELOW WL 110

0600-315-01I0600-316-01I


ZONE 317/318 - AFT SECTION OF FUSELAGE TAIL AND FWD FACE OF PRESSURE BULKHEAD

0600-317-01I0600-318-01I


ZONE 319 - AFT FACE OF PRESSURE BULKHEAD AND TAIL CAP


ZONE 321 - DORSAL FIN

0600-321-01I General visual inspection 6Y 4 Y 06/2004 06/2008

ZONE 322 - VERTICAL STABILIZER LEADING EDGE


ZONE 323 - VERTICAL STAB FRONT SPAR TO REAR SPAR


ZONE 324 - RUDDER LEADING EDGE



ZONE 325 - RUDDER

0600-325-01I General visual inspection 4Y 2Y 06/2004 06/2006 1628.6


ZONE 331/341 - HORIZONTAL STABILIZER LEADING EDGE

0600-331-01I0600-341-01I


ZONE 332/342 - HORIZONTAL STABILIZER FRONT TO REAR SPAR

0600-332-01I0600-342-01I


ZONE 333/343 - ELEVATOR LEADING EDGE

0600-333-01I0600-343-01I


ZONE 334/344 - ELEVATOR

0600-334-01I0600-344-01I


ZONE 336/346 - HORIZONTAL STABILIZER TIP

0600-336-01I0600-346-01I


ZONE 430/440 - POWERPLANT

0600-430-01E0600-440-01E


ZONE 450/460 - NACELLE

0600-450-01E0600-460-01E


ZONE 452/462 - INLET COMPARTMENT

0600-452-01I0600-462-01I

General visual inspection 4000 FH 4000 FH 32535.4 37535.4 295

ZONE 453/463 - NACELLE/POWERPLANT

0600-453-01I0600-463-01I


0600-453-03I0600-463-03I

General visual inspection 8000 FH 8000 FH 36213.6 44213.6 6973.2

ZONE 454/464 - EXHAUST PIPE / SHROUD ASSY

0600-454-01E0600-464-01E


0600-454-01I0600-464-01I

General visual inspection."Firewall shiels" Insti-Nac STA 281 to324.

8000 FH 8000 FH 36213.6 44213.6 6973.2

ZONE 455/465 - NACELLE EQUIPMENT COMPARTMENT

0600-455-01I0600-465-01I


ZONE 456/466 - LOWER NACELLE

0600-456-01I0600-466-01I


ZONE 457/467 - LOWER NACELLE / WHEEL WELL

0600-457-01I0600-467-01I


ZONE 458/468 - LOWER NACELLE AFT OF MAIN WHEEL WELL

0600-458-01I0600-468-01I


ZONE 500/600 - LEFT AND RIGHT WING

0600-500-01E0600-600-01E

General visual inspection 800 FH 800 FH 36431.7 37231.7 -8.7AB ODD

0600-500-01I0600-600-01I


ZONE 501/601 - WING FWD SPAR TO REAR SPAR

0600-501-01I0600-601-01I


ZONE 511/611 - WING LEADING EDGE

0600-511-01I0600-611-01I

General visual inspection 9000 FH 9000 FH 36213.6 44213.6 6973.2


0600-512-01I0600-612-01I



0600-513-01I0600-613-01I


ZONE 514/614 - WING LEADING EDGE-EXTENDED WING TIP

0600-514-01I0600-614-01I


ZONE 521/621 - WING FORWARD SPAR TO REAR SPAR

0600-521-01I0600-621-01I

General visual inspection.NOTE: Operational check of low levelfloat switch is to be performed at thistime (Ref.: TASK NO 284101)

6 Y 4 Y 06/2004 06/2008

ZONE 522/622 - WING FORWARD SPAR TO REAR SPAR AT THE NACELLE

0600-522-01I0600-622-01I



0600-523-01I0600-623-01I



0600-524-01I0600-624-01I


ZONE 525/625 - EXTENDED WING TIP

0600-525-01I0600-625-01I


ZONE 531/631 - REAR SPAR TO FLAP COVE TRAILING EDGE

0600-531-01I0600-631-01I


ZONE 541/641 - FLAP ASSY LEADING EDGE TO TRAILING EDGE

0600-541-01E0600-641-01E


0600-541-01I0600-641-01I


ZONE 551/651 - AILERON ASSY LEADING EDGE TO TRAILING EDGE

0600-551-01I0600-651-01I


0600-551-80I0600-651-80I


ZONE 552/652 - AILERON TRIM TAB ASSEMBLY

0600-552-01I0600-652-01I


ZONE 561/661 - WING TIP

0600-561-01I0600-661-01I


ZONE 710 - NOSE LANDING GEAR AND DOORS

0600-710-01E General visual inspection 800 FH 800 FH 36431.7 37231.7 -8.7 AB ODD

ZONE 732/742 - MAIN LANDING GEAR

0600-732-01I0600-742-01I


ZONE 811 - PILOT ESCAPE HATCH



ZONE 813 - ENTRANCE DOOR


ZONE 814 - EMERGENCY EXIT DOOR TYPE II



ZONE 815/816 - EMERGENCY EXIT DOOR TYPE III

0600-815-01E0600-816-01E


0600-815-01I0600-816-01I


ZONE 817 - CARGO DOOR

0600-817-01E General visual inspection 800 FH 800 FH 36926.9 37626.9 386.5 AB EVEN


Fig & Item Description Intervals Last Done Due Next Remaining

AD1-00126-001R1 inspection and exchange of the left and right nacelle fire extinghising

manifolds. Visual: do the inspection of manifold P/N 7226263-535every 100FH until replaced with manifold P/N 7226263-540MOD1052

100FH SB26-001R1 CW at DEL NA

30-015R1 installation of the heater blanket for the tail de-icer valve with periodicchecks. Do the periodic check every 100 FH during icing conditionoperations until further notice EFF 003 to 041, 044 and 047. MOD1334

100FH N/a by S/N N/A

32-019R1 nose gear- insp/replacement of retract actuator pin EFF ALL.MOD1301

daily until AIR127300 isembodied

refer gear rec NA by PN refer CMM

32A-025 insp.and functional test of connectors and wiring of emergencyextension explosive bolt EFF. 003-007. Compliance with both SB`s 32-038 and 32-041 supersedes this SB

N/A by SN term

32-059 LG- insp check and renewing of MLG strut and DB outboard trunionbearing. EFF All strut 83022-5 to -12 and DB 84310/11-2 to -4installed. Note: 32-060 supersedes 32-059

first conv. And repeat atB check interval

VCW gear records Term

32-089 nose and MLG drag brace- new method of locking microswitchadjuster.EFF 004-159 certain PN and SN, same for -160 and up

within 200FL and everyC check after

Status board

AD1-06132-094R2 MLG/NLG shock strut- MLG retract actuator bracket retaining bolt

failures MOD 2481- Do the inspection during the landing gearoverhaul after initial short term action MOD 2481

gear overhaul CW SB32-094R2 TAS 419.022 TERM

AD1-075R132-105 brakes- inspection of the brake stack for damaged carbon and

installation of the torque tube heat shield EFF-004-346every 225FH after initialuntil 32-106 is actioned

CW SB 105,106 TAS 419.023 TERM

AD1-03151-006 inspection of composite structure do the inspection after heavy

landings until the repair/ replacement procedures are actioned EFF.103 thru 139

N/A by S/N N/A

REPETITIVE INSPECTION

AD1-060RA51-012 inspection of the elevator and aileron coves if temp repair option was

chosen, every 800FHuntil the permanentsolution is actioned

CW SB51-12 EXP346129 TERM

AD1-049RA54-027R3 inspection of the lower drag strut assembly EFF 004-260 if the detailed insp. Is not

actioned do the 1500FH,do the 300FH continue

until 22000FH

CW SB54-027 EAL 338394 TERM

55-002 inspection of migrating lower hinge bushing. EFF 001-031 evry 200 hr up to1000hrs

NA BY SN

55-004R2 insp. Repair/reinforcement of rudder LE nose rib.EFF 001 to 038.MOD 1320

initial LC2 with crackevery 100 FH. Repairwithin 500 hrs. Withoutcrack every 100FH to

1000FH

NA BY SN

55-006R1 inspection and repair of rudder stop. EFF 004-078. repair of 55-007or 55-030 removes need inspection.MOD1356

within 100FH. Every 500FH thereafter

55A-011R1 inspection of vertical stabilizer top closure rib. EFF 031-120 55-012eliminates this inspection

if crack and al tape,check tape every 100FH,

if not cracked repeatevery 500FH until MOD

is performed

NA SB 55-012 CW exp 98028 17 june 92

AD1-036RA55-022R1 vert. stab- re-inspection of the top closure rib EFF 031-194 if cracked every 100FH,

if no cracks every50FH,continue until SB55-023

is actioned

CW 55-023 EAL29716 TERM

AD1-074

55-032R1 rudder inspection and reinforcement of the nose rib EFF 004-369MOD 2569

when no cracks or minorand stopped drilled doevery 800FH until nose

rib is replaced/reinforced

CW55-032 EAL 13644 TERM

AD1-110R255-033R4 hor-stab inspection of holes EFF 004-439 for A/C004-159 do the

NDT every 12000flights,for A/C 160-439 do NDT

every 6000 flights

SUP BY 1-133 CW EAL 02/01 TERM

AD1-07257-027R1 flaps- inspection and mod of flap fittings at WS 123.38 EFF 004-379

MOD 2628if no cracks do every

800FHCWSB027 EAL 570099 TERM

AD1-15257-035 flaps- isnp. And replacement of bolt and bushing EFF 004-459 in cracks every 800FH CW57-034 TAS419.066 TERM

AD1-15357-037 flaps- insp. Of the aft attach lug on fitting WS123.38 EFF 004-459

Visual every 800FH until NDT is actioned; NDT every 6000FL until 57-038 actioned.

800FH na ndt done #VALUE!

6000FL 38819 44819 4815AD1-064R161-032R1 ops test of prop brake valve limit switch EFF004 and up every 100FH until SB61-

033 actionedBRAKE DEACTIVATED TERM

71-008R2 insp of engine vibration isolators and replacement of fwd, bottomvibrator isolator. EFF. All A/C with PN 93948-37, -38, -39, -41installed. MOD1113

PN -41 every 500 FHand eng chg, -37, -38

every 1000FH and engchg, -39 replace molded

assy 00-12193 every1000FH

41 INST MRB INSP ON STATUS

AD1-135R171-057R2 Engine mounts-inspection of the bottom bolts every 250FH if the

conditions of the SB para. 2B apply250FH CW at TAS N/A by S/N TERM

AD1-01474-002 R1 intro of a new switch allowing continuous ignition and periodic

inspections MOD1365 A/C003 to 048 MOD1365LC2 N/A by S/N N/A

AD1-024RB76-024R2 insp of PCU control cable between HMU and PCU EFF all 340A with

power control cable P/N C82146-1 and/or -2if no axial play do every200FH until final mod of

the power control

CW76A024R2 TAS419.015 TERM

AD1-14376-043R1 control quadrant- insp of flight idle stop solenoid bracket screw

EFF004-459CW76-043 TAS419.067 TERM

006-10-99 NDT on propeller hub assemblies with more than 7500hrs as perSB340-61-95R4

LH prop 1200FH 36563.2 37763.2 522.8RH prop 1200FH 37180.1 38380.1 1139.7

TECHNICAL DATA Aircraft Type : Saab 340 Effective Date : · PDF file ·...

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