operator make & model serial no date hours landings · item no ata/ad/sb description part no /...

193
Complete Tracked Items Operator Make & Model Serial No Date Hours Landings Component Make & Model Serial No Hours Cycles ENGINE 1 ENGINE 2 APU 1 N80EJ 29-JAN-2015 1146.70 953 PW617F-E 1146.70 1146.70 0.00 953 953 0 PCE-LC0108 PCE-LC0111 PW617F-E GOLD AVIATION SERVICES 1420 LEE WAGNER BLVD FT LAUDERDALE, FL 33315 UNITED STATES 954-359-8999 EMBRAER EMB 500 50000056 Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time At Inst Next Due Installed Remaining Adjustment Items Copyright © Flightdocs, Inc. All Rights Reserved. 600 FH MAINTENANCE PACKAGE 5 30-01 600HR AIRFRAME 1 14-SEP-2014 H: 1038.80 L: 883 H: 600.00 H: +/-30 H: 1638.80 H: 492.10 AMM 05-30-01 600 FH/12 MO MAINTENANCE PACKAGE 5 30-02 600HR/12MO AIRFRAME 2 14-SEP-2014 H: 1038.80 L: 883 M: 12 H: 600.00 D: +/-30 H: +/-30 14-SEP-2015 H: 1638.80 M: 7 D: 11 H: 492.10 AMM 05-30-02 1200 FH MAINTENANCE PACKAGE 5 30-10 1200HR AIRFRAME 3 14-AUG-2009 H: 1200.00 H: +/-30 H: 1200.00 H: 53.30 AMM 05-30-10 1200 FH/24 MO MAINTENANCE PACKAGE 5 30-12 1200HR/24MO AIRFRAME 4 12-SEP-2013 H: 786.90 L: 722 M: 24 H: 1200.00 D: +/-30 H: +/-30 12-SEP-2015 H: 1986.90 M: 7 D: 9 H: 840.20 AMM 05-30-12 1800 FH MAINTENANCE PACKAGE 5 30-20 1800HR AIRFRAME 5 14-AUG-2009 H: 1800.00 H: +/-30 H: 1800.00 H: 653.30 AMM 05-30-20 3000 FH MAINTENANCE PACKAGE 5 30-40 3000HR AIRFRAME 7 14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30 AMM 05-30-40 Page 1 of 193 PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Page 1: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Complete Tracked Items

Operator Make & Model Serial No Date Hours Landings

Component Make & Model Serial No Hours CyclesENGINE 1ENGINE 2APU 1

N80EJ

29-JAN-2015 1146.70 953

PW617F-E 1146.701146.700.00

9539530

PCE-LC0108PCE-LC0111PW617F-E

GOLD AVIATION SERVICES1420 LEE WAGNER BLVDFT LAUDERDALE, FL 33315UNITED STATES954-359-8999

EMBRAER EMB 500 50000056

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

600 FH MAINTENANCE PACKAGE5 30-01600HRAIRFRAME1

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

AMM 05-30-01

600 FH/12 MO MAINTENANCE PACKAGE5 30-02600HR/12MOAIRFRAME2

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 05-30-02

1200 FH MAINTENANCE PACKAGE5 30-101200HRAIRFRAME3

14-AUG-2009 H: 1200.00 H: +/-30 H: 1200.00 H: 53.30

AMM 05-30-10

1200 FH/24 MO MAINTENANCE PACKAGE5 30-121200HR/24MOAIRFRAME4

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

AMM 05-30-12

1800 FH MAINTENANCE PACKAGE5 30-201800HRAIRFRAME5

14-AUG-2009 H: 1800.00 H: +/-30 H: 1800.00 H: 653.30

AMM 05-30-20

3000 FH MAINTENANCE PACKAGE5 30-403000HRAIRFRAME7

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 05-30-40

Page 1 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 2: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

3000 FH/48 MO MAINTENANCE PACKAGE5 30-41300HR/48MOAIRFRAME8

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 05-30-41

4800 FH/72 MO MAINTENANCE PACKAGE5 30-464800HR/72MOAIRFRAME11

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 05-30-46

6000 FH MAINTENANCE PACKAGE5 30-506000HRAIRFRAME13

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 05-30-50

6000 FH/96 MO MAINTENANCE PACKAGE5 30-536000HR/96MOAIRFRAME14

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 05-30-53

7800 FH MAINTENANCE PACKAGE5 30-607800HRAIRFRAME15

14-AUG-2009 H: 7800.00 H: +/-30 H: 7800.00 H: 6653.30

AMM 05-30-60

12000 FH/120 MOS MAINTENANCE PACKAGE5 30-6612000H/120MAIRFRAME16

14-AUG-2009 M: 120H:12000.00

D: +/-30H: +/-30

14-AUG-2019H: 12000.00

M: 54 D: 11H: 10853.30

AMM 05-30-66

12 MO MAINTENANCE PACKAGE5 30-8012MOAIRFRAME17

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 05-30-80

24 MO MAINTENANCE PACKAGE5 30-8124MOAIRFRAME18

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 05-30-81

48 MO MAINTENANCE PACKAGE5 30-8348MOAIRFRAME19

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

AMM 05-30-83

60 MO MAINTENANCE PACKAGE5 30-8460MOAIRFRAME20

14-SEP-2014H: 1038.80L: 883

M: 60 D: +/-30 14-SEP-2019 M: 55 D: 11

AMM 05-30-84

Page 2 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 3: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

72 MO MAINTENANCE PACKAGE5 30-8572MOAIRFRAME21

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

AMM 05-30-85

96 MO MAINTENANCE PACKAGE5 30-8696MOAIRFRAME22

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

AMM 05-30-86

GENERAL VISUAL INSPECTION OF INTERFACE CONNECTORSON THE FORWARD FUSELAGE COCKPIT SECTION

5 H05-01-120-0014800HR/72MOAIRFRAME23

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACE CONNECTORSON THE CENTER FUSELAGE FRONT SECTION

5 H05-02-130-0014800HR/72MOAIRFRAME24

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACECONNECTORS/ OVERBRAIDS ON THE CENTER FUSELAGEBOTTOM REAR SECTION

5 H05-03-140-0014800HR/72MOAIRFRAME25

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACE CONNECTORSON THE CENTER FUSELAGE REAR SECTION

5 H05-04-190-0014800HR/72MOAIRFRAME26

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACECONNECTORS/ OVERBRAIDS ON THE FORWARD FUSELAGENOSE SECTION

5 H05-05-210-0014800HR/72MOAIRFRAME27

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACECONNECTORS/ OVERBRAIDS ON THE CENTER FUSELAGE TOPREAR SECTION

5 H05-06-240-0014800HR/72MOAIRFRAME28

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACE CONNECTORSON THE AFT FUSELAGE REAR SECTION

5 H05-07-320-0014800HR/72MOAIRFRAME29

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

GENERAL VISUAL INSPECTION OF INTERFACE CONNECTORSON THE PYLON

5 H05-08-410-0014800HR/72MOAIRFRAME30

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 05-46-00

PERFORM WEIGHT AND BALANCE CHECK (FAR 91.423 OR135.185)

8 8-0001-1 FAR

AIRFRAME31

26-FEB-2013H: 684.70L: 651

M: 36 26-FEB-2016 M: 12 D: 23

ELECTROMECHANICAL LINEAR ACTUATOR21 00-00

AIRFRAME32

14-AUG-2009 H: 0

100000-77 24689

Page 3 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 4: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

PRESSURIZATION AND AIR CONDITIONING CONTROL PANEL21 01-01

AIRFRAME33

14-AUG-2009 H: 0

441-40931-002 0074

LEFT REAR FUS FLOW CONTROL SHUT OFF VALVE ASSEMBLY21 21-01

AIRFRAME34

10-FEB-2010 H: 0

1300230-15 336

RIGHT REAR FUS FLOW CONTROL SHUT OFF VALVEASSEMBLY

21 21-01

AIRFRAME35

10-FEB-2010 H: 0

1300230-25 332

LH AFT INLET AIR CHECK VALVE21 21-02

AIRFRAME36

14-AUG-2009 H: 0

PN SN-UNKNOWN

RH AFT INLET AIR CHECK VALVE21 21-02

AIRFRAME37

14-AUG-2009 H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK LH AFT INLET AIR CHECK VALVE21 21-02-0016000HRAIRFRAME38

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 21-21-02

OPERATIONAL CHECK RH AFT INLET AIR CHECK VALVE21 21-02-0016000HRAIRFRAME39

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 21-21-02

RAM AIR VALVE21 23-03

AIRFRAME40

14-AUG-2009 H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK OF RAM AIR VALVE POSITION21 23-03-0026000HRAIRFRAME41

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 21-23-03

OPERATIONAL CHECK OF RAM AIR VALVE ACTUATION21 23-03-003 OPC600HRAIRFRAME2005

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: 30 H: 1638.80 H: 492.10

AMM 21-23-03-710-802-A/500

LH AFT FUSELAGE RAM AIR CHECK VALVE21 23-04

AIRFRAME42

14-AUG-2009 H: 0

PN SN-UNKNOWN

Page 4 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 5: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LH CENTER FUSELAGE RAM AIR CHECK VALVE21 23-04

AIRFRAME43

14-AUG-2009 H: 0

PN SN-UNKNOWN

RH AFT FUSELAGE RAM AIR CHECK VALVE21 23-04

AIRFRAME44

14-AUG-2009 H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK LH AFT FUSELAGE RAM AIR CHECKVALVE

21 23-04-0016000HRAIRFRAME45

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 21-23-04

OPERATIONAL CHECK LH CENTER FUSELAGE RAM AIR CHECKVALVE

21 23-04-0016000HRAIRFRAME46

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 21-23-04

OPERATIONAL CHECK RH AFT FUSELAGE RAM AIR CHECKVALVE

21 23-04-0016000HRAIRFRAME47

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 21-23-04

TAIL CONE GROUND BLOWER (COOLING FAN) ASSEMBLY21 23-05

AIRFRAME48

27-APR-2011H: 409.30L: 435

H: 0

1133710-5 322

GENERAL VISUAL INSPECTION TAIL CONE GROUND BLOWER(COOLING FAN) ASSEMBLY

21 23-05-0011200HRAIRFRAME49

14-AUG-2009 H: 1200.00 H: +/-30 H: 1200.00 H: 53.30

1133710-5 322 AMM 21-23-05

OPERATIONAL CHECK AFT BULKHEAD OUTFLOW (OFV)VALVE MANUAL PRESSURIZATION CONTROL MODE

21 31-00-002600HRAIRFRAME50

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

PN SN-UNKNOWN AMM 21-31-00

OPERATIONAL CHECK OF EMERGENCY CABINDECOMPRESSION (AUTO MODE)

21 31-00-003600HRAIRFRAME51

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

AMM 21-31-00

ELECTRONIC CONTROL AND MONITORING UNIT21 31-01

AIRFRAME52

13-SEP-2011H: 504.20L: 504

H: 0

2119286-4 2119286-00504

Page 5 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 6: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

RESTORE ELECTRONIC CONTROL AND MONITORING UNIT21 31-01-001

AIRFRAME53

13-SEP-2011H: 504.20L: 504

H: 4800.00 H: +/-30 H: 0 H: 5304.20 H: 4157.50

2119286-4 2119286-00504 AMM 21-31-01

AFT BULKHEAD OUTFLOW (OFV) VALVE21 31-02

AIRFRAME54

14-AUG-2009 H: 0

PN SN-UNKNOWN

RESTORE AFT BULKHEAD OUTFLOW (OFV) VALVE21 31-02-001

AIRFRAME55

14-AUG-2009 H: 4800.00 H: +/-30 H: 0 H: 4800.00 H: 3653.30

PN SN-UNKNOWN AMM 21-31-02

NEGATIVE PRESSURE RELIEF VALVE21 31-03

AIRFRAME56

14-AUG-2009 H: 0

130664-2 34163-0110

OPERATIONAL CHECK NEGATIVE PRESSURE RELIEF VALVE21 31-03-0016000HRAIRFRAME57

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

130664-2 34163-0110 AMM 21-31-03

AFT BULKHEAD PRESSURE RELIEF (PRV) VALVE21 31-04

AIRFRAME58

14-AUG-2009 H: 0

103916-2 103916-00082

FUNCTIONAL CHECK AFT BULKHEAD PRESSURE RELIEF(PRV) VALVE

21 31-04-0016000HRAIRFRAME59

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

103916-2 103916-00082 AMM 21-31-04

COMPRESSOR DRIVE MODULE CONTROLLER21 52-00

AIRFRAME60

13-SEP-2011H: 504.20L: 504

H: 0

1240240-306 576

VCS COMPRESSOR DRIVE MODULE21 52-01

AIRFRAME61

13-SEP-2011H: 504.20L: 504

H: 0

1133630-9 419

DETAILED VISUAL INSPECTION VCS COMPRESSOR DRIVEMODULE OF VCS COMPRESSOR MOTOR DRIVE

21 52-01-001600HR/12MOAIRFRAME62

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

1133630-9 419 AMM 21-52-01

Page 6 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 7: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

DISCARD VCS COMPRESSOR DRIVE MODULE BELT21 52-01-0021200HR/24MOAIRFRAME63

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

M: 0H: 0

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

1133636-2 N/A AMM 21-52-01

FUNCTIONAL CHECK VCS COMPRESSOR DRIVE MODULE BELT TENSION

21 52-01-003600HR/12MOAIRFRAME64

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

1133630-9 419 AMM 21-52-01

HEAT EXCHANGER PACK21 52-02

AIRFRAME65

14-AUG-2009 H: 0

1133750-3 153

GENERAL VISUAL INSPECTION HEAT EXCHANGER PACK21 52-02-0011200HRAIRFRAME66

14-AUG-2009 H: 1200.00 H: +/-30 H: 1200.00 H: 53.30

1133750-3 153 AMM 21-52-02

HEAT EXCHANGER RECEIVER21 52-02-701

AIRFRAME67

13-SEP-2011H: 504.20L: 504

H: 0

1134275-12 8004152740

GENERAL VISUAL INSPECTION OF EVAPORATOR MODULES21 52-03-001600HRAIRFRAME68

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

AMM 21-52-03

FWD FUS VCS SYSTEM FWD EVAPORATOR BLOWER21 52-04

AIRFRAME69

14-AUG-2009 H: 0

1133850-104 165

SERVICING OF VCS REFRIGERANT FLUID21 52-06-001600HR/12MOAIRFRAME70

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-17-00

OPERATIONAL CHECK OF MANUAL TEMPERATURE CONTROLSYSTEM

21 61-00-001600HRAIRFRAME71

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

AMM 21-61-00

REAR FUS ECS TEMPERATURE CONTROLLER21 61-01

AIRFRAME72

26-MAR-2012H: 587.40L: 584

H: 0

1300650-12 577

Page 7 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 8: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

COCKPIT DUCT TEMPERATURE SENSOR SWITCH21 61-03

AIRFRAME73

14-AUG-2009 H: 0

1300450-10 273

LH REAR DUCT TEMPERATURE SENSOR SWITCH21 61-03

AIRFRAME74

14-AUG-2009 H: 0

1300450-10 355

PAX DUCT TEMPERATURE SENSOR SWITCH21 61-03

AIRFRAME75

14-AUG-2009 H: 0

1300450-10 398

RH REAR DUCT TEMPERATURE SENSOR SWITCH21 61-03

AIRFRAME76

14-AUG-2009 H: 0

1300450-10 604

OPERATIONAL CHECK OF E-BAY OVERTEMPERATURE SENSOR21 61-06-0016000HRAIRFRAME77

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 21-61-06

FUNCTIONAL CHECK AILERON GSA 81 LOW TORQUEAUTOPILOT SERVO ACTUATOR

22 11-00-001 AIRWORTHINESS

AIRFRAME78

14-SEP-2014H: 1038.80L: 883

M: 12 14-SEP-2015 M: 7 D: 11

011-00878-10 71306360 AMM 22-11-00

FUNCTIONAL CHECK ELEVATOR GSA 81 LOW TORQUEAUTOPILOT SERVO ACTUATOR

22 11-00-001 AIRWORTHINESS

AIRFRAME79

14-SEP-2014H: 1038.80L: 883

M: 12 14-SEP-2015 M: 7 D: 11

011-00878-10 71306501 AMM 22-11-00

FUNCTIONAL CHECK RUDDER GSA 81 LOW TORQUEAUTOPILOT SERVO ACTUATOR

22 11-00-001 AIRWORTHINESS

AIRFRAME80

14-SEP-2014H: 1038.80L: 883

M: 12 14-SEP-2015 M: 7 D: 11

011-00878-10 71306561 AMM 22-11-00

LUBRICATION OF SERVO ACTUATORS22 11-00-0021200HR/24MOAIRFRAME81

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

AMM 22-11-00

DETAILED VISUAL INSPECTION OF AUTOPILOT SERVOCABLE

22 11-00-0033000HRAIRFRAME82

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 22-11-00

GMC 715 GUIDANCE PANEL22 11-01

AIRFRAME83

14-AUG-2009 H: 0

011-01430-00 15900202

Page 8 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 9: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

AILERON GSA 81 LOW TORQUE AUTOPILOT SERVO ACTUATOR22 11-02

AIRFRAME84

14-AUG-2009 H: 0

011-00878-10 71306360

AILERON GSM 85A MED TORQUE SERVO MOUNT22 11-03

AIRFRAME85

14-AUG-2009 H: 0

011-01436-01 22305235

FUNCTIONAL CHECK AILERON GSA 81 LOW TORQUEAUTOPILOT SERVO ACTUATOR CABLE

22 11-04-001

AIRFRAME1872

14-SEP-2014H: 1038.80L: 883

H: 3000.00 H: 4038.80 H: 2892.10

011-00878-10 71306360 AMM 22-11-04

ELEVATOR GSA 81 LOW TORQUE AUTOPILOT SERVOACTUATOR

22 11-05

AIRFRAME86

14-AUG-2009 H: 0

011-00878-10 71306501

ELEVATOR GSM 85A MED TORQUE SERVO MOUNT22 11-06

AIRFRAME87

14-AUG-2009 H: 0

011-01436-01 22305243

FUNCTIONAL CHECK ELEVATOR GSA 81 LOW TORQUEAUTOPILOT SERVO ACTUATOR CABLE

22 11-07-001

AIRFRAME1873

14-SEP-2014H: 1038.80L: 883

H: 3000.00 H: 4038.80 H: 2892.10

011-00878-10 71306501 AMM 22-11-07

RUDDER GSA 81 LOW TORQUE AUTOPILOT SERVO ACTUATOR22 11-08

AIRFRAME88

14-AUG-2009 H: 0

011-00878-10 71306561

RUDDER GSM 85A MED TORQUE SERVO MOUNT22 11-09

AIRFRAME89

14-AUG-2009 H: 0

011-01436-01 22305256

FUNCTIONAL CHECK RUDDER GSA 81 LOW TORQUEAUTOPILOT SERVO ACTUATOR CABLE

22 11-10-001

AIRFRAME1874

14-SEP-2014H: 1038.80L: 883

H: 3000.00 H: 4038.80 H: 2892.10

011-00878-10 71306561 AMM 22-11-10

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE AUTOPILOT SERVOS

22H22-01-321-001 4800HR/72MO

AIRFRAME90

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 22-11-00

BOTTOM VHF ANTENNA23 12-02

AIRFRAME91

14-AUG-2009 H: 0

S65-8280-41 322-1988

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

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Items

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TOP VHF ANTENNA23 12-02

AIRFRAME92

14-AUG-2009 H: 0

S65-8280-41 322-1879

IRIDIUM ANTENNA23 15-03

AIRFRAME93

14-AUG-2009 H: 0

PN SN-UNKNOWN

WIFI - DATALINK ANTENNA23 23-03

AIRFRAME94

14-AUG-2009 H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK OF AIRBORNE AUDIO SYSTEMFAIL-SAFE MODE

23 51-00-0013000HRAIRFRAME95

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 23-51-00

COPILOT GMA 1347D AUDIO PANEL23 51-01

AIRFRAME96

14-AUG-2009 H: 0

011-01257-20 17105693

PILOT GMA 1347D AUDIO PANEL23 51-01

AIRFRAME97

14-AUG-2009 H: 0

011-01257-20 17100715

LH AUDIO JACK CONTROL PANEL23 51-05

AIRFRAME98

14-AUG-2009 H: 0

441-40943-002 0165

RH AUDIO JACK CONTROL PANEL23 51-05

AIRFRAME99

14-AUG-2009 H: 0

441-40943-002 0168

LH MODEL HME 25-KA-2 HEADSET23 51-09

AIRFRAME100

14-AUG-2009 H: 0

025-250-015 002989

RH MODEL HME 25-KA-2 HEADSET23 51-09

AIRFRAME101

14-AUG-2009 H: 0

025-250-015 003001

COCKPIT ELECTRODYNAMIC MICROPHONE23 51-11

AIRFRAME102

14-AUG-2009 H: 0

85-03-12369-04 199625

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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FUNCTIONAL CHECK OF STATIC DISCHARGERS23 61-00-00148MOAIRFRAME103

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

AMM 23-61-00

RELAY ASSEMBLY24 00-07

AIRFRAME104

14-AUG-2009 H: 0

PN SN-UNKNOWN

ELECTRICAL CONTROL PANEL24 01-01

AIRFRAME105

14-AUG-2009 H: 0

441-40929-002 0077

NO.1 28V, 325A -DC STARTER-GENERATOR24 31-01

AIRFRAME106

27-APR-2011H: 409.30L: 435

H: 0

MG94F-1 503

NO.2 28V, 325A -DC STARTER-GENERATOR24 31-01

AIRFRAME107

27-APR-2011H: 409.30L: 435

H: 0

MG94F-1 557

RESTORATION OF LEFT STARTER GENERATOR (OVERHAUL)24 31-01-001 N/A

AIRFRAME108

H: +/-30 H: 0

MG94F-1 503 AMM 24-31-01Notes: N/A BY P/N INSTALLED.

RESTORATION OF RIGHT STARTER GENERATOR(OVERHAUL)

24 31-01-001 N/A

AIRFRAME109

H: +/-30 H: 0

MG94F-1 557 AMM 24-31-01Notes: N/A BY P/N INSTALLED.

DETAILED INSPECTION NO.1 28V, 325A -DCSTARTER-GENERATOR BRUSHES

24 31-01-002 N/A

AIRFRAME110

H: +/-30

MG94F-1 503 AMM 24-31-01Notes: N/A BY P/N INSTALLED.

DETAILED INSPECTION NO.2 28V, 325A -DCSTARTER-GENERATOR BRUSHES

24 31-01-002 N/A

AIRFRAME111

H: +/-30

MG94F-1 557 AMM 24-31-01Notes: N/A BY P/N INSTALLED.

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

RESTORATION OF LEFT STARTER GENERATOR (OVERHAUL)24 31-01-003 OVERHAUL

AIRFRAME2019

27-APR-2011H: 409.30L: 435

H: 600.00 H: 30 H: 0 14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

MG94F-10 503 AMM 24-31-01-920-801-A/200

RESTORATION OF RIGHT STARTER GENERATOR(OVERHAUL)

24 31-01-003 OVERHAUL

AIRFRAME2020

27-APR-2011H: 409.30L: 435

H: 600.00 H: 30 H: 0 14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

MG94F-10 557 AMM 24-31-01-920-801-A/200

DETAILED DIMENSIONAL INSPECTION OF STARTER LEFTGENERATOR

24 31-01-004 DET

AIRFRAME2021

14-SEP-2014H: 1038.80L: 883

H: 300.00 H: 30 H: 1338.80 H: 192.10

AMM 24-31-01-220-801-A/600

DETAILED DIMENSIONAL INSPECTION OF STARTER RIGHTGENERATOR

24 31-01-004 DET

AIRFRAME2022

14-SEP-2014H: 1038.80L: 883

H: 300.00 H: 30 H: 1338.80 H: 192.10

AMM 24-31-01-220-801-A/600

NO.1 GENERATOR - DC, 28V CONTROL UNIT24 31-02

AIRFRAME112

14-AUG-2009 H: 0

CG301A-10 273

NO.2 GENERATOR - DC, 28V CONTROL UNIT24 31-02

AIRFRAME113

14-AUG-2009 H: 0

CG301A-10 274

NO. 2 ENGINE START CONTACTOR24 31-04

AIRFRAME114

10-FEB-2012H: 575.60L: 570

H: 0

SM400D117 5596

NO.1 MAIN BATTERY24 36-01

AIRFRAME115

13-SEP-2011H: 504.20L: 504

H: 0

7639-27 G02670171

NO.2 MAIN BATTERY24 36-01

AIRFRAME116

13-SEP-2011H: 504.20L: 504

H: 0

7639-27 G02670170

Page 12 of 193

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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FUNCTIONAL CHECK NO.1 MAIN BATTERY NOTE: INTERVALBASED ON INSTALLATION DATE

24 36-01-001

AIRFRAME117

14-SEP-2014H: 1038.80L: 883

M: 6H: 300.00

D: +/-30 14-MAR-2015H: 1338.80

M: 1 D: 11H: 192.10

7639-27 G02670171 AMM 24-36-01

FUNCTIONAL CHECK NO.2 MAIN BATTERY NOTE: INTERVALBASED ON INSTALLATION DATE

24 36-01-001

AIRFRAME118

14-SEP-2014H: 1038.80L: 883

M: 6H: 300.00

D: +/-30 14-MAR-2015H: 1338.80

M: 1 D: 11H: 192.10

7639-27 G02670170 AMM 24-36-01

NO.1 MAIN BATTERY24 36-01-002

AIRFRAME119

12-SEP-2013H: 786.90L: 722

H: 0

7639-27 G02777363 AMM 24-36-01

NO.2 MAIN BATTERY24 36-01-002

AIRFRAME120

12-SEP-2013H: 786.90L: 722

H: 0

7639-27 G02777364 AMM 24-36-01

BATTERY CURRENT (HB2) SENSOR24 36-02

AIRFRAME121

14-AUG-2009 H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK BATTERY CURRENT (HB2) SENSOR24 36-02-0016000HRAIRFRAME122

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 24-36-02

28 VDC / 115 VAC STATIC INVERTER24 54-05

AIRFRAME123

14-AUG-2009 H: 0

AS-24-0026-001 0083

CABLE W109 LPDU/RPDU FEEDER24 65-00

AIRFRAME124

14-AUG-2009 H: 0

PN SN-UNKNOWN

LEFT POWER DISTRIBUTION UNIT ASSEMBLY24 65-01

AIRFRAME125

20-SEP-2012H: 662.00L: 637

H: 0

SX7EG16-1 0034

RIGHT POWER DISTRIBUTION UNIT ASSEMBLY24 65-02

AIRFRAME126

20-SEP-2012H: 662.00L: 637

H: 0

SX7EG17-1 0092

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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CENTER POWER DISTRIBUTION UNIT ASSEMBLY24 65-03

AIRFRAME127

20-SEP-2012H: 662.00L: 637

M: 21H: 345.7L: 276

SX7EG18-1 0223

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE GCUS

24H24-01-240-001 6000HR/96MO

AIRFRAME128

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 24-31-02

DETAILED VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE GENERATORS

24H24-02-433-001 4800HR/72MO

AIRFRAME129

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 24-31-01

COPILOT CITRINE FINISH GOODRICH SEAT25 11-01

AIRFRAME130

14-AUG-2009 H: 0

1429-621AN 659-1429

PILOT CITRINE FINISH GOODRICH SEAT25 11-01

AIRFRAME131

14-AUG-2009 H: 0

1429-521AN 481-1429

DETAILED VISUAL INSPECTION COPILOT CITRINE FINISHGOODRICH SEAT

25 11-01-001300HR/48MOAIRFRAME132

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

1429-621AN 659-1429 AMM 25-11-01

DETAILED VISUAL INSPECTION PILOT CITRINE FINISHGOODRICH SEAT

25 11-01-001300HR/48MOAIRFRAME133

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

1429-521AN 481-1429 AMM 25-11-01

DETAILED VISUAL INSPECTION OF COCKPIT SEAT BELTS25 11-01-002300HR/48MOAIRFRAME134

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 25-11-01

LH AFT PAX SEAT25 21-01

AIRFRAME135

14-SEP-2010H: 260.50L: 312

H: 0

403176-1AD 48400

LH FWD PAX SEAT25 21-01

AIRFRAME136

14-SEP-2010H: 260.50L: 312

H: 0

403176-3AD 48402

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

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Items

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RH AFT PAX SEAT25 21-01

AIRFRAME137

14-SEP-2010H: 260.50L: 312

H: 0

403176-4AD 48403

RH FWD PAX SEAT25 21-01

AIRFRAME138

14-SEP-2010H: 260.50L: 312

H: 0

403176-2AD 48401

DETAILED VISUAL INSPECTION RH FWD PAX SEAT25 21-01-001300HR/48MOAIRFRAME142

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

403176-2AD 48401 AMM 25-21-01

DETAILED VISUAL INSPECTION LH FWD PAX SEAT25 21-01-001300HR/48MOAIRFRAME140

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

403176-3AD 48402 AMM 25-21-01

DETAILED VISUAL INSPECTION RH AFT PAX SEAT25 21-01-001300HR/48MOAIRFRAME141

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

403176-4AD 48403 AMM 25-21-01

DETAILED VISUAL INSPECTION LH AFT PAX SEAT25 21-01-001300HR/48MOAIRFRAME139

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

403176-1AD 48400 AMM 25-21-01

DETAILED VISUAL INSPECTION OF PASSENGER SEATBELTS

25 21-01-002300HR/48MOAIRFRAME143

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 25-21-01

DEATILED INSPECTION OF FIFTH SEAT (NOTE:AIRCRAFT WITH FIFTH SEAT INSTALLED.)

25 21-03-001 N/A

AIRFRAME144

14-AUG-2009

AMM 25-21-01

DEATILED INSPECTION OF THE FIFTH SEAT BELT(NOTE:AIRCRAFT WITH FIFTH SEAT INSTALLED.)

25 21-03-002 N/A

AIRFRAME145

14-AUG-2009

AMM 25-21-03

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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DETAILED VISUAL INSPECTION OF BELTED TOILET UNIT(NOTE: AIRCRAFT WITH BELTED TOILET UNITINSTALLED)

25 43-01-001300HR/48MOAIRFRAME146

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 25-43-02

DETAILED VISUAL INSPECTION OF BELTED TOILET SEATBELT (NOTE: AIRCRAFT WITH BELTED TOILET UNITINSTALLED)

25 43-01-002300HR/48MOAIRFRAME147

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 25-43-02

OPERATIONAL CHECK EMERGENCY LOCATOR TRANSMITTER SYSTEM

25 61-00-001

AIRFRAME148

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

S1821502-02 2620858-0028 AMM 25-61-00

GENERAL VISUAL INSPECTION EMERGENCY LOCATORTRANSMITTER FOR CONDITION: PROPER INSTALLATIONAND BATTERY CORROSION/ LEAKAGE

25 61-00-002

AIRFRAME149

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

S1821502-02 2620858-0028 AMM 25-61-00

EMERGENCY LOCATOR TRANSMITTER25 61-01

AIRFRAME150

26-FEB-2013H: 684.70L: 651

M: 42H: 684.7L: 651

S1821502-02 2620858-0028

EMERGENCY LOCATOR TRANSMITTER BATTERY25 61-02

AIRFRAME151

14-AUG-2009 H: 0

S1820506-01 SN-UNKNOWN

ELT ANTENNA25 61-03

AIRFRAME152

14-AUG-2009 H: 0

S65-8282-406 401-1353

DISCARD EMERGENCY LOCATOR TRANSMITTER BATTERY25 61-04-001

AIRFRAME153

M: 72 D: +/-30 M: 0 30-JUN-2015 M: 4 D: 27

S1820506-01 SN-UNKNOWN AMM 25-61-04

ELT/NAV INTERFACE - CS144-A MODULE25 61-05

AIRFRAME154

14-AUG-2009 H: 0

PN SN-UNKNOWN

FIRST AID KIT25 62-01

AIRFRAME155

16-SEP-2010H: 260.50L: 312

H: 0

S06-01-0005-312 SN-UNKNOWN

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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VISUAL CHECK FIRST AID KIT25 62-01-001

AIRFRAME156

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

S06-01-0005-312 SN-UNKNOWN AMM 25-62-01

DISCARD OF CREW 1 LIFE VEST25 62-02-003 DIS

AIRFRAME162

14-AUG-2009 M: 120 N/A M: 0 01-NOV-2017 M: 32 D: 29

66601-505 L132171 AMM 25-62-02-960-801-A/200

DISCARD OF CREW 2 LIFE VEST25 62-02-003 DIS

AIRFRAME157

14-AUG-2009 M: 120 N/A M: 0 01-NOV-2017 M: 32 D: 29

66601-505 L132198 AMM 25-62-02-960-801-A/200

DISCARD OF PASSENGER 1 LIFE VEST25 62-02-003 DIS

AIRFRAME158

14-AUG-2009 M: 120 N/A M: 0 01-MAY-2019 M: 50 D: 28

66601-105 L1238249 AMM 25-62-02-960-801-A/200

DISCARD OF PASSENGER 2 LIFE VEST25 62-02-003 DIS

AIRFRAME159

14-AUG-2009 M: 120 N/A M: 0 01-MAY-2019 M: 50 D: 28

66601-105 L1238247 AMM 25-62-02-960-801-A/200

DISCARD OF PASSENGER 3 LIFE VEST25 62-02-003 DIS

AIRFRAME160

14-AUG-2009 M: 120 N/A M: 0 01-MAY-2019 M: 50 D: 28

66601-105 L1238250 AMM 25-62-02-960-801-A/200

DISCARD OF PASSENGER 4 LIFE VEST25 62-02-003 DIS

AIRFRAME161

14-AUG-2009 M: 120 N/A M: 0 01-MAY-2019 M: 50 D: 28

66601-105 L1238251 AMM 25-62-02-960-801-A/200

LAV WATER BARRIER25 62-04

AIRFRAME169

14-AUG-2009 H: 0

PN SN-UNKNOWN

DETAILED DIMENSIONAL INSPECTION LAV WATER BARRIER25 62-04-00124MOAIRFRAME170

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

PN SN-UNKNOWN AMM 25-62-04

LIFE RAFT:NOT FITTED25 66-00

AIRFRAME171

H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK EMERGENCY LOCATOR TRANSMITTER (FAR 91.207)

25 FAR01 FAR

AIRFRAME172

14-SEP-2014H: 1038.80L: 883

M: 12 14-SEP-2015 M: 7 D: 11

S1821502-02 2620858-0028 FAR 91.207

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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LH ENGINE FIRE DETECTOR26 11-01

AIRFRAME173

14-AUG-2009 H: 0

3951-49-565/211C-3.7 42216

RH ENGINE FIRE DETECTOR26 11-01

AIRFRAME174

14-AUG-2009 H: 0

3951-49-565/211C-3.7 42224

DETAILED VISUAL INSPECTION LH ENGINE FIRE DETECTOR26 11-01-0011200HRAIRFRAME175

14-AUG-2009 H: 1200.00 H: +/-30 H: 1200.00 H: 53.30

3951-49-565/211C-3.7 42216 AMM 26-11-01

DETAILED VISUAL INSPECTION RH ENGINE FIRE DETECTOR26 11-01-0011200HRAIRFRAME176

14-AUG-2009 H: 1200.00 H: +/-30 H: 1200.00 H: 53.30

3951-49-565/211C-3.7 42224 AMM 26-11-01

OPERATIONAL CHECK LH ENGINE FIRE DETECTOR26 11-01-002 AIRWORTHINESS

AIRFRAME177

14-AUG-2009 H: 1200.00 H: 1200.00 H: 53.30

3951-49-565/211C-3.7 42216 AMM 26-11-01

OPERATIONAL CHECK RH ENGINE FIRE DETECTOR26 11-01-002 AIRWORTHINESS

AIRFRAME178

14-AUG-2009 H: 1200.00 H: 1200.00 H: 53.30

3951-49-565/211C-3.7 42224 AMM 26-11-01

FIRE/ENGINE START STOP/IGNITION/TRIM CONTROL PANEL26 21-01

AIRFRAME179

25-JUN-2010H: 186.70L: 213

H: 0

441-42702-002 0093

FUNCTIONAL CHECK FIRE/ENGINE STARTSTOP/IGNITION/TRIM CONTROL PANEL FIREXPANEL/SYSTEM

26 21-01-001 AIRWORTHINESS

AIRFRAME180

14-AUG-2009 H: 2400.00 H: 2400.00 H: 1253.30

441-42702-002 0093 AMM 26-21-00

ENGINE FIRE EXTINGUISHING BOTTLE26 21-03

AIRFRAME181

31-JAN-2009 H: 0

33000073-4 53035A1

HYDROSTATIC TEST ENGINE FIRE EXTINGUISHING BOTTLE26 21-03-001 AIRWORTHINESS

AIRFRAME182

31-JAN-2009 M: 120 31-JAN-2019 M: 47 D: 28

33000073-4 53035A1 AMM 26-21-03

OPERATIONAL CHECK OF TEMPERATURE COMPENSATEDPRESSURE SWITCH (TCPS)

26 21-05-001 AIRWORTHINESS

AIRFRAME183

14-AUG-2009 H: 2400.00 H: 2400.00 H: 1253.30

AMM 26-21-05

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

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Items

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LEFT ENG FIREX CARTRIDGE26 21-07

AIRFRAME184

31-JAN-2009 H: 0

30903962-1 0813JJ

RIGHT ENG FIREX CARTRIDGE26 21-07

AIRFRAME185

31-JAN-2009 H: 0

30903963-1 0789JM

DISCARD LEFT ENG FIREX CARTRIDGE26 21-07-001 LIFE LIMIT

AIRFRAME186

31-JAN-2009 M: 120 M: 0 31-JAN-2019 M: 47 D: 28

30903962-1 0813JJ AMM 26-21-07

DISCARD RIGHT ENG FIREX CARTRIDGE26 21-07-001 LIFE LIMIT

AIRFRAME187

31-JAN-2009 M: 120 M: 0 31-JAN-2019 M: 47 D: 28

30903963-1 0789JM AMM 26-21-07

DETAILED VISUAL INSPECTION OF ENGINE FIREEXTINGUISHING DISCHARGE PIPING

26 21-09-0011800HRAIRFRAME188

14-AUG-2009 H: 1800.00 H: +/-30 H: 1800.00 H: 653.30

AMM 26-21-09

COCKPIT PORTABLE EXTINGUISHER26 24-01

AIRFRAME189

14-AUG-2009 M: 4

RT-A1200 S739169

WEIGHT CHECK COCKPIT PORTABLE EXTINGUISHER26 24-01-001

AIRFRAME190

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

RT-A1200 S739169 AMM 26-24-01

DISCARD COCKPIT PORTABLE EXTINGUISHER26 24-01-002

AIRFRAME191

30-APR-2009 M: 144 D: +/-30 M: 0 30-APR-2021 M: 74 D: 27

RT-A1200 S739169 AMM 26-24-01

DISCARD OF PORTABLE FIRE EXTINGUISHER26 24-01-003

AIRFRAME1924

30-APR-2009 M: 120 D: 30 M: 0 30-APR-2019 M: 50 D: 27

BA51015G-3 AMM 26-24-01-960-801-A/200

LEFT FLAP ACTUATOR27 001 LIFE LIMIT

AIRFRAME192

14-AUG-2009 H:10500.00

H: 0 H: 10500.00 H: 9353.30

6094A0001-03 0316

RIGHT FLAP ACTUATOR27 001 LIFE LIMIT

AIRFRAME193

14-AUG-2009 H:10500.00

H: 0 H: 10500.00 H: 9353.30

6094A0001-03 0320

Page 19 of 193

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ROLL TRIM ACTUATOR27 002 LIFE LIMIT

AIRFRAME194

14-AUG-2009 H:35000.00

H: 0 H: 35000.00 H: 33853.30

452900-1007 0067

YAW TRIM ACTUATOR27 003 LIFE LIMIT

AIRFRAME195

14-AUG-2009 H:35000.00

H: 0 H: 35000.00 H: 33853.30

453000-1007 0072

LEFT PITCH TRIM ACTUATOR27 004 LIFE LIMIT

AIRFRAME196

14-AUG-2009 H: 3200.00 H: 0 H: 3200.00 H: 2053.30

453100-1009 0012

RIGHT PITCH TRIM ACTUATOR27 004 LIFE LIMIT

AIRFRAME197

14-AUG-2009 H: 3200.00 H: 0 H: 3200.00 H: 2053.30

453100-1009 0149

GROUND SPOILER ACTUATOR27 005 LIFE LIMIT

AIRFRAME198

14-AUG-2009 H: 1750.00 H: 0 H: 1750.00 H: 603.30

PN SN-UNKNOWN

PITCH TRIM ACTUATOR.27 008 LIFE LIMIT

AIRFRAME1919

H:35000.00

H: 0 H: 35000.00 H: 33853.30

453100-9009

LEFT FLAP ACTUATOR27 009 LIFE LIMIT

AIRFRAME1964

H:10750.00

H: 0 H: 10750.00 H: 9603.30

6094A0001-06

RIGHT FLAP ACTUATOR27 009 LIFE LIMIT

AIRFRAME1965

H:10750.00

H: 0 H: 10750.00 H: 9603.30

6094A0001-06

LEFT FLAP ACTUATOR27 010 LIFE LIMIT

AIRFRAME1966

H:10750.00

H: 0 H: 10750.00 H: 9603.30

6094A0001-08

RIGHT FLAP ACTUATOR27 010 LIFE LIMIT

AIRFRAME1967

H:10750.00

H: 0 H: 10750.00 H: 9603.30

6094A0001-08

LEFT CONTROL YOKE27 01-01

AIRFRAME199

13-SEP-2011H: 504.20L: 504

H: 0

83912139 00561

Page 20 of 193

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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RIGHT CONTROL YOKE27 01-01

AIRFRAME200

13-SEP-2011H: 504.20L: 504

H: 0

83912140 00564

LH PEDAL ASSEMBLY27 01-02

AIRFRAME201

14-AUG-2009 H: 0

500-15010-411 0000501977

LUBRICATION OF ROTARY BALL SPLINE27 01-03-00124MOAIRFRAME202

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 12-21-00

NO.1 TRIM ACTUATOR CONTROLLER27 04-01

AIRFRAME203

13-SEP-2011H: 504.20L: 504

M: 176

461600-1007 0453

NO.2 TRIM ACTUATOR CONTROLLER27 04-01

AIRFRAME204

13-SEP-2011H: 504.20L: 504

M: 176

461600-1007 0497

FUNCTIONAL CHECK OF TRIM ACTUATION TIME LIMITER27 04-01-0016000HRAIRFRAME205

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 27-04-01

FUNCTIONAL CHECK OF TRIM TABS ELECTRICAL STOP27 04-01-0026000HRAIRFRAME206

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 27-04-01

OPERATIONAL CHECK OF TRIM TAB JAM MONITORINGFUNCTION

27 04-01-0036000HRAIRFRAME207

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

GENERAL VISUAL INSPECTION OF AILERON ACTUATINGSYSTEM MECHANICAL COMPONENTS

27 11-00-0013000HRAIRFRAME208

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 27-11-00

LH AILERON BALANCED ASSEMBLY27 11-01

AIRFRAME209

14-AUG-2009 H: 0

500-14650-407 0000508371

RH AILERON BALANCED ASSEMBLY27 11-01

AIRFRAME210

14-AUG-2009 H: 0

500-14651-403 0000506157

Page 21 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

FUNCTIONAL CHECK OF AILERON CONTROL CABLESTENSION

27 11-02-0013000HRAIRFRAME211

26-MAR-2012H: 587.40L: 584

H: 3000.00 H: +/-30 H: 3587.40 H: 2440.70

AMM 27-11-02

DETAILED VISUAL INSPECTION OF AILERON CONTROLCABLES

27 11-02-0023000HRAIRFRAME212

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 27-11-02

FUNCTIONAL CHECK ROLL TRIM ACTUATOR AILERON TRIMBACKLASH/ INTEGRITY

27 14-02-001 AIRWORTHINESS

AIRFRAME213

14-AUG-2009 H: 6000.00 H: 6000.00 H: 4853.30

452900-1007 0067 AMM 27-14-03

LEFT AILERON TRIM TAB27 14-03

AIRFRAME214

14-AUG-2009 H: 0

500-14630-403 0000500742

GENERAL VISUAL INSPECTION OF RUDDER ACTUATINGSYSTEM MECHANICAL COMPONENTS

27 21-00-0013000HRAIRFRAME215

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 27-21-00

RUDDER BALANCED ASSEMBLY27 21-01

AIRFRAME216

14-AUG-2009 H: 0

500-10520-411 0000508752

FUNCTIONAL CHECK OF RUDDER CONTROL CABLES TENSION27 21-02-0013000HRAIRFRAME217

26-MAR-2012H: 587.40L: 584

H: 3000.00 H: +/-30 H: 3587.40 H: 2440.70

AMM 27-21-02

DETAILED VISUAL INSPECTION OF RUDDER CONTROLCABLES

27 21-02-0023000HRAIRFRAME218

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 27-21-02

FUNCTIONAL CHECK YAW TRIM ACTUATOR RUDDER TRIMBACKLASH INTEGRITY

27 24-02-001 AIRWORTHINESS

AIRFRAME219

14-AUG-2009 H: 6000.00 H: 6000.00 H: 4853.30

453000-1007 0072 AMM 27-24-03

TAB RUDDER27 24-03

AIRFRAME220

14-AUG-2009 H: 0

500-10420-407 0000501712

GENERAL VISUAL INSPECTION OF ELEVATOR ACTUATINGSYSTEM MECHANICAL COMPONENTS

27 31-00-0013000HRAIRFRAME221

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 27-31-00

Page 22 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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LEFT ELEVATOR27 31-01

AIRFRAME222

14-AUG-2009 H: 0

500-11085-4001 0000500721

RIGHT ELEVATOR27 31-01

AIRFRAME223

14-AUG-2009 H: 0

500-11085-4002 0000500710

FUNCTIONAL CHECK OF ELEVATOR CONTROL CABLESTENSION

27 31-02-0013000HRAIRFRAME224

26-MAR-2012H: 587.40L: 584

H: 3000.00 H: +/-30 H: 3587.40 H: 2440.70

AMM 27-31-02

DETAILED VISUAL INSPECTION OF ELEVATOR CONTROLCABLES

27 31-02-0023000HRAIRFRAME225

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 27-31-02

FUNCTIONAL CHECK OF PITCH TRIM BACKLASH/INTEGRITY

27 34-02-001 AIRWORTHINESS

AIRFRAME226

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 27-34-05

PITCH TRIM INTERCONNECTION ACTUATOR27 34-04

AIRFRAME227

14-AUG-2009 H: 0

453110-1001 0181

LEFT ELEVATOR TRIM TAB27 34-05

AIRFRAME228

14-AUG-2009 H: 0

500-11010-4001 0000501725

RIGHT ELEVATOR TRIM TAB27 34-05

AIRFRAME229

14-AUG-2009 H: 0

500-11010-4002 0000501627

LEFT ANGLE-OF-ATTACK SENSOR27 36-01

AIRFRAME230

13-SEP-2011H: 504.20L: 504

H: 0

C100117-3 296

RIGHT ANGLE-OF-ATTACK SENSOR27 36-01

AIRFRAME231

13-SEP-2011H: 504.20L: 504

H: 0

C100117-3 446

Page 23 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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OPERATIONAL CHECK OF ANGLE-OF-ATTACK (AOA)SENSOR

27 36-01-001600HR/12MOAIRFRAME232

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 27-36-01

STICK PUSHER LINEAR ACTUATOR27 36-02

AIRFRAME233

14-AUG-2009 H: 0

260926258-0101 169

OPERATIONAL CHECK OF SPWS CUTOUT SWITCH27 36-03-0011200HR/24MOAIRFRAME234

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

AMM 27-36-03

STALL WARNING AND PROTECTION COMPUTER27 36-04

AIRFRAME235

14-AUG-2009 H: 0

C-100106-2 206

LUBRICATION OF FLAP ACTUATORS BALL SCREWS27 51-01-00112MOAIRFRAME236

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 12-21-00

DETAILED VISUAL INSPECTION LEFT FLAP ACTUATOR27 51-01-0026000HRAIRFRAME237

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

6094A0001-03 0316 AMM 27-51-01

DETAILED VISUAL INSPECTION RIGHT FLAP ACTUATOR27 51-01-0026000HRAIRFRAME238

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

6094A0001-03 0320 AMM 27-51-01

RESTORE LEFT FLAP ACTUATOR27 51-01-003

AIRFRAME1875

14-AUG-2009 H: 3600.00 H: +/-30 H: 3600.00 H: 2453.30

AMM 27-51-01Notes: NEW REQUIREMENT ADDED ON 18-MAR-2013. REVIEW BASE TIMES TO ENSURE CORRECT DUE TIMES.

RESTORE RIGHT FLAP ACTUATOR27 51-01-003

AIRFRAME1876

14-AUG-2009 H: 3600.00 H: +/-30 H: 0 H: 3600.00 H: 2453.30

AMM 27-51-01Notes: NEW REQUIREMENT ADDED ON 18-MAR-2013. REVIEW BASE TIMES TO ENSURE CORRECT DUE TIMES.

LH WING FLAP27 51-03

AIRFRAME239

14-AUG-2009 H: 0

500-14301-403 0000504288

Page 24 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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RH WING FLAP27 51-03

AIRFRAME240

14-AUG-2009 H: 0

500-14301-404 0000500015

FLAP SELECTOR LEVER27 53-01

AIRFRAME241

25-JUN-2010H: 186.70L: 213

H: 0

780501-9 1052

FLAP SYSTEM CONTROL UNIT27 53-02

AIRFRAME242

14-SEP-2010H: 260.50L: 312

H: 0

8025A0001-08 0197

LH WING FLAP POSITION SENSOR UNIT27 53-03

AIRFRAME243

14-AUG-2009 H: 0

7906A0001-01 KA1213

RH WING FLAP POSITION SENSOR UNIT27 53-03

AIRFRAME244

14-AUG-2009 H: 0

7906A0001-01 KA1222

OPERATIONAL CHECK OF GROUND SPOILER SYSTEM27 60-00-001 AIRWORTHINESS

AIRFRAME245

14-AUG-2009 H: 6000.00 H: 6000.00 H: 4853.30

AMM 27-60-00

DETAILED VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE FLAP SYSTEM CONTROL UNIT

27H27-01-240-001 6000HR/96MO

AIRFRAME246

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 27-53-02

DETAILED VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE FLAP LINEAR ACTUATOR

27H27-02-571-001 4800HR/72MO

AIRFRAME247

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-51-01

DETAILED VISUAL INSPECTION RIGHT L/HIRFPROTECTION ON THE FLAP LINEAR ACTUATOR

27H27-02-571-001 4800HR/72MO

AIRFRAME248

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-51-01

DETAILED VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE FLAP SENSOR POSITION UNIT

27H27-03-571-001 4800HR/72MO

AIRFRAME249

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-53-03

DETAILED VISUAL INSPECTION RIGHT L/HIRFPROTECTION ON THE FLAP SENSOR POSITION UNIT

27H27-03-571-001 4800HR/72MO

AIRFRAME250

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-53-03

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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DETAILED VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE FLAP SELECTOR LEVER

27H27-04-220-001 4800HR/72MO

AIRFRAME251

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-53-01

DETAILED VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE TRIM ACTUATOR CONTROLLER

27H27-05-310-001 6000HR/96MO

AIRFRAME252

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 27-04-01

DETAILED VISUAL INSPECTION RIGHT L/HIRFPROTECTION ON THE TRIM ACTUATOR CONTROLLER

27H27-05-310-001 6000HR/96MO

AIRFRAME253

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 27-04-01

DETAILED VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE ROLL TRIM ACTUATOR

27H27-06-572-001 4800HR/72MO

AIRFRAME254

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-14-02

DETAILED VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE YAW TRIM ACTUATOR

27H27-07-330-001 4800HR/72MO

AIRFRAME255

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-24-02

DETAILED VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE PITCH TRIM ACTUATOR

27H27-08-340-001 4800HR/72MO

AIRFRAME256

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-34-02

DETAILED VISUAL INSPECTION RIGHT L/HIRFPROTECTION ON THE PITCH TRIM ACTUATOR

27H27-08-340-001 4800HR/72MO

AIRFRAME257

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 27-34-02

FUNCTIONAL CHECK OF FUEL TANKS FORMICRO-ORGANISMS

28 11-00-001600HR/12MOAIRFRAME258

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 28-11-00

LH WING WATER DRAIN VALVE28 11-05

AIRFRAME259

14-AUG-2009 H: 0

L83A13-628 D79611

RH WING WATER DRAIN VALVE28 11-05

AIRFRAME260

14-AUG-2009 H: 0

L83A13-628 D79612

LH WING DUMP VALVE28 11-07

AIRFRAME261

14-AUG-2009 H: 0

V98A32-001 D84960

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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RH WING DUMP VALVE28 11-07

AIRFRAME262

14-AUG-2009 H: 0

V98A32-001 D90339

SPECIAL DETAILED INSPECTION OF FUEL VENT NACA28 12-01-001600HR/12MOAIRFRAME263

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 28-12-01

LH WING FUEL TANK FLOAT VENT VALVE28 12-03

AIRFRAME264

14-AUG-2009 H: 0

L87-19-001P2 D95237

RH WING FUEL TANK FLOAT VENT VALVE28 12-03

AIRFRAME265

14-AUG-2009 H: 0

L87-19-001P2 D95227

OPERATIONAL CHECK LH WING FUEL TANK FLOAT VENTVALVE

28 12-03-0016000HRAIRFRAME266

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

L87-19-001P2 D95237 AMM 28-12-03

OPERATIONAL CHECK RH WING FUEL TANK FLOAT VENTVALVE

28 12-03-0016000HRAIRFRAME267

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

L87-19-001P2 D95227 AMM 28-12-03

LH WING DRAIN CHECK VALVE28 12-05

AIRFRAME268

14-AUG-2009 H: 0

PN SN-UNKNOWN

RH WING DRAIN CHECK VALVE28 12-05

AIRFRAME269

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.1 3/4 IN CHECK VALVE28 21-00

AIRFRAME270

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.2 3/4 IN CHECK VALVE28 21-00

AIRFRAME271

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.3 3/4 IN CHECK VALVE28 21-00

AIRFRAME272

14-AUG-2009 H: 0

PN SN-UNKNOWN

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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NO.4 3/4 IN CHECK VALVE28 21-00

AIRFRAME273

14-AUG-2009 H: 0

PN SN-UNKNOWN

LH WING DC AUXILIARY CANISTER BOOST PUMP28 21-03

AIRFRAME274

14-AUG-2009 H: 0

C93R19-601 D72104

RH WING DC AUXILIARY CANISTER BOOST PUMP28 21-03

AIRFRAME275

14-AUG-2009 H: 0

C93R19-601 D72101

LH WING DC AUXILIARY CARTRIDGE BOOST PUMP28 21-04

AIRFRAME276

14-AUG-2009 H: 0

P99C19-601 D89514

RH WING DC AUXILIARY CARTRIDGE BOOST PUMP28 21-04

AIRFRAME277

14-AUG-2009 H: 0

P99C19-601 D89506

LH WING MAIN EJECTOR PUMP28 21-05

AIRFRAME278

14-AUG-2009 H: 0

T99A19-601 D67804

RH WING MAIN EJECTOR PUMP28 21-05

AIRFRAME279

14-AUG-2009 H: 0

T99A19-601 D67805

OPERATIONAL CHECK LEFT WING 0.75 IN SHUTOFF VALVE28 21-07-001 AIRWORTHINESS

AIRFRAME280

14-AUG-2009 H: 1200.00 H: 1200.00 H: 53.30

B97-15-601 D79467 AMM 28-21-07

OPERATIONAL CHECK RIGHT WING 0.75 IN SHUTOFF VALVE28 21-07-001 AIRWORTHINESS

AIRFRAME281

14-AUG-2009 H: 1200.00 H: 1200.00 H: 53.30

B97-15-601 D79468 AMM 28-21-07

LEFT WING 0.75 IN SHUTOFF VALVE28 21-07-01

AIRFRAME282

14-AUG-2009 H: 0

B97-15-601 D79467

RIGHT WING 0.75 IN SHUTOFF VALVE28 21-07-01

AIRFRAME283

14-AUG-2009 H: 0

B97-15-601 D79468

Page 28 of 193

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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LH WING 28-V DC ENGINE SHUTOFF VALVE ACTUATORASSEMBLY

28 21-07-02

AIRFRAME284

14-AUG-2009 H: 0

D97C00-644P2 C70301

RH WING 28-V DC ENGINE SHUTOFF VALVE ACTUATORASSEMBLY

28 21-07-02

AIRFRAME285

14-AUG-2009 H: 0

D97C00-644P2 C70288

OPERATIONAL CHECK 1.5 IN FUEL SYSTEM SHUTOFFVALVE

28 21-08-0011200HR/24MOAIRFRAME286

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

B97-38-603P2 D84987 AMM 28-21-08

1.5 IN FUEL SYSTEM SHUTOFF VALVE28 21-08-01

AIRFRAME287

14-AUG-2009 H: 0

B97-38-603P2 D84987

ENGINE 28-V DC TRANSFER VALVE ACTUATOR ASSEMBLY28 21-08-02

AIRFRAME288

14-AUG-2009 H: 0

D97C00-644P2 C70285

LH WING MOTIVE FLOW 3/8 IN CHECK VALVE28 21-11

AIRFRAME289

14-AUG-2009 H: 0

L96-09-001P4 D84406

RH WING MOTIVE FLOW 3/8 IN CHECK VALVE28 21-11

AIRFRAME290

14-AUG-2009 H: 0

L96-09-001P4 D84409

FUEL CONTROL PANEL28 21-13

AIRFRAME291

14-AUG-2009 H: 0

441-42854-002 0075

NO. 1 LEFT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME292

14-AUG-2009 H: 0

765551-1-0 765551IN00148

NO. 1 RIGHT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME293

14-AUG-2009 H: 0

765826-1-0 765826IN00187

NO. 2 LEFT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME294

14-AUG-2009 H: 0

765548-1-0 765548IN00186

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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NO. 2 RIGHT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME295

14-AUG-2009 H: 0

765827-1-0 765827IN00200

NO. 3 LEFT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME296

14-AUG-2009 H: 0

765549-1-0 765549IN00296

NO. 3 RIGHT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME297

14-AUG-2009 H: 0

765549-1-0 765549IN00308

NO. 4 LEFT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME298

14-AUG-2009 H: 0

765550-1-0 765550IN00109

NO. 4 RIGHT WING FUEL QUANTITY PROBE28 41-01

AIRFRAME299

14-AUG-2009 H: 0

765550-1-0 765550IN00218

ELECTRONIC FUEL CONTROL UNIT28 41-05

AIRFRAME300

14-AUG-2009 H: 0

738667-2-6 738790IN00137

FUEL TEMPERATURE SENSOR28 43-01

AIRFRAME301

14-AUG-2009 H: 0

798840-1-0 01831

FUNCTIONAL CHECK FUEL TEMPERATURE SENSOR28 43-01-0016000HRAIRFRAME302

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

798840-1-0 01831 AMM 28-43-01

NO.1 FUEL LOW PRESSURE SWITCH28 45-01

AIRFRAME303

14-AUG-2009 H: 0

D98C07-611 0155

NO.2 FUEL LOW PRESSURE SWITCH28 45-01

AIRFRAME304

14-AUG-2009 H: 0

D98C07-611 0187

VISUAL CHECK HYDRAULIC SYSTEM FILTER DIFFERENTIALPRESSURE INDICATOR (DPI)

29 00-00-001600HR/12MOAIRFRAME305

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

PN SN-UNKNOWN AMM 29-31-02

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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HYDRAULIC POWERPACK29 11-01

AIRFRAME306

10-FEB-2012H: 575.60L: 570

H: 0

3032683-000 MX742451A

RESTORATION HYDRAULIC POWERPACK ELECTRICAL MOTOR29 11-01-001

AIRFRAME307

10-FEB-2012H: 575.60L: 570

H: 1200.00 H: +/-30 H: 0 H: 1775.60 H: 628.90

3032683-000 MX742451A AMM 29-11-01

HYDRAULIC FLUID TEMPERATURE SWITCH29 11-09

AIRFRAME308

14-AUG-2009 H: 0

PN SN-UNKNOWN

FUNCTIONAL CHECK HYDRAULIC FLUID TEMPERATURESWITCH

29 11-09-0016000HRAIRFRAME309

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 29-11-09

DISCARD OF HYDRAULIC RESERVOIR29 11-11-001

AIRFRAME1921

14-AUG-2009 H: 3600.00 H: 3600.00 H: 2453.30

AMM 29-11-11-960-801-A/200

DISCARD OF BLEED/ RELIEF VALVE29 11-12-001

AIRFRAME1922

14-AUG-2009 H: 3600.00 H: 3600.00 H: 2453.30

AMM 29-11-12-960-801-A/200

HYDRAULIC ACCUMULATOR29 15-03

AIRFRAME310

14-AUG-2009 H: 0

MS28797-3 8423-12670

POWERPACK VENTILATION FAN29 20-01

AIRFRAME311

01-APR-2011H: 384.30L: 416

H: 0

SF9202D00 L00159

OPERATIONAL CHECK POWERPACK VENTILATION FAN29 20-01-001600HRAIRFRAME312

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

SF9202D00 L00159 AMM 29-20-01

HYDRAULIC SYSTEM FILTER DIFFERENTIAL PRESSUREINDICATOR

29 31-02

AIRFRAME313

14-AUG-2009 H: 0

PN SN-UNKNOWN

ICE PROTECTION/HEATING SYSTEM CONTROL PANEL30 01-01

AIRFRAME314

14-AUG-2009 H: 0

441-43199-001 0060

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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OPERATIONAL CHECK OF PNEUMATIC DE-ICING SYSTEM30 10-00-001600HR/12MOAIRFRAME315

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 30-10-00

DE-ICING SYSTEM CONTROLLER30 11-01

AIRFRAME316

14-AUG-2009 H: 0

4D2037-24 U0101

NO.1 REAR FUSELAGE CHECK VALVE30 11-02

AIRFRAME317

14-AUG-2009 H: 0

3D3555-01 N085771

NO.2 REAR FUSELAGE CHECK VALVE30 11-02

AIRFRAME318

14-AUG-2009 H: 0

3D3555-01 N085772

REAR FUS PRESSURE REGULATOR/RELIEVER VALVE30 11-03

AIRFRAME319

14-AUG-2009 H: 0

4D2095-201 N084993

CLEANING REAR FUS PRESSURE REGULATOR/RELIEVERVALVE

30 11-03-0016000HRAIRFRAME320

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

4D2095-201 N084993 AMM 30-11-03

WATER SEPARATOR30 11-04

AIRFRAME321

14-AUG-2009 H: 0

44E13-1A N086189

CLEANING WATER SEPARATOR30 11-04-0016000HRAIRFRAME322

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

44E13-1A N086189 AMM 30-11-04

REAR FUS LOW PRESSURE SWITCH30 11-05

AIRFRAME323

14-AUG-2009 H: 0

3D3552-02 0088

FUNCTIONAL CHECK REAR FUS LOW PRESSURE SWITCH30 11-05-0016000HRAIRFRAME324

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

3D3552-02 0088 AMM 30-11-05

INBOARD WING FLOW CONTROL VALVE30 13-01

AIRFRAME325

14-AUG-2009 H: 0

3D2376-07 N086208

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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OUTBOARD WING FLOW CONTROL VALVE30 13-01

AIRFRAME326

14-AUG-2009 H: 0

3D2376-07 N086203

NO.1 L/H WING DE ICE PRESSURE SWITCH30 13-02

AIRFRAME327

14-AUG-2009 H: 0

3D3533-04 0285

NO.1 R/H WING DE ICE PRESSURE SWITCH30 13-02

AIRFRAME328

14-AUG-2009 H: 0

3D3533-04 0286

NO.2 L/H WING DE ICE PRESSURE SWITCH30 13-02

AIRFRAME329

14-AUG-2009 H: 0

3D3533-04 0295

NO.2 R/H WING DE ICE PRESSURE SWITCH30 13-02

AIRFRAME330

14-AUG-2009 H: 0

3D3533-04 0284

FUNCTIONAL CHECK NO.1 L/H WING DE ICE PRESSURESWITCH

30 13-02-0016000HRAIRFRAME331

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

3D3533-04 0285 AMM 30-13-03

FUNCTIONAL CHECK NO.1 R/H WING DE ICE PRESSURESWITCH

30 13-02-0016000HRAIRFRAME332

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

3D3533-04 0286 AMM 30-13-02

FUNCTIONAL CHECK NO.2 L/H WING DE ICE PRESSURESWITCH

30 13-02-0016000HRAIRFRAME333

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

3D3533-04 0295 AMM 30-13-02

FUNCTIONAL CHECK NO.2 R/H WING DE ICE PRESSURESWITCH

30 13-02-0016000HRAIRFRAME334

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

3D3533-04 0284 AMM 30-13-02

LH WING DE-ICER BOOT30 13-03

AIRFRAME335

14-AUG-2009 H: 0

PS29S4D5321-23 MBLT110

RH WING DE-ICER BOOT30 13-03

AIRFRAME336

14-AUG-2009 H: 0

PS29S4D5321-24 MBLT180

Page 33 of 193

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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GENERAL VISUAL INSPECTION LH WING DE-ICER BOOT30 13-03-001600HR/12MOAIRFRAME337

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

PS29S4D5321-23 MBLT110 AMM 30-13-03

GENERAL VISUAL INSPECTION RH WING DE-ICER BOOT30 13-03-001600HR/12MOAIRFRAME338

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

PS29S4D5321-24 MBLT180 AMM 30-13-03

REAR FUS FLOW CONTROL VALVE30 15-01

AIRFRAME339

14-AUG-2009 H: 0

3D2376-07 N086207

REAR FUS DE ICE PRESSURE SWITCH30 15-02

AIRFRAME340

14-AUG-2009 H: 0

3D3533-04 0254

FUNCTIONAL CHECK REAR FUS DE ICE PRESSURE SWITCH30 15-02-0016000HRAIRFRAME341

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

3D3533-04 0254 AMM 30-15-02

LH TAIL DE-ICER BOOT30 15-03

AIRFRAME342

14-AUG-2009 H: 0

PS29S4D5321-21 MBKT080

RH TAIL DE-ICER BOOT30 15-03

AIRFRAME343

14-AUG-2009 H: 0

PS29S4D5321-22 MBJX020

GENERAL VISUAL INSPECTION LH TAIL DE-ICER BOOT30 15-03-001600HR/12MOAIRFRAME344

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 30-15-03

GENERAL VISUAL INSPECTION RH TAIL DE-ICER BOOT30 15-03-001600HR/12MOAIRFRAME345

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 30-15-03

LEFT ENGINE ANTI-ICE SYSTEM SHUTOFF VALVE30 21-01

AIRFRAME346

14-AUG-2009 H: 0

5727-00-5 0152

RIGHT ENGINE ANTI-ICE SYSTEM SHUTOFF VALVE30 21-01

AIRFRAME347

14-AUG-2009 H: 0

5727-00-5 0184

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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LH ENG ANTI-ICE PRESSURE TRANSDUCER30 21-02

AIRFRAME348

14-AUG-2009 H: 0

APTE-473A-1000-50G 7367-6-95

RH ENG ANTI-ICE PRESSURE TRANSDUCER30 21-02

AIRFRAME349

14-AUG-2009 H: 0

APTE-473A-1000-50G 7367-6-322

FUNCTIONAL CHECK LH ENG ANTI-ICE PRESSURETRANSDUCER

30 21-02-00112000H/120MAIRFRAME350

14-AUG-2009 M: 120H:12000.00

D: +/-30H: +/-30

14-AUG-2019H: 12000.00

M: 54 D: 11H: 10853.30

APTE-473A-1000-50G 7367-6-95 AMM 30-21-02

FUNCTIONAL CHECK RH ENG ANTI-ICE PRESSURETRANSDUCER

30 21-02-00112000H/120MAIRFRAME351

14-AUG-2009 M: 120H:12000.00

D: +/-30H: +/-30

14-AUG-2019H: 12000.00

M: 54 D: 11H: 10853.30

APTE-473A-1000-50G 7367-6-322 AMM 30-21-02

BORESCOPE INSPECTION OF PICCOLO TUBE30 21-03-0016000HRAIRFRAME352

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 30-21-03

DETAILED VISUAL INSPECTION OF ENGINE ANTI-ICEDUCTS

30 21-04-0011800HRAIRFRAME353

14-AUG-2009 H: 1800.00 H: +/-30 H: 1800.00 H: 653.30

AMM 30-21-00

OPERATIONAL CHECK OF PITOT, STATIC, AOA ANDP-STATIC HEATING

30 31-00-00124MOAIRFRAME354

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 30-30-00

AIR DATA PROBES HEATER CURRENT MONITOR30 31-01

AIRFRAME355

14-AUG-2009 H: 0

C-100131-1 227

FUNCTIONAL CHECK OF WINDSHIELD RAIN REPELLENTCOATING

30 41-01-001600HR/12MOAIRFRAME356

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 30-41-01

OPERATIONAL CHECK OF WINDSHIELD HEATING SYSTEM30 42-00-001600HRAIRFRAME357

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

AMM 30-42-00

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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LH WINDSHIELD HEATER CONTROL UNIT30 42-01

AIRFRAME358

18-DEC-2009H: 44.10L: 49

H: 0

EPM-112-1 00570

RH WINDSHIELD HEATER CONTROL UNIT30 42-01

AIRFRAME359

15-JUN-2011H: 464.30L: 480

H: 0

EPM-112-2 00744

CREW CABIN LIGHT ICING INDICATOR30 81-01

AIRFRAME360

14-AUG-2009 H: 0

PN SN-UNKNOWN

OPERATIONAL CHECK CVR31 31-00-00212MOAIRFRAME361

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

2100-3083-50 000596465 AMM 31-31-00

CVR31 31-01

AIRFRAME362

14-AUG-2009 H: 0

2100-3083-50 000596465

CVDR/ULB UNDERWATER LOCATOR BEACON31 31-03

AIRFRAME363

14-AUG-2009 H: 0

DK120 SC62151

DISCARD CVDR/ULB UNDERWATER LOCATOR BEACON BATTERY

31 31-03-001 DISCARD

AIRFRAME364

M: 72 D: +/-30 M: 0 31-MAY-2015 M: 3 D: 28

DK120 SC62151 AMM 31-31-03

IMPACT SWITCH31 31-04

AIRFRAME365

14-AUG-2009 H: 0

5930-4-000 4379

CVDR INSC ILLUM PANEL31 31-09

AIRFRAME366

14-AUG-2009 H: 0

441-42635-002 0065

UNDERWATER LOCATOR BEACON BATTERY31 31-13

AIRFRAME367

14-AUG-2009 H: 0

PN SN-UNKNOWN

GSD 41 DATA CONCENTRATOR UNIT31 41-01

AIRFRAME368

14-AUG-2009 H: 0

011-01457-00 16905051

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Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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NO.1 ENGINE/AIRFRAME INTERFACE UNIT31 41-03

AIRFRAME369

14-AUG-2009 H: 0

011-00831-00 46710038

NO.2 ENGINE/AIRFRAME INTERFACE UNIT31 41-03

AIRFRAME370

14-AUG-2009 H: 0

011-00831-00 46710015

NO.3 ENGINE/AIRFRAME INTERFACE UNIT31 41-03

AIRFRAME371

14-AUG-2009 H: 0

011-00831-00 46709995

NO.1 GIA63W INTEGRATED AVIONICS UNIT31 41-05

AIRFRAME372

14-AUG-2009 H: 0

011-01105-01 15W008843

NO.2 GIA63W INTEGRATED AVIONICS UNIT31 41-05

AIRFRAME373

14-AUG-2009 H: 0

011-01105-01 15W008872

NO.1 AMLCD (GDU1240A, 12IN) DISPLAY UNIT31 41-06

AIRFRAME374

14-AUG-2009 H: 0

011-01440-10 18T000705

NO.2 AMLCD (GDU1240A, 12IN) DISPLAY UNIT31 41-06

AIRFRAME375

14-AUG-2009 H: 0

011-01440-10 18T000718

NO.3 AMLCD (GDU1240A, 12IN) DISPLAY UNIT31 41-06

AIRFRAME376

21-DEC-2011H: 546.70L: 550

H: 0

011-01440-10 18T000668

OPERATIONAL CHECK OF HSDB SWITCH REVERSION31 42-00-0016000HRAIRFRAME377

14-AUG-2009 H: 6000.00 H: +/-30 H: 6000.00 H: 4853.30

AMM 31-42-00

MAINTENANCE CONTROL PANEL31 42-01

AIRFRAME378

14-AUG-2009 H: 0

441-40947-001 0081

OPERATIONAL CHECK MFD 1 FLIGHT DISPLAY SYSTEM(MANUAL AND AUTOMATIC REVERSION MODE)

31 61-00-0013000HRAIRFRAME379

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 31-61-00

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Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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OPERATIONAL CHECK PFD 1 FLIGHT DISPLAY SYSTEM(MANUAL AND AUTOMATIC REVERSION MODE)

31 61-00-0013000HRAIRFRAME380

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 31-61-00

OPERATIONAL CHECK PFD 2 FLIGHT DISPLAY SYSTEM(MANUAL AND AUTOMATIC REVERSION MODE)

31 61-00-0013000HRAIRFRAME381

14-AUG-2009 H: 3000.00 H: +/-30 H: 3000.00 H: 1853.30

AMM 31-61-00

GENERAL VISUAL INSPECTION PFD 2 L/HIRF PROTECTIONON THE DISPLAYS (PFD AND MFD)

31H31-01-220-001 6000HR/96MO

AIRFRAME384

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-61-01

GENERAL VISUAL INSPECTION PFD 1 L/HIRF PROTECTIONON THE DISPLAYS (PFD AND MFD)

31H31-01-220-001 6000HR/96MO

AIRFRAME383

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-61-01

GENERAL VISUAL INSPECTION MFD 1 L/HIRF PROTECTIONON THE DISPLAYS (PFD AND MFD)

31H31-01-220-001 6000HR/96MO

AIRFRAME382

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-61-01

GENERAL VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE GIAS

31H31-02-220-001 6000HR/96MO

AIRFRAME385

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-41-05

GENERAL VISUAL INSPECTION RIGHT L/HIRF PROTECTIONON THE GIAS

31H31-02-220-001 6000HR/96MO

AIRFRAME386

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-41-05

GENERAL VISUAL INSPECTION NO. 1 L/HIRF PROTECTIONON THE GEAS

31H31-03-220-001 6000HR/96MO

AIRFRAME387

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-41-03

GENERAL VISUAL INSPECTION NO. 2 L/HIRF PROTECTIONON THE GEAS

31H31-03-220-001 6000HR/96MO

AIRFRAME388

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-41-03

GENERAL VISUAL INSPECTION NO. 3 L/HIRF PROTECTIONON THE GEAS

31H31-03-220-001 6000HR/96MO

AIRFRAME389

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 31-41-03

LEFT MAIN GEAR ASSEMBLY32 000

AIRFRAME391

14-AUG-2009 H: 0

PN SN-UNKNOWN

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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RIGHT MAIN GEAR ASSEMBLY32 000

AIRFRAME392

14-AUG-2009 H: 0

PN SN-UNKNOWN

EXTERNAL GENERAL VISUAL INSPECTION OF LANDINGGEAR POLYURETHANE FILMS

32 00-00-00112MOAIRFRAME390

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 32-13-20

LEFT MAIN GEAR SHOCK STRUT FITTING32 001 LIFE LIMIT

AIRFRAME393

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2206-501 1264867/001

RIGHT MAIN GEAR SHOCK STRUT FITTING32 002 LIFE LIMIT

AIRFRAME394

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2206-502 1279063/001

NO.1 LEFT MAIN GEAR PINTLE PIN32 005 LIFE LIMIT

AIRFRAME395

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2107-001 1249572/004

NO.1 RIGHT MAIN GEAR PINTLE PIN32 005 LIFE LIMIT

AIRFRAME396

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2107-001 1249572/006

NO.2 LEFT MAIN GEAR PINTLE PIN32 005 LIFE LIMIT

AIRFRAME397

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2107-001 1249572/017

NO.2 RIGHT MAIN GEAR PINTLE PIN32 005 LIFE LIMIT

AIRFRAME398

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2107-001 1249572/018

LEFT MAIN GEAR UPPER AXLE32 006 LIFE LIMIT

AIRFRAME399

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2104-001 1263612/001

RIGHT MAIN GEAR UPPER AXLE32 006 LIFE LIMIT

AIRFRAME400

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2104-001 1263612/014

LEFT MAIN GEAR LOWER AXLE32 007 LIFE LIMIT

AIRFRAME401

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2108-003 1259880/026

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Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

RIGHT MAIN GEAR LOWER AXLE32 007 LIFE LIMIT

AIRFRAME402

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2108-003 1259880/021

LEFT MAIN GEAR JACKING PIN32 008 LIFE LIMIT

AIRFRAME403

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2109-001 1265803/004

RIGHT MAIN GEAR JACKING PIN32 008 LIFE LIMIT

AIRFRAME404

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2109-001 1265803/018

LEFT MAIN GEAR PIN32 009 LIFE LIMIT

AIRFRAME405

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2103-001 1263611/012

RIGHT MAIN GEAR PIN32 009 LIFE LIMIT

AIRFRAME406

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2103-001 1263611/009

LEFT MAIN GEAR PIN32 010 LIFE LIMIT

AIRFRAME407

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2113-003 1247292/008

RIGHT MAIN GEAR PIN32 010 LIFE LIMIT

AIRFRAME408

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-2113-003 1257052/006

LEFT MAIN LANDING GEAR MAIN FITTING.32 014 LIFE LIMIT

AIRFRAME1891

L: 7000 L: 0 L: 7000 L: 6047

2310-2206-503

RIGHT MAIN LANDING GEAR MAIN FITTING.32 014 LIFE LIMIT

AIRFRAME1897

L: 7000 L: 0 L: 7000 L: 6047

2310-2206-503

LEFT MAIN LANDING GEAR MAIN FITTING32 015 LIFE LIMIT

AIRFRAME1892

L: 7000 L: 0 L: 7000 L: 6047

2310-2206-504

RIGHT MAIN LANDING GEAR MAIN FITTING32 015 LIFE LIMIT

AIRFRAME1898

L: 7000 L: 0 L: 7000 L: 6047

2310-2206-504

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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LEFT MAIN LANDING GEAR PINTLE PIN32 016 LIFE LIMIT

AIRFRAME1893

L: 7000 L: 0 L: 7000 L: 6047

2310-2107-003

LEFT MAIN LANDING GEAR PINTLE PIN.32 016 LIFE LIMIT

AIRFRAME1899

L: 7000 L: 0 L: 7000 L: 6047

2310-2107-003

RIGHT MAIN LANDING GEAR PINTLE PIN32 016 LIFE LIMIT

AIRFRAME1900

L: 7000 L: 0 L: 7000 L: 6047

2310-2107-003

RIGHT MAIN LANDING GEAR PINTLE PIN.32 016 LIFE LIMIT

AIRFRAME1901

L: 7000 L: 0 L: 7000 L: 6047

2310-2107-003

LEFT MAIN GEAR TRAILING ARM ASSEMBLY32 100

AIRFRAME409

14-AUG-2009 H: 0

2310-3000-401 00072

RIGHT MAIN GEAR TRAILING ARM ASSEMBLY32 100

AIRFRAME410

14-AUG-2009 H: 0

PN SN-UNKNOWN

LEFT MAIN GEAR TRAILING ARM AXLE32 101 LIFE LIMIT

AIRFRAME411

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2102-001 1256017/007

RIGHT MAIN GEAR TRAILING ARM AXLE32 101 LIFE LIMIT

AIRFRAME412

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-2102-001 1256017/004

LEFT MAIN GEAR TRAILING ARM32 102 LIFE LIMIT

AIRFRAME413

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-3002-501 1255978/002

RIGHT MAIN GEAR TRAILING ARM32 103 LIFE LIMIT

AIRFRAME414

14-AUG-2009 L: 6360 L: 0 L: 6360 L: 5407

2310-3002-502 12559B4/004

LEFT MAIN GEAR TRAILING ARM WHEEL AXLE32 106 LIFE LIMIT

AIRFRAME415

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-3010-001 1267265/009

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

RIGHT MAIN GEAR TRAILING ARM WHEEL AXLE32 106 LIFE LIMIT

AIRFRAME416

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-3010-001 1267265/005

LEFT MAIN LANDING GEAR AXLE32 107 LIFE LIMIT

AIRFRAME1894

L: 7000 L: 0 L: 7000 L: 6047

2310-2102-003

RIGHT MAIN LANDING GEAR AXLE32 107 LIFE LIMIT

AIRFRAME1902

L: 7000 L: 0 L: 7000 L: 6047

2310-2102-003

LEFT MAIN LANDING GEAR TRAILING ARM32 108 LIFE LIMIT

AIRFRAME1895

L: 7000 L: 0 L: 7000 L: 6047

2310-3002-503

RIGHT MAIN LANDING GEAR TRAILING ARM32 108 LIFE LIMIT

AIRFRAME1903

L: 7000 L: 0 L: 7000 L: 6047

2310-3002-503

LEFT MAIN LANDING GEAR TRAILING ARM.32 109 LIFE LIMIT

AIRFRAME1896

L: 7000 L: 0 L: 7000 L: 6047

2310-3002-504

RIGHT MAIN LANDING GEAR TRAILING ARM.32 109 LIFE LIMIT

AIRFRAME1904

L: 7000 L: 0 L: 7000 L: 6047

2310-3002-504

GENERAL VISUAL INSPECTION LEFT MAIN GEAR ASSEMBLY32 11-00-001600HR/12MOAIRFRAME417

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

GENERAL VISUAL INSPECTION RIGHT MAIN GEAR ASSEMBLY32 11-00-001600HR/12MOAIRFRAME418

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

RESTORE LEFT MAIN GEAR ASSEMBLY32 11-00-002

AIRFRAME419

30-JUN-2009 M: 96L: 12000

D: +/-30L: +/-30

M: 0L: 0

30-JUN-2017L: 12000

M: 28 D: 27L: 11047

PN SN-UNKNOWN

RESTORE RIGHT MAIN GEAR ASSEMBLY32 11-00-002

AIRFRAME420

30-JUN-2009 M: 96L: 12000

D: +/-30L: +/-30

M: 0L: 0

30-JUN-2017L: 12000

M: 28 D: 27L: 11047

PN SN-UNKNOWN

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LUBRICATION LEFT MAIN GEAR ASSEMBLY32 11-00-003600HR/12MOAIRFRAME421

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-21-00

LUBRICATION RIGHT MAIN GEAR ASSEMBLY32 11-00-003600HR/12MOAIRFRAME422

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-21-00

LEFT MAIN GEAR SHOCK STRUT32 11-01

AIRFRAME423

14-AUG-2009 H: 0

2310-2000-403 00069

RIGHT MAIN GEAR SHOCK STRUT32 11-01

AIRFRAME424

14-AUG-2009 H: 0

2310-2000-404 00062

SERVICING LEFT MAIN GEAR SHOCK ABSORBER ASSEMBLY32 11-03-004600HR/12MOAIRFRAME425

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-14-02

SERVICING RIGHT MAIN GEAR SHOCK ABSORBER ASSEMBLY32 11-03-004600HR/12MOAIRFRAME426

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-14-02

LEFT MAIN GEAR SHOCK ABSORBER ASSEMBLY32 200

AIRFRAME427

14-AUG-2009 H: 0

2310-4000-403 00204

RIGHT MAIN GEAR SHOCK ABSORBER ASSEMBLY32 200

AIRFRAME428

14-AUG-2009 H: 0

2310-4000-403 00215

LEFT MAIN GEAR SHOCK ABSORBER CYLINDER32 201 LIFE LIMIT

AIRFRAME429

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4102-501 1262143/003

RIGHT MAIN GEAR SHOCK ABSORBER CYLINDER32 201 LIFE LIMIT

AIRFRAME430

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4102-501 1282853/003

LEFT MAIN GEAR SHOCK ABSORBER SLIDING TUBE32 204 LIFE LIMIT

AIRFRAME431

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4201-003 1263137/004

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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RIGHT MAIN GEAR SHOCK ABSORBER SLIDING TUBE32 204 LIFE LIMIT

AIRFRAME432

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4201-003 1265924/004

LEFT MAIN GEAR SHOCK ABSORBER BEARING32 206 LIFE LIMIT

AIRFRAME433

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4006-007 1278450/009

RIGHT MAIN GEAR SHOCK ABSORBER BEARING32 206 LIFE LIMIT

AIRFRAME434

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4006-007 1280249/009

LEFT MAIN GEAR SHOCK ABSORBER BEARING CAP32 207 LIFE LIMIT

AIRFRAME435

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4014-001 1278429/005

RIGHT MAIN GEAR SHOCK ABSORBER BEARING CAP32 207 LIFE LIMIT

AIRFRAME436

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-4014-001 1287355/005

GENERAL VISUAL INSPECTION NOSE LANDING GEARASSEMBLY

32 21-00-001600HR/12MOAIRFRAME437

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 32-21-00

RESTORE NOSE LANDING GEAR ASSEMBLY32 21-00-002

AIRFRAME438

30-JUN-2009 M: 84L: 12000

D: +/-30L: +/-30

M: 0L: 0

30-JUN-2016L: 12000

M: 16 D: 27L: 11047

PN SN-UNKNOWN AMM 32-21-00

LUBRICATION NOSE LANDING GEAR ASSEMBLY32 21-00-003600HR/12MOAIRFRAME439

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-21-00

NOSE LANDING GEAR SHOCK STRUT32 21-01

AIRFRAME440

14-AUG-2009 H: 0

2310-1000-403 00068

NOSE LANDING GEAR RETRACT ACTUATOR ASSEMBLY32 21-02

AIRFRAME441

14-AUG-2009 H: 0

2135-1000-403 00077

NOSE LANDING GEAR DOWNLOCK RELEASE ACTUATORASSEMBLY

32 21-03

AIRFRAME442

14-AUG-2009 H: 0

2137-1000-401 00069

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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SERVICING NOSE LANDING GEAR (ALUM STRUT) SHOCKABSORBER

32 21-05-004600HR/12MOAIRFRAME443

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 12-14-03

VISUAL CHECK NOSE LANDING GEAR SHIMMY DAMPER32 21-06-005600HR/12MOAIRFRAME444

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

M: 0H: 0

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

SAME Same AMM 12-14-04

LEFT MAIN GEAR LOCKING ACTUATOR ASSEMBLY32 300

AIRFRAME445

14-AUG-2009 H: 0

2136-1000-403 00141

RIGHT MAIN GEAR LOCKING ACTUATOR ASSEMBLY32 300

AIRFRAME446

14-AUG-2009 H: 0

2136-1000-403 00142

LEFT MAIN GEAR LOCKING ACTUATOR CYLINDER32 301 LIFE LIMIT

AIRFRAME447

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1013-501 1262144/003

RIGHT MAIN GEAR LOCKING ACTUATOR CYLINDER32 301 LIFE LIMIT

AIRFRAME448

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1013-501 1262144/009

LEFT MAIN GEAR LOCKING ACTUATOR PISTON32 304 LIFE LIMIT

AIRFRAME449

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1035-003 1263684/004

RIGHT MAIN GEAR LOCKING ACTUATOR PISTON32 304 LIFE LIMIT

AIRFRAME450

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1035-003 1263684/002

LEFT MAIN GEAR LOCKING ACTUATOR FINGER32 305 LIFE LIMIT

AIRFRAME451

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1050-003 1265870/004

RIGHT MAIN GEAR LOCKING ACTUATOR FINGER32 305 LIFE LIMIT

AIRFRAME452

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1050-003 1265870/007

LEFT MAIN GEAR LOCKING ACTUATOR ROD32 306 LIFE LIMIT

AIRFRAME453

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1020-001 1263588/055

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

RIGHT MAIN GEAR LOCKING ACTUATOR ROD32 306 LIFE LIMIT

AIRFRAME454

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1020-001 1263588/006

LEFT MAIN GEAR LOCKING ACTUATOR LOCKING PISTON32 307 LIFE LIMIT

AIRFRAME455

14-AUG-2009 L: 5500 L: 0 L: 5500 L: 4547

2136-1046-007 1249689/007

RIGHT MAIN GEAR LOCKING ACTUATOR LOCKING PISTON32 307 LIFE LIMIT

AIRFRAME456

14-AUG-2009 L: 5500 L: 0 L: 5500 L: 4547

2136-1046-007 1249689/005

LEFT MAIN GEAR LOCKING ACTUATOR PIN32 309 LIFE LIMIT

AIRFRAME457

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1049-001 1258408/004

RIGHT MAIN GEAR LOCKING ACTUATOR PIN32 309 LIFE LIMIT

AIRFRAME458

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1049-001 1258408/002

RIGHT MAIN GEAR LOCKING ACTUATOR LOCKING SLEEVE32 310 LIFE LIMIT

AIRFRAME462

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1036-003 1262125/008

LEFT MAIN GEAR LOCKING ACTUATOR LOCKING SLEEVE32 310 LIFE LIMIT

AIRFRAME461

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1036-003 1268883/010

LANDING GEAR CONTROL LEVER PANEL32 31-01

AIRFRAME459

14-AUG-2009 H: 0

827101-5 1072

LANDING GEAR HYDRAULIC SYSTEM (MANIFOLD)ASSEMBLY

32 31-02

AIRFRAME460

20-JUN-2011H: 464.30L: 481

H: 0

72375-1 0340

LEFT MAIN GEAR LOCKING ACTUATOR CAP BEARING32 311 LIFE LIMIT

AIRFRAME463

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1005-003 1264846/004

RIGHT MAIN GEAR LOCKING ACTUATOR CAP BEARING32 311 LIFE LIMIT

AIRFRAME464

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1005-003 1264845/005

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LEFT MAIN GEAR LOCKING ACTUATOR NUT32 312 LIFE LIMIT

AIRFRAME465

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1042-003 1268453/001

RIGHT MAIN GEAR LOCKING ACTUATOR NUT32 312 LIFE LIMIT

AIRFRAME466

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1042-003 1268453/004

LEFT MAIN GEAR LOCKING ACTUATOR STOP32 313 LIFE LIMIT

AIRFRAME467

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1008-003 1249598/010

RIGHT MAIN GEAR LOCKING ACTUATOR STOP32 313 LIFE LIMIT

AIRFRAME468

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2136-1008-003 1249598/015

LEFT MAIN GEAR LOCKING ACTUATOR ROD END32 314 LIFE LIMIT

AIRFRAME469

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

MEKS12EL 00024

RIGHT MAIN GEAR LOCKING ACTUATOR ROD END32 314 LIFE LIMIT

AIRFRAME470

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

MEKS12EL 00079

FUNCTIONAL CHECK OF LANDING GEAR EMERGENCYEXTENSION SYSTEM

32 35-00-00124MOAIRFRAME471

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 32-35-00

GENERAL VISUAL INSPECTION OF EMERGENCY EXTENSIONSYSTEM LINKAGES

32 35-00-00260MOAIRFRAME472

14-SEP-2014H: 1038.80L: 883

M: 60 D: +/-30 14-SEP-2019 M: 55 D: 11

AMM 32-35-00

NOSE LANDING GEAR ASSEMBLY32 400

AIRFRAME473

14-AUG-2009 H: 0

PN SN-UNKNOWN

LEFT SIDE NLG SIDE PINTLE PIN32 401 LIFE LIMIT

AIRFRAME474

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1137-003 1263734/006

RIGHT SIDE NLG SIDE PINTLE PIN32 401 LIFE LIMIT

AIRFRAME475

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1137-003 1263734/019

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NOSE LANDING GEAR MAIN FITTING32 402 LIFE LIMIT

AIRFRAME476

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1204-501 1249656/002

NOSE LANDING GEAR TORQUE LINK32 404 LIFE LIMIT

AIRFRAME477

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1124-501 1262139/003

NOSE LANDING GEAR SHOCK STRUT PIN32 406 LIFE LIMIT

AIRFRAME478

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

PN SN-UNKNOWN

NOSE LANDING GEAR AXLE32 407 LIFE LIMIT

AIRFRAME479

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1165-001 1263669/010

NOSE LANDING GEAR STEERING BELLCRANK32 408 LIFE LIMIT

AIRFRAME480

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1131-001 1267618/007

NOSE LANDING GEAR SHIMMY DAMPER32 409 LIFE LIMIT

AIRFRAME481

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1500-403 00077

NOSE LANDING GEAR WHEEL AXLE32 410 LIFE LIMIT

AIRFRAME494

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2317-5101-001 1259883/012

DIGITAL BRAKE CONTROL UNIT32 41-01

AIRFRAME482

25-JUN-2010H: 186.70L: 213

H: 0

90005034-3 MAR09-1007

LH PEDAL TRANSDUCER32 41-02

AIRFRAME483

14-AUG-2009 H: 0

Q3008 825633

RH PEDAL TRANSDUCER32 41-02

AIRFRAME484

14-AUG-2009 H: 0

Q3008 825637

OPERATIONAL CHECK LH PEDAL TRANSDUCER BRAKE PEDALTRANSDUCER

32 41-02-0016000HR/96MOAIRFRAME485

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

Q3008 825633 AMM 32-41-02

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

OPERATIONAL CHECK RH PEDAL TRANSDUCER BRAKE PEDALTRANSDUCER

32 41-02-0016000HR/96MOAIRFRAME486

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

Q3008 825637 AMM 32-41-02

FUNCTIONAL CHECK OF BRAKE PEDAL TRANSDUCER32 41-02-002600HR/12MOAIRFRAME1929

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: 30 H: 30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 32-41-02-820-801-A/500

MAIN BRAKE SHUT-OFF VALVE32 41-03

AIRFRAME487

14-AUG-2009 H: 0

90005027 DEC08-0106

RH BRAKE CONTROL VALVE32 41-04

AIRFRAME489

13-SEP-2011H: 504.20L: 504

H: 0

90005035-2 08-09-0122

LH BRAKE CONTROL VALVE32 41-04

AIRFRAME488

13-SEP-2011H: 504.20L: 504

H: 0

90005035-2 09-01-0210

LH MAIN BRAKE SYSTEM PRESSURE TRANSDUCER32 41-05

AIRFRAME490

14-AUG-2009 H: 0

90005191-1 NOV08-0148

RH MAIN BRAKE SYSTEM PRESSURE TRANSDUCER32 41-05

AIRFRAME491

14-AUG-2009 H: 0

90005191-1 NOV08-0151

LEFT MAIN GEAR WHEEL SPEED TRANSDUCER32 41-06

AIRFRAME492

14-AUG-2009 H: 0

90005036 JAN09-0161

RIGHT MAIN GEAR WHEEL SPEED TRANSDUCER32 41-06

AIRFRAME493

14-AUG-2009 H: 0

90005036 DEC08-0157

NOSE LANDING GEAR LOCK PIN32 411 LIFE LIMIT

AIRFRAME495

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

57675-1 00035

FUNCTIONAL CHECK OF BRAKE HYDRAULIC ACCUMULATOR32 41-11-0016000HRAIRFRAME1923

14-AUG-2009 H: 6000.00 H: 6000.00 H: 4853.30

AMM 32-41-11-720-801-A/500

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NOSE LANDING GEAR AXLE BOLT32 412 LIFE LIMIT

AIRFRAME496

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1144-005 1263780/008

NOSE LANDING GEAR BOLT32 413 LIFE LIMIT

AIRFRAME497

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1172-003 1242107/001

NOSE LANDING GEAR PIN32 414 LIFE LIMIT

AIRFRAME498

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1173-001 1265838/008

NOSE LANDING GEAR BOLT32 415 LIFE LIMIT

AIRFRAME499

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1183-001 1263669/010

EMERGENCY/PARKING BRAKE VALVE32 43-02

AIRFRAME500

13-SEP-2011H: 504.20L: 504

H: 0

11056-5 0370

EMERGENCY/PARKING BRAKE ACCUMULATOR32 43-04

AIRFRAME501

14-AUG-2009 H: 0

860231003 60231-2078

EMERGENCY/PARKING BRAKE PRESSURE SWITCH32 43-05

AIRFRAME502

14-AUG-2009 H: 0

15H0126PH 0141

FUNCTIONAL CHECK EMERGENCY/PARKING BRAKE VALVE32 43-05-0011200HR/24MOAIRFRAME503

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

11056-5 0370 AMM 32-43-02-720-801-A/500

EMERGENCY/PARKING BRAKE PRESSURE- TRANSDUCER32 43-06

AIRFRAME504

14-AUG-2009 H: 0

APT-218A-1000-3000A 7539-9-57

EMERGENCY/PARKING BRAKE SHUT OFF VALVE32 43-11

AIRFRAME505

14-AUG-2009 H: 0

2216-0001-401 00030

OPERATIONAL CHECK EMERGENCY/PARKING BRAKE SHUTOFF VALVE

32 43-11-001 AIRWORTHINESS

AIRFRAME506

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

2216-0001-401 00030 AMM 32-43-11

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LH MLG 21X6.5-10 12PR TIRE32 45-01

AIRFRAME507

29-MAR-2012H: 587.40L: 584

H: 0

215K26-1 82620169

RH MLG 21X6.5-10 12PR TIRE32 45-01

AIRFRAME508

29-MAR-2012H: 587.40L: 584

H: 0

215K26-1 82620185

RESTORATION (OVERHAUL) OF LEFT MAIN LANDING GEARWHEEL ASSEMBLY

32 45-01-001 OVERHAUL

AIRFRAME509

26-MAR-2012 H: 0

500-19026-401 DEC09-0508 AMM 32-45-00Notes: AT 6TH, 12TH, 16TH AND EVERY SUBSEQUENT 2ND TIRE CHANGE

RESTORATION (OVERHAUL) OF RIGHT MAIN LANDINGGEAR WHEEL ASSEMBLY

32 45-01-001 OVERHAUL

AIRFRAME510

26-MAR-2012 H: 0

500-19026-401 DEC09-0507 AMM 32-45-00Notes: AT 6TH, 12TH, 16TH AND EVERY SUBSEQUENT 2ND TIRE CHANGE

SPECIAL DETAILED INSPECTION (EDDY CURRENT) OFLEFT MAIN LANDING GEAR WHEEL ASSEMBLY

32 45-01-002 SDI

AIRFRAME2016

N/A

AMM 32-45-00-200-801-A/600Notes: AT 3RD, 9TH, 14TH, 19TH AND EVERY SUBSEQUENT 2ND TIRE CHANGE

SPECIAL DETAILED INSPECTION (EDDY CURRENT) OFRIGHT MAIN LANDING GEAR WHEEL ASSEMBLY

32 45-01-002 SDI

AIRFRAME2017

N/A

AMM 32-45-00-200-801-A/600Notes: AT 3RD, 9TH, 14TH, 19TH AND EVERY SUBSEQUENT 2ND TIRE CHANGE

LH MLG 21X6.5-10, AL WHEEL32 45-02

AIRFRAME511

29-MAR-2012H: 587.40L: 584

H: 0

500-19026-401 DEC09-0508

RH MLG 21X6.5-10, AL WHEEL32 45-02

AIRFRAME512

29-MAR-2012H: 587.40L: 584

H: 0

500-19026-401 DEC09-0507

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LH MLG WHEEL ASSEMBLY32 45-03

AIRFRAME513

29-MAR-2012H: 587.40L: 584

H: 0

500-19026-401 DEC09-0508

RH MLG WHEEL ASSEMBLY32 45-03

AIRFRAME514

29-MAR-2012H: 587.40L: 584

H: 0

500-19026-401 DEC09-0507

NLG 15X6.0-6 10PR TIRE32 45-10

AIRFRAME515

27-MAR-2012H: 587.40L: 584

H: 0

156E06B1 92227100

NLG WHEEL ASSEMBLY32 45-11

AIRFRAME516

27-MAR-2012H: 587.40L: 584

H: 0

90005023-1 JUN09-0251

RESTORATION (OVERHAUL) OF NOSE LANDING GEARWHEEL ASSEMBLY

32 45-11-001 OVERHAUL

AIRFRAME517

26-MAR-2012 H: 0

90005023-1 JUN09-0251 AMM 32-45-00Notes: AT 3RD, 6TH, 8TH AND EVERY SUBSEQUENT 2ND TIRE CHANGE

SPECIAL DETAILED INSPECTION (EDDY CURRENT) OFNOSE LANDING GEAR WHEEL ASSEMBLY

32 45-11-002 SDI

AIRFRAME2018

N/A

AMM 32-45-00-200-801-A/600Notes: AT 2ND, 5TH AND 7TH TIRE CHANGE

NLG 15X6.0-6, AL WHEEL32 45-12

AIRFRAME518

27-MAR-2012H: 587.40L: 584

H: 0

90005023-1 JUN09-0251

LH MLG STEEL BRAKE ASSEMBLY32 45-21

AIRFRAME519

01-APR-2011H: 384.30L: 416

H: 0

90005025-3 AUG10-0553

RH MLG STEEL BRAKE ASSEMBLY32 45-21

AIRFRAME520

01-APR-2011H: 384.30L: 416

H: 0

90005025-3 AUG10-0548

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LH MLG SHUTTLE VALVE32 45-21-20

AIRFRAME521

14-AUG-2009 H: 0

PN SN-UNKNOWN

RH MLG SHUTTLE VALVE32 45-21-20

AIRFRAME522

14-AUG-2009 H: 0

PN SN-UNKNOWN

NOSE LANDING GEAR (ALUM STRUT) SHOCK ABSORBER32 500

AIRFRAME523

14-AUG-2009 H: 0

2310-1100-403 00071

NOSE LANDING GEAR SHOCK ABSORBER PISTON TUBE32 501 LIFE LIMIT

AIRFRAME524

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1225-003 1219823/003

NOSE LANDING GEAR SHOCK ABSORBER BEARING32 502 LIFE LIMIT

AIRFRAME525

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1221-009 1276115/005

NOSE LANDING GEAR SHOCK ABSORBER TURNING CYLINDER32 504 LIFE LIMIT

AIRFRAME526

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1241-501 1280667/003

NOSE LANDING GEAR SHOCK ABSORBER FORK32 506 LIFE LIMIT

AIRFRAME527

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1308-501 1255989/001

NLG DRAG BRACE ASSEMBLY32 600

AIRFRAME528

14-AUG-2009 H: 0

2310-1400-403 00070

NOSE LANDING GEAR UPPER DRAG BRACE32 601 LIFE LIMIT

AIRFRAME529

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1424-501 1267270/001

NOSE LANDING GEAR LOWER DRAG BRACE32 603 LIFE LIMIT

AIRFRAME530

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1451-005 1252389/003

LEFT SIDE NLG DRAG BRACE PINTLE PIN32 605 LIFE LIMIT

AIRFRAME531

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1415-003 1257055/005

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

RIGHT SIDE NLG DRAG BRACE PINTLE PIN32 605 LIFE LIMIT

AIRFRAME532

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1415-003 1257055/007

NOSE LANDING GEAR DRAG BRACE PIN32 606 LIFE LIMIT

AIRFRAME533

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1407-001 1238815/005

LH MLG PROXIMITY SWITCH32 61-01

AIRFRAME534

14-AUG-2009 H: 0

80-057-01 21484

NLG PROXIMITY SWITCH32 61-01

AIRFRAME535

14-AUG-2009 H: 0

80-057-01 21526

RH MLG PROXIMITY SWITCH32 61-01

AIRFRAME536

14-AUG-2009 H: 0

80-057-01 21473

LH MLG PROXIMITY SWITCH32 61-02

AIRFRAME537

14-AUG-2009 H: 0

PN SN-UNKNOWN

RH MLG PROXIMITY SWITCH32 61-02

AIRFRAME538

14-AUG-2009 H: 0

PN SN-UNKNOWN

NLG LOCKING STAY ASSEMBLY32 700

AIRFRAME539

14-AUG-2009 H: 0

2310-1700-403 00068

LOWER NLG LOCKING STAY32 701 LIFE LIMIT

AIRFRAME540

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1711-001 1260461/001

UPPER NLG LOCKING STAY32 701 LIFE LIMIT

AIRFRAME541

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1722-501 1259879/008

LOWER NLG LOCKING STAY BOLT32 706 LIFE LIMIT

AIRFRAME542

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1734-001 1263791/022

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

UPPER NLG LOCKING STAY BOLT32 706 LIFE LIMIT

AIRFRAME543

14-AUG-2009 L: 7000 L: 0 L: 7000 L: 6047

2310-1734-001 1263791/011

BRAKE ACCUMULATOR32 801 LIFE LIMIT

AIRFRAME1920

L: 700 L: 0 L: 1400 L: 447

61627-A6

EXTERNAL GENERAL VISUAL INSPECTION OF THE MAINLANDING GEAR BAY

32 Z700-001300HR/48MOAIRFRAME544

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

UPPER COCKPIT LIGHTING SYSTEM CONTROL PANEL33 01-01

AIRFRAME545

14-AUG-2009 H: 0

441-40941-002 0060

FORWARD FUSELAGE BOTTOM DIMMER33 12-01

AIRFRAME546

14-AUG-2009 H: 0

81-01760-002 0063

MAIN TEST ANUNCIATOR/FIRE PANEL ASSEMBLY33 12-02

AIRFRAME547

14-AUG-2009 H: 0

441-43213-001 0062

PASSENGER-CABIN LED LIGHT DIMMER33 21-05

AIRFRAME548

14-AUG-2009 H: 0

AS-33-0038-001 0083

W001 ELECTRICAL NOSE HARNESS33 31-02

AIRFRAME549

14-AUG-2009 H: 0

PN SN-UNKNOWN

LEFT LANDING/TAXI LIGHT33 41-01

AIRFRAME550

14-AUG-2009 H: 0

81012-3 000062

RIGHT LANDING/TAXI LIGHT33 41-01

AIRFRAME551

14-AUG-2009 H: 0

81012-4 000067

LH WING POSITION/TAIL/ANTICOLLISION LIGHT33 43-01

AIRFRAME552

14-AUG-2009 H: 0

84016-1 000080

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Intervals Tolerance Time At Inst Next DueInstalled

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RH WING POSITION/TAIL/ANTICOLLISION LIGHT33 43-01

AIRFRAME553

14-AUG-2009 H: 0

84016-2 000059

DISCARD LH WING POSITION/TAIL/ANTICOLLISION LIGHT33 43-01-0017800HRAIRFRAME554

14-AUG-2009 H: 7800.00 H: +/-30 H: 0 H: 7800.00 H: 6653.30

84016-1 000080 AMM 33-43-01

DISCARD RH WING POSITION/TAIL/ANTICOLLISION LIGHT33 43-01-0017800HRAIRFRAME555

14-AUG-2009 H: 7800.00 H: +/-30 H: 0 H: 7800.00 H: 6653.30

84016-2 000059 AMM 33-43-01

GENERAL VISUAL INSPECTION LH WINGPOSITION/TAIL/ANTICOLLISION LIGHT

33 43-01-0021800HRAIRFRAME556

14-AUG-2009 H: 1800.00 H: +/-30 H: 1800.00 H: 653.30

84016-1 000080 AMM 33-43-01

GENERAL VISUAL INSPECTION RH WINGPOSITION/TAIL/ANTICOLLISION LIGHT

33 43-01-0021800HRAIRFRAME557

14-AUG-2009 H: 1800.00 H: +/-30 H: 1800.00 H: 653.30

84016-2 000059 AMM 33-43-01

FUNCTIONAL CHECK INTEGRATED ELECTRONIC STANDBYINSTRUMENT UNIT

34 11-00-001

AIRFRAME559

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

C16221ANA01 C16221017151 AMM 34-11-00

INTEGRATED ELECTRONIC STANDBY INSTRUMENT UNIT34 11-01

AIRFRAME560

14-AUG-2009 H: 0

C16221ANA01 C16221017151

PITOT-STATIC PROBE34 11-02

AIRFRAME561

09-MAY-2011H: 417.20L: 442

H: 0

101469-4-003 867888

RESTORATION OF PITOT-STATIC PROBE (CLEANING)34 11-02-00124MOAIRFRAME562

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

FUNCTIONAL CHECK OF AIR DATA SYSTEM34 15-00-00124MOAIRFRAME563

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 34-15-00

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Intervals Tolerance Time At Inst Next DueInstalled

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SPECIAL DETAILED INSPECTION OF RVSM CRITICALREGION (SKIN) FOR WAVINESS

34 15-00-00224MOAIRFRAME564

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 34-15-00

SPECIAL DETAILED INSPECTION OF STATIC PORTSURROUNDING PLATE FOR FLUSHNESS

34 15-00-00324MOAIRFRAME565

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 34-15-00

FUNCTIONAL CHECK NO. 1 GDC 74B AIR DATA COMPUTERUNIT OF AIR DATA SYSTEM

34 15-00-004 N/A

AIRFRAME566

22-SEP-2010H: 260.50L: 312

011-01110-00 43805508 AMM 34-15-00

FUNCTIONAL CHECK NO. 2 GDC 74B AIR DATA COMPUTERUNIT OF AIR DATA SYSTEM

34 15-00-004 N/A

AIRFRAME567

22-SEP-2010H: 260.50L: 312

011-01110-00 43805462 AMM 34-15-00

NO. 1 GDC 74B AIR DATA COMPUTER UNIT34 15-01

AIRFRAME568

14-AUG-2009 H: 0

011-01110-00 43805508

NO. 2 GDC 74B AIR DATA COMPUTER UNIT34 15-01

AIRFRAME569

14-AUG-2009 H: 0

011-01110-00 43805462

LH FWD PITOT TUBE34 15-03

AIRFRAME570

14-SEP-2010H: 260.50L: 312

H: 0

0851LP 265326

RH FWD PITOT TUBE34 15-03

AIRFRAME571

14-SEP-2010H: 260.50L: 312

H: 0

0851LP 265324

RESTORATION OF PITOT PROBE (CLEANING)34 15-03-00124MOAIRFRAME572

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

LH FWD DUAL STATIC PORT34 15-05

AIRFRAME573

13-SEP-2011H: 504.20L: 504

H: 0

100442-106 809446

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Intervals Tolerance Time At Inst Next DueInstalled

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RH FWD DUAL STATIC PORT34 15-05

AIRFRAME574

13-SEP-2011H: 504.20L: 504

H: 0

100442-107 806642

LH ATTITUDE AND HEADING REFERENCE UNIT34 21-01

AIRFRAME575

14-AUG-2009 H: 0

011-00868-10 42011051

RH ATTITUDE AND HEADING REFERENCE UNIT34 21-01

AIRFRAME576

14-AUG-2009 H: 0

011-00868-10 42011556

LH WING MAGNETOMETER34 21-02

AIRFRAME577

14-AUG-2009 H: 0

011-00870-00 47513046

RH WING MAGNETOMETER34 21-02

AIRFRAME578

14-AUG-2009 H: 0

011-00870-00 47513033

FUNCTIONAL CHECK MAGNETIC COMPASS34 23-00-001

AIRFRAME579

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

KCA0120W BB8781008 AMM 34-23-00

MAGNETIC COMPASS34 23-01

AIRFRAME580

14-AUG-2009 H: 0

KCA0120W BB8781008

TAIL PHASING COUPLER34 32-01

AIRFRAME581

14-AUG-2009 H: 0

SSPD-113-10 5690

LEFT VOR/LOC 2&3 ANTENNA BLADE34 32-03

AIRFRAME582

14-AUG-2009 H: 0

S65-247170 8433

RIGHT VOR/LOC 2&3 ANTENNA BLADE34 32-03

AIRFRAME583

14-AUG-2009 H: 0

S65-247170 8424

LW FWR MARKER BEACON ANTENNA34 32-04

AIRFRAME584

14-AUG-2009 H: 0

S35-1000-2 102-7883

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Intervals Tolerance Time At Inst Next DueInstalled

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WEATHER RADAR ANTENNA34 42-01

AIRFRAME585

13-SEP-2011H: 504.20L: 504

H: 0

011-00883-20 47203716

BAGGAGE COMPARTMENT GTS 850 TRAFFIC PROCESSOR UNIT34 43-01

AIRFRAME586

14-AUG-2009 H: 0

PN SN-UNKNOWN

TRC899 TRANSMITTER RECEIVER COMPUTER34 43-02

AIRFRAME587

14-AUG-2009 H: 0

PN SN-UNKNOWN

LOWER DIRECTIONAL ANTENNA34 43-05

AIRFRAME588

14-AUG-2009 H: 0

PN SN-UNKNOWN

UPPER DIRECTIONAL ANTENNA34 43-05

AIRFRAME589

14-AUG-2009 H: 0

PN SN-UNKNOWN

LOW NOISE (TCAS) POWER AMPLIFIER34 43-08

AIRFRAME590

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.1 CENTER DISTANCE MEASURING EQUIP UNIT34 51-01

AIRFRAME591

14-AUG-2009 H: 0

066-01070-0001 31083

NO.2 CENTER DISTANCE MEASURING EQUIP UNIT34 51-01

AIRFRAME592

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO. 1 DME L BAND ANTENNA34 51-02

AIRFRAME593

14-AUG-2009 H: 0

S65-5366-7L 261-83003

NO. 2 DME L BAND ANTENNA34 51-02

AIRFRAME594

14-AUG-2009 H: 0

S65-5366-7L 261-82985

FUNCTIONAL CHECK NO. 1 TRANSPONDER SYSTEM34 52-00-001

AIRFRAME595

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 34-52-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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FUNCTIONAL CHECK NO. 2 TRANSPONDER SYSTEM34 52-00-001

AIRFRAME596

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

AMM 34-52-00

LH MODE S GTX33 TRANSPONDER MODULE34 52-01

AIRFRAME597

14-AUG-2009 H: 0

011-00779-10 89108699

RH TRANSPONDER (DIVERSITY) MODULE34 52-01

AIRFRAME598

14-AUG-2009 H: 0

011-00779-01 84805530

BOTTOM TRANSPONDOR 1 L BAND ANTENNA34 52-02

AIRFRAME599

14-AUG-2009 H: 0

PN SN-UNKNOWN

TOP TRANSPONDOR 2 L BAND ANTENNA34 52-02

AIRFRAME600

14-AUG-2009 H: 0

S65-5366-7L 261-82940

COAXIAL SWITCH34 52-04

AIRFRAME601

14-AUG-2009 H: 0

D2-729B005 554549

LH TOP CENTER GPS WAAS - GA 36 ANTENNA34 56-02

AIRFRAME602

14-AUG-2009 H: 0

013-00244-00 6039

RH TOP CENTER WAAS & SATELLITE WEATHER AND RADARANTENNA

34 56-02

AIRFRAME603

14-AUG-2009 H: 0

013-00245-00 6217

SATELLITE WEATHER AND RADIO RECIEVER34 57-01

AIRFRAME604

14-AUG-2009 H: 0

011-00987-00 47761653

FLIGHT MANAGEMENT SYSTEM PANEL34 61-01

AIRFRAME605

14-AUG-2009 H: 0

011-01054-10 21805239

FUNCTIONAL CHECK INTEGRATED ELECTRONIC STANDBYINSTRUMENT UNIT (FAR 91.411)

34 FAR01 FAR

AIRFRAME606

12-SEP-2013H: 786.90L: 722

M: 24 12-SEP-2015 M: 7 D: 9

C16221ANA01 C16221017151 FAR 91.411

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Intervals Tolerance Time At Inst Next DueInstalled

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FUNCTIONAL CHECK OF AIR DATA SYSTEM (FAR91.411)

34 FAR02 FAR

AIRFRAME607

12-SEP-2013H: 786.90L: 722

M: 24 12-SEP-2015 M: 7 D: 9

FAR 91.411

FUNCTIONAL CHECK STATIC PRESSURE (FAR 43APPENDIX E)

34 FAR03 FAR

AIRFRAME608

12-SEP-2013H: 786.90L: 722

M: 24 12-SEP-2015 M: 7 D: 9

FAR PART 43 APPENDIX E

FUNCTIONAL CHECK NO. 1 TRANSPONDER SYSTEM (FAR91.413)

34 FAR04 FAR

AIRFRAME609

12-SEP-2013H: 786.90L: 722

M: 24 12-SEP-2015 M: 7 D: 9

FAR 91.413

FUNCTIONAL CHECK NO. 2 TRANSPONDER SYSTEM (FAR91.413)

34 FAR04 FAR

AIRFRAME610

12-SEP-2013H: 786.90L: 722

M: 24 12-SEP-2015 M: 7 D: 9

FAR 91.413

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE AHRS

34H34-01-220-001 6000HR/96MO

AIRFRAME611

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 34-21-01

GENERAL VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE MAGNETOMETER

34H34-02-551-001 4800HR/72MO

AIRFRAME612

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 34-21-02

GENERAL VISUAL INSPECTION RIGHT L/HIRF PROTECTIONON THE MAGNETOMETER

34H34-02-551-001 4800HR/72MO

AIRFRAME613

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 34-21-02

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE PITOT-STATIC PROBE

34H34-03-224-001 4800HR/72MO

AIRFRAME614

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 34-11-02

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE AIR DATA COMPUTER

34H34-04-220-001 6000HR/96MO

AIRFRAME615

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 34-15-01

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE STATIC PORT

34H34-05-220-001 4800HR/72MO

AIRFRAME616

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 34-15-05

GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE PITOT PROBE

34H34-06-220-001 4800HR/72MO

AIRFRAME617

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 34-15-03

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Intervals Tolerance Time At Inst Next DueInstalled

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GENERAL VISUAL INSPECTION OF THE L/HIRFPROTECTION ON THE INTEGRATED ELECTRONIC STANDBYINSTRUMENT UNIT

34H34-07-220-001 6000HR/96MO

AIRFRAME618

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 34-11-01

PERFORM VOR ACCURACY CHECK (FAR 91.171)34 VOR-01-1 MANDATORY

AIRFRAME558

D: 30

FAR 91.171

FUNCTIONAL CHECK OF OXYGEN SYSTEM PRESSURE LINESFOR LEAKAGE

35 00-00-001 AIRWORTHINESS

AIRFRAME619

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-00-00

FUNCTIONAL CHECK OF CREW OXYGEN PRESSUREINDICATION

35 01-00-00160MOAIRFRAME620

14-SEP-2014H: 1038.80L: 883

M: 60 D: +/-30 14-SEP-2019 M: 55 D: 11

AMM 35-01-02

OXYGEN CYLINDER PRESSURE AND TEMPERATURETRANSDUCER

35 01-02

AIRFRAME621

14-AUG-2009 H: 0

4441125-000 7470-2-267

OXYGEN SYSTEM LOW PRESSURE SWITCH35 01-05

AIRFRAME622

14-AUG-2009 H: 0

4421134-000 0110

LH CSL OXYGEN SYSTEM CONTROL PANEL35 01-06

AIRFRAME623

14-AUG-2009 H: 0

441-40945-002 0079

OXYGEN SYSTEM CABIN ALTITUDE SWITCH35 01-07

AIRFRAME624

14-AUG-2009 H: 0

4421133-000 0837061

CENTER FUSELAGE ALTITUDE COMPENSATING REGULATOR35 01-09

AIRFRAME625

14-AUG-2009 H: 0

4421135-000 00078

OXYGEN LOW PRESSURE 3 POSITION VALVE35 01-10

AIRFRAME626

14-AUG-2009 H: 0

4421132-109 00065

50 CU.FT OXYGEN CYLINDER35 02-01

AIRFRAME627

14-AUG-2009 H: 0

4441122-050 0115-1036

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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FUNCTIONAL CHECK (HYDROSTATIC TEST) 50 CU.FTOXYGEN CYLINDER

35 02-01-001

AIRFRAME628

30-APR-2014H: 964.40L: 833

M: 60 D: +/-30 M: -7D: -1

29-SEP-2018 M: 43 D: 26

4441122-050 0115-1036 AMM 35-02-01

RESTORE 50 CU.FT OXYGEN CYLINDER REGULATOR35 02-01-002

AIRFRAME629

30-APR-2014H: 964.40L: 833

M: 60 D: +/-30 M: 7D: -1

29-SEP-2018 M: 43 D: 26

4441122-050 585815601 AMM 35-02-01

DISCARD 50 CU.FT OXYGEN CYLINDER35 02-01-003

AIRFRAME630

31-DEC-2008 M: 180 D: +/-30 M: 0 31-DEC-2023 M: 106 D: 28

4441122-050 0115-1036 AMM 35-02-01

OPERATIONAL CHECK OF CREW OXYGEN MASKS ANDSTOWAGE BOX

35 11-00-001

AIRFRAME631

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

D: +/-30H: +/-30

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-11-02

LH CREW OXYGEN-MASK STOWAGE BOX35 11-01

AIRFRAME632

14-AUG-2009 H: 0

1186F6-23 00155

RH CREW OXYGEN-MASK STOWAGE BOX35 11-01

AIRFRAME633

14-AUG-2009 H: 0

1186F6-23 00146

LH CREW MASK SWEEP35 11-02

AIRFRAME634

14-AUG-2009 H: 0

174232-93 23319

RH CREW MASK SWEEP35 11-02

AIRFRAME635

14-AUG-2009 H: 0

174232-93 26257

DETAILED VISUAL INSPECTION LH CREW MASK SWEEP35 11-02-001

AIRFRAME636

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

D: +/-30H: +/-30

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-11-02

DETAILED VISUAL INSPECTION RH CREW MASK SWEEP35 11-02-001

AIRFRAME637

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

D: +/-30H: +/-30

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-11-02

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RESTORATION LH CREW MASK SWEEP35 11-02-002

AIRFRAME638

14-AUG-2009 M: 72 D: +/-30 M: 0 14-AUG-2015 M: 6 D: 11

174232-93 23319

RESTORATION RH CREW MASK SWEEP35 11-02-002

AIRFRAME639

14-AUG-2009 M: 72 D: +/-30 M: 0 14-AUG-2015 M: 6 D: 11

174232-93 26257

DETAILED VISUAL INSPECTION OF CREW GOGGLES35 11-04-001

AIRFRAME640

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

D: +/-30H: +/-30

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-11-04

FUNCTIONAL CHECK OF PASSENGER OXYGEN SYSTEM INAUTO MODE

35 21-00-001 AIRWORTHINESS

AIRFRAME641

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-21-00

OPERATIONAL CHECK OF PASSENGER OXYGEN SYSTEM INMANUAL MODE

35 21-00-002 AIRWORTHINESS

AIRFRAME642

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-21-00

PAX 1 OXYGEN MASK35 21-01

AIRFRAME643

14-AUG-2009 H: 0

PN SN-UNKNOWN

PAX 2 OXYGEN MASK35 21-01

AIRFRAME644

14-AUG-2009 H: 0

PN SN-UNKNOWN

PAX 3 OXYGEN MASK35 21-01

AIRFRAME645

14-AUG-2009 H: 0

PN SN-UNKNOWN

PAX 4 OXYGEN MASK35 21-01

AIRFRAME646

14-AUG-2009 H: 0

PN SN-UNKNOWN

DETAILED VISUAL INSPECTION OF PASSENGER OXYGENMASKS

35 21-01-001

AIRFRAME647

20-SEP-2012H: 662.00L: 637

M: 36H: 1800.00

D: +/-30H: +/-30

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

AMM 35-21-01

CABIN OXYGEN THREE MASK DEPLOYMENT CONTAINER35 21-02

AIRFRAME648

14-AUG-2009 H: 0

4411073-001 4411073-001-00007

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Intervals Tolerance Time At Inst Next DueInstalled

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LH OXYGEN TWO MASK DEPLOYMENT CONTAINER35 21-02

AIRFRAME649

14-AUG-2009 H: 0

4411072-001 4411072-001-00145

RH OXYGEN TWO MASK DEPLOYMENT CONTAINER35 21-02

AIRFRAME650

14-AUG-2009 H: 0

4411072-001 4411072-001-00156

CREW PBE35 31-01

AIRFRAME651

14-AUG-2009 H: 0

MR-10022NEMB E0901886

DISCARD CREW PBE35 31-01-001

AIRFRAME652

14-AUG-2009 M: 126 D: +/-30 M: 0 14-AUG-2019 M: 54 D: 11

MR-10022NEMB E0901886 AMM 35-31-01

OPERATIONAL CHECK LH PYLON PRESSURE REGULATINGSHUTOFF VALVE

36 11-00-001600HRAIRFRAME653

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

1330310-1 169 AMM 36-11-00

OPERATIONAL CHECK RH PYLON PRESSURE REGULATINGSHUTOFF VALVE

36 11-00-001600HRAIRFRAME654

14-SEP-2014H: 1038.80L: 883

H: 600.00 H: +/-30 H: 1638.80 H: 492.10

1330310-1 160 AMM 36-11-00

LH PYLON PRESSURE REGULATING SHUTOFF VALVE36 11-01

AIRFRAME655

27-JUN-2011H: 467.90L: 483

H: 0

1330310-1 169

RH PYLON PRESSURE REGULATING SHUTOFF VALVE36 11-01

AIRFRAME656

14-AUG-2009 H: 0

1330310-1 160

DETAILED INSPECTION OF BLEED LINE WATER DRAINS36 11-02-0011200HR/24MOAIRFRAME1930

M: 24H: 1200.00

D: 30 H: 30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

AMM 36-11-02-210-802-A/600

OPERATIONAL CHECK OF BLEED LEAKAGE SENSORS36 21-01-001 AIRWORTHINESS

AIRFRAME657

14-AUG-2009 H: 6000.00 H: 6000.00 H: 4853.30

AMM 36-21-01

DC CONVERTER44 24-21-03

AIRFRAME658

14-AUG-2009 H: 0

PN SN-UNKNOWN

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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OPTIONAL DOOR EQUIPPED STEP ASSEMBLY52 10-00

AIRFRAME659

14-AUG-2009 H: 0

PN SN-UNKNOWN

EXTERNAL GENERAL VISUAL INSPECTION MAIN PAX DOORASSEMBLY STRUCTURE

52 10-01-00148MOAIRFRAME660

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

500-09910-443 0000499668 NDT PART 5 52-10-00

INTERNAL GENERAL VISUAL INSPECTION MAIN PAX DOORASSEMBLY STRUCTURE

52 10-01-002

AIRFRAME661

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

500-09910-443 0000499668 NDT PART 5 52-10-00

INTERNAL DETAILED VISUAL INSPECTION MAIN DOORSTRUCTURE UPPER EXTERNAL FRAME, UPPER HORIZONTALSTRINGER, EXTERNAL VERTICAL FRAME, AND LOWERHORIZONTAL FRAME.

52 10-01-01-901 AIRWORTHINESS

AIRFRAME662

L: 17500 L: 17500 L: 16547

NDT PART 5 52-10-00

EXTERNAL DETAILED VISUAL INSPECTION MAIN DOORSTRUCTURE DOOR SKIN, VENT FLAP SKIN AND SKIN/VENTFLAP SKIN FASTENER.

52 10-01-01-902 AIRWORTHINESS

AIRFRAME663

L: 17500 L: 17500 L: 16547

NDT PART 5 52-10-00

INTERNAL DETAILED VISUAL INSPECTION MAIN DOORLATCH MECHANISM LATCH PINS.

52 10-02-01-901 AIRWORTHINESS

AIRFRAME664

L: 17500 L: 17500 L: 16547

NDT PART 5 52-10-00

GENERAL VISUAL INSPECTION MAIN PAX DOOR ASSEMBLY RUBBER SEAL

52 10-20-0011200HR/24MOAIRFRAME665

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

500-09910-443 0000499668 AMM 52-10-20

MAIN PAX DOOR ASSEMBLY52 11-00

AIRFRAME666

14-AUG-2009 H: 0

500-09910-443 0000499668

GENERAL VISUAL INSPECTION MAIN PAX DOOR ASSEMBLY LOCKING AND ACTUATING MECHANISM

52 11-00-001300HR/48MOAIRFRAME667

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

500-09910-443 0000499668 AMM 52-11-00

LUBRICATION OF MAIN DOOR LATCH PINS52 11-00-002 LUB12MOAIRFRAME1905

14-SEP-2014H: 1038.80L: 883

M: 12 14-SEP-2015 M: 7 D: 11

AMM 52-11-21-640-801-A/300

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Intervals Tolerance Time At Inst Next DueInstalled

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DOOR KEY LOCK KIT52 11-01

AIRFRAME668

14-AUG-2009 H: 0

500-38850-901 100012-10012

MAIN DOOR BALANCE ASSEMBLY52 13-00

AIRFRAME669

14-AUG-2009 H: 0

PN SN-UNKNOWN

DISCARD MAIN DOOR BALANCE ASSEMBLY GEAR SECTOR52 13-21-0016000HRAIRFRAME670

14-AUG-2009 H: 6000.00 H: +/-30 H: 0 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 52-13-21

DISCARD MAIN DOOR BALANCE ASSEMBLY MECHANISMCABLE

52 13-22-0021800HRAIRFRAME671

14-AUG-2009 H: 1800.00 H: +/-30 H: 0 H: 1800.00 H: 653.30

PN0 SN-UNKNOWN AMM 52-13-22

DISCARD MAIN DOOR BALANCE ASSEMBLY PINION SHAFT52 13-23-0016000HRAIRFRAME672

14-AUG-2009 H: 6000.00 H: +/-30 H: 0 H: 6000.00 H: 4853.30

PN SN-UNKNOWN AMM 52-13-23

INTERNAL DETAILED VISUAL INSPECTION EMERGENCYDOOR STRUCTURE SPAR AND FRAMES.

52 20-01-01-901 AIRWORTHINESS

AIRFRAME673

L: 17500 L: 17500 L: 16547

NDT PART 5 52-20-00

EXTERNAL - DETAILED INSPECTION EMERGENCY DOORSTRUCTURE DOOR SKIN, VENT FLAP SKIN AND SKIN/VENTFLAP SKIN FASTENER.

52 20-01-01-902 AIRWORTHINESS

AIRFRAME674

L: 17500 L: 17500 L: 16547

NDT PART 5 52-20-00

GENERAL VISUAL INSPECTION CENTER FUSELAGEEMERGENCY DOOR ASSEMBLY LOCKING AND ACTUATINGMECHANISM

52 20-20-001300HR/48MOAIRFRAME675

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

500-09700-417 0000504301 AMM 52-20-20

CENTER FUSELAGE EMERGENCY DOOR ASSEMBLY52 20-21

AIRFRAME676

14-AUG-2009 H: 0

500-09700-417 0000504301

GENERAL VISUAL INSPECTION CENTER FUSELAGEEMERGENCY DOOR ASSEMBLY RUBBER SEAL

52 20-21-0011200HR/24MOAIRFRAME677

12-SEP-2013H: 786.90L: 722

M: 24H: 1200.00

D: +/-30H: +/-30

12-SEP-2015H: 1986.90

M: 7 D: 9H: 840.20

500-09700-417 0000504301 AMM 52-20-21

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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GENERAL VISUAL INSPECTION OF FORWARD BAGGAGE DOORLOCKING AND ACTUATING MECHANISM

52 31-20-001300HR/48MOAIRFRAME678

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 52-31-20

GENERAL VISUAL INSPECTION OF AFT BAGGAGE DOORLOCKING ACTUATING MECHANISM

52 32-20-001300HR/48MOAIRFRAME679

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

AMM 52-32-20

LOWER DOOR MICRO SWITCH52 71-20

AIRFRAME680

14-AUG-2009 H: 0

500-38876-401 0000497145

UPPER DOOR MICRO SWITCH52 71-20

AIRFRAME681

14-AUG-2009 H: 0

500-38876-401 0000498502

EXTERNAL GENERAL VISUAL INSPECTION OF FUSELAGEPOLYURETHANE FILMS

53 00-00-00112MOAIRFRAME682

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 53-00-20

DETAILED VISUAL INSPECTION OF FUSELAGE DRAINS53 05-00-001600HR/12MOAIRFRAME683

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 53-05-00

INTERNAL DETAILED VISUAL INSPECTION OF FORWARDFUSELAGE LOWER SKIN PANEL AND COCKPIT FLOORSTRUCTURES

53 10-00-001

AIRFRAME684

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-10-00

INTERNAL DETAILED VISUAL INSPECTION OF FORWARDFUSELAGE SKIN PANELS, SKIN SPLICES AND WINDSHIELDCUTOUT STRUCTURE

53 10-00-002

AIRFRAME685

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-10-00

INTERNAL DETAILED INSPECTION FORWARD FUSELAGEUPPER SKIN PANEL AND WINDSHIELD CUTOUT STRUCTUREMACHINE FR07, BEAMS, POSTS, GUSSET (SPLICES)

53 10-01-01-901 AIRWORTHINESS

AIRFRAME686

L: 6300 L: 6300 L: 5347

NDT PART 5 53-10-00

INTERNAL DETAILED INSPECTION FORWARD FUSELAGEUPPER SKIN PANEL AND WINDSHIELD CUTOUT STRUCTUREMACHINE FR07, BEAMS, POSTS, GUSSET (SPLICES).

53 10-01-01-902 AIRWORTHINESS

AIRFRAME687

L: 14000 L: 14000 L: 13047

NDT PART 5 53-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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EXTERNAL - DETAILED INSPECTION FORWARD FUSELAGEUPPER SKIN PANEL AND WINDSHIELD CUTOUT STRUCTURESKIN PANEL AND FASTENERS.

53 10-01-01-903 AIRWORTHINESS

AIRFRAME688

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

INTERNAL GENERAL VISUAL INSPECTION FORWARDFUSELAGE LEFT AND RIGHT SIDE SKIN PANELS FRAMESAND SPLICES.

53 10-02-01-901 AIRWORTHINESS

AIRFRAME689

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL - DETAILED INSPECTION FORWARD FUSELAGELEFT AND RIGHT SIDE SKIN PANELS SKIN-TO-FRAMESAREA.

53 10-02-01-902 AIRWORTHINESS

AIRFRAME690

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

INTERNAL GENERAL VISUAL INSPECTION FORWARDFUSELAGE LEFT AND RIGHT SIDE SKIN PANELSSTRINGERS.

53 10-02-02-901 AIRWORTHINESS

AIRFRAME691

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL - DETAILED INSPECTION FORWARD FUSELAGELEFT AND RIGHT SIDE SKIN PANELS SKIN-TO-STRINGERSAREA.

53 10-02-02-902 AIRWORTHINESS

AIRFRAME692

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

INTERNAL GENERAL VISUAL INSPECTION FORWARDFUSELAGE LOWER SKIN PANEL FRAMES AND STRINGERS.

53 10-03-01-901 AIRWORTHINESS

AIRFRAME693

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL - DETAILED INSPECTION FORWARD FUSELAGELOWER SKIN PANEL SKIN-TO-FRAME/STRINGERS AREA.

53 10-03-01-902 AIRWORTHINESS

AIRFRAME694

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

INTERNAL DETAILED INSPECTION FORWARD FUSELAGELONGITUDINAL AND CIRCUMFERENTIAL SKIN SPLICESLONGITUDINAL SPLICE

53 10-04-01-901 AIRWORTHINESS

AIRFRAME695

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL - DETAILED INSPECTION FORWARD FUSELAGELONGITUDINAL AND CIRCUNFERENTIAL SKIN SPLICES -SKIN-TO-LONGITUDINAL SPLICE AREA.

53 10-04-01-902 AIRWORTHINESS

AIRFRAME696

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INTERNAL DETAILED INSPECTION FORWARD FUSELAGELONGITUDINAL AND CIRCUNFERENTIAL SKIN SPLICESCIRCUMFERENTIAL SPLICE.

53 10-04-02-901 AIRWORTHINESS

AIRFRAME697

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL - DETAILED INSPECTION FORWARD FUSELAGELONGITUDINAL AND CIRCUNFERENTIAL SKIN SPLICESSKIN-TO-CIRCUMFERENTIAL-SPLICE AREA.

53 10-04-02-902 AIRWORTHINESS

AIRFRAME698

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL DETAILED VISUAL INSPECTION OF FORWARDFUSELAGE PRESSURE BULKHEAD

53 10-05-001

AIRFRAME699

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-10-00

INTERNAL DETAILED VISUAL INSPECTION OF FORWARDFUSELAGE PRESSURE BULKHEAD

53 10-05-002

AIRFRAME700

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-10-00

INTERNAL GENERAL VISUAL INSPECTION FORWARDFUSELAGE PRESSURE BULKHEAD.

53 10-05-01-901 AIRWORTHINESS

AIRFRAME701

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

INTERNAL DETAILED VISUAL INSPECTION OF FORWARDFUSELAGE FORWARD SKIN PANELS

53 10-06-002

AIRFRAME702

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-10-00

EXTERNAL GENERAL VISUAL INSPECTION OF NOSELANDING GEAR WHEELWELL METALLIC STRUCTURE

53 10-07-00124MOAIRFRAME703

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

NDT PART 5 53-10-00

EXTERNAL SPECIAL DETAILED INSPECTION NOSE LANDINGGEAR WHEEL WEEL METALLIC STRUCTURE (EDDYCURRENT) TRUNION.

53 10-07-01-901 AIRWORTHINESS

AIRFRAME704

L: 17500 L: 17500 L: 16547

NDT PART 6 53-10-00

EXTERNAL - DETAILED INSPECTION NOSE LANDING GEARWHEEL WEEL METALLIC STRUCTURE.

53 10-07-02-901 AIRWORTHINESS

AIRFRAME705

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

EXTERNAL SPECIAL DETAILED INSPECTION NOSE LANDINGGEAR WHEEL WEEL METALLIC STRUCTURE (EDDYCURRENT) DRAG LOCKING STRUTS.

53 10-07-02-902 AIRWORTHINESS

AIRFRAME706

L: 17500 L: 17500 L: 16547

NDT PART 6 53-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL GENERAL VISUAL INSPECTION OF NOSELANDING GEAR WHEELWELL COMPOSITE STRUCTURE

53 10-08-00296MOAIRFRAME707

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 53-10-00

EXTERNAL - DETAILED INSPECTION NOSE LANDING GEARWEEL COMPOSITE STRUCTURE UPPER PANEL AND SIDESKIN.

53 10-08-01-901 AIRWORTHINESS

AIRFRAME708

L: 17500 L: 17500 L: 16547

NDT PART 5 53-10-00

NOSE RADOME53 14-00

AIRFRAME709

14-AUG-2009 H: 0

5190-102-1 124

EXTERNAL DETAILED VISUAL INSPECTION OF CENTERFUSELAGE SKIN PANELS AND SKIN SPLICES

53 20-00-001

AIRFRAME710

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-20-00

INTERNAL DETAILED VISUAL INSPECTION OF CENTERFUSELAGE SKIN PANELS, SKIN SPLICES, AND FLOORSTRUCTURE

53 20-00-002

AIRFRAME711

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-20-00

EXTERNAL DETAILED VISUAL INSPECTION OF CENTERFUSELAGE-TO-WING LATERAL AND CENTER LINKS

53 20-00-003

AIRFRAME712

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION CENTERFUSELAGE UPPER SKIN PANEL (FROM FRAME 8 TO 19 ANDFROM STRINGER 1R TO 6L) FRAMES.

53 20-01-01-901 AIRWORTHINESS

AIRFRAME713

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGEUPPER SKIN PANEL (FROM FRAME 8 TO 19 AND FROMSTRINGER 1R TO 6L) SKIN TO FRAMES AREA.

53 20-01-01-902 AIRWORTHINESS

AIRFRAME714

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION CENTERFUSELAGE UPPER SKIN PANEL (FROM STRINGER 1R TO 6LAND FROM FRAME 8 TO 19) STRINGERS.

53 20-01-02-901 AIRWORTHINESS

AIRFRAME715

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

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Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

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EXTERNAL - DETAILED INSPECTION CENTER FUSELAGEUPPER SKIN PANEL (FROM STRINGER 1R TO 6L AND FROMFRAME 8 TO 19) SKIN TO STRINGERS AREA.

53 20-01-02-902 AIRWORTHINESS

AIRFRAME716

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION CENTERFUSELAGE SIDE SKIN PANEL (FROM FRAME 8 TO 19 ANDFROM STRINGER 2R TO 11R) FRAMES.

53 20-02-01-901 AIRWORTHINESS

AIRFRAME717

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGESIDE SKIN PANEL (FROM FRAME 8 TO 19 AND FROMSTRINGER 2R TO 11R) SKIN TO FRAMES AREA.

53 20-02-01-902 AIRWORTHINESS

AIRFRAME718

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION CENTERFUSELAGE SIDE SKIN PANEL (FROM STRINGER 2R TO 11RAND FROM FRAME 8 TO 19) STRINGERS.

53 20-02-02-901 AIRWORTHINESS

AIRFRAME719

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGESIDE SKIN PANEL (FROM STRINGER 2R TO 11R AND FROMFRAME 8 TO 19) SKIN TO STRINGERS AREA.

53 20-02-02-902 AIRWORTHINESS

AIRFRAME720

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION CENTERFUSELAGE LOWER SKIN PANEL (FROM STRINGER 7L TO12R AND FROM FRAME 8 TO 19) CUT-OUT REINFORCEMENT(SKIN DOUBLER).

53 20-03-01-901 AIRWORTHINESS

AIRFRAME721

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGELOWER SKIN PANEL (FROM STRINGER 7L TO 12R ANDFROM FRAME 8 TO 19) SKIN TO CUT-OUT AREA.

53 20-03-01-902 AIRWORTHINESS

AIRFRAME722

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION CENTERFUSELAGE LOWER SKIN PANEL (FROM STRINGER 7L TO12R AND FROM FRAME 8 TO 19) FRAMES AND STRINGERS.

53 20-03-02-901 AIRWORTHINESS

AIRFRAME723

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGELOWER SKIN PANEL (FROM STRINGER 7L TO 12R ANDFROM FRAME 8 TO 19) SKIN TO FRAMES AND STRINGERSAREA.

53 20-03-02-902 AIRWORTHINESS

AIRFRAME724

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

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Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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INTERNAL DETAILED INSPECTION CENTER FUSELAGELONGITUDINAL LAP JOINT SKIN SPLICE ANDCIRCUMFERENTIAL SKIN SPLICE LONGITUDINAL LAP JOINTSKIN SPLICE.

53 20-04-01-901 AIRWORTHINESS

AIRFRAME725

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGELONGITUDINAL LAP JOINT SKIN SPLICE ANDCIRCUMFERENTIAL SKIN SPLICE LONGITUDINAL LAP JOINTSKIN SPLICE.

53 20-04-01-902 AIRWORTHINESS

AIRFRAME726

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION CENTER FUSELAGELONGITUDINAL LAP JOINT SKIN SPLICE ANDCIRCUMFERENTIAL SKIN SPLICE CIRCUNFERENTIAL SKINSPLICE.

53 20-04-02-901 AIRWORTHINESS

AIRFRAME727

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGELONGITUDINAL LAP JOINT SKIN SPLICE ANDCIRCUMFERENTIAL SKIN SPLICE SKIN ATCIRCUMFERENTIAL SKIN SPLICE AREA.

53 20-04-02-902 AIRWORTHINESS

AIRFRAME728

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED VISUAL INSPECTION OF CENTERFUSELAGE CIRCUMFERENTIAL SKIN SPLICES AND ENDFITTINGS

53 20-05-002

AIRFRAME729

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION CENTER FUSELAGE TOAFT FUSELAGE CIRCUMFERENTIAL SKIN SPLICES AND ENDFITTINGS SKIN (FROM STRINGER 12L TO 12R).

53 20-05-01-901 AIRWORTHINESS

AIRFRAME730

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL SPECIAL DETAILED INSPECTION CENTERFUSELAGE TO AFT FUSELAGE CIRCUMFERENTIAL SKINSPLICES AND END FITTINGS (EDDY CURRENT) SPLICE(1ST AND 3RD ROWS) (FROM STRINGER 01R TO 01L,FROM STINGER 04R TO 07R AND FROM STRINGER 04L TO07L).

53 20-05-01-902 AIRWORTHINESS

AIRFRAME731

L: 17500 L: 17500 L: 16547

NDT PART 6 53-20-00

EXTERNAL - DETAILED INSPECTION CENTER FUSELAGE TOAFT FUSELAGE CIRCUMFERENTIAL SKIN SPLICES AND ENDFITTINGS SKIN (FROM STRINGER 01R TO 01L, FROMSTRINGER 04R TO 07R AND FROM STRINGER 04L TO07L).

53 20-05-01-903 AIRWORTHINESS

AIRFRAME732

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION CENTER FUSELAGE TOAFT FUSELAGE CIRCUMFERENTIAL SKIN SPLICES ENDFITTINGS

53 20-05-01-904 AIRWORTHINESS

AIRFRAME733

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

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Intervals Tolerance Time At Inst Next DueInstalled

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EXTERNAL GENERAL VISUAL INSPECTION OF MAIN DOORCUTOUT STRUCTURE

53 20-06-00148MOAIRFRAME734

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 53-20-00

INTERNAL DETAILED VISUAL INSPECTION OF MAIN DOORCUTOUT STRUCTURE

53 20-06-00248MOAIRFRAME735

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 53-20-00

EXTERNAL SPECIAL DETAILED INSPECTION (EDDYCURRENT) THE DOUBLER 1 AT CORNERS OF MAIN DOORCUTOUT STRUCTURE.

53 20-06-01-901 AIRWORTHINESS

AIRFRAME736

L: 17500 L: 17500 L: 16547

NDT PART 6 53-20-00

EXTERNAL SPECIAL DETAILED INSPECTION (EDDYCURRENT) THE SKIN AT CORNERS OF THE MAIN DOORCUTOUT STRUCTURE.

53 20-06-01-902 AIRWORTHINESS

AIRFRAME737

L: 17500 L: 17500 L: 16547

NDT PART 6 53-20-00

EXTERNAL - DETAILED INSPECTION THE MAIN DOORCUTOUT STRUCTURE SKIN TO DOOR CUTOUT STRUCTURE.

53 20-06-01-903 AIRWORTHINESS

AIRFRAME738

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION THE MAIN DOORCUT-OUT STRUCTURE.

53 20-06-01-904 AIRWORTHINESS

AIRFRAME739

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION MAIN DOOR CUTOUTSTRUCTURE MACHINED FRAME AT LATCH PIN BOX AREA .

53 20-06-01-905 AIRWORTHINESS

AIRFRAME740

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL GENERAL VISUAL INSPECTION OF EMERGENCYDOOR CUTOUT STRUCTURE

53 20-07-00148MOAIRFRAME741

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION OF EMERGENCYDOOR CUTOUT STRUCTURE

53 20-07-00248MOAIRFRAME742

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 53-20-00

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INTERNAL GENERAL VISUAL INSPECTION EMERGENCY DOORCUTOUT STRUCTURE (FROM STRINGER 3R TO 7R AND FROMFRAME 14 TO 16)

53 20-07-01-901 AIRWORTHINESS

AIRFRAME743

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION THE SKIN TOEMERGENCY DOOR CUTOUT STRUCTURE (FROM STRINGER 3RTO 7R AND FROM FRAME 14 TO 16)

53 20-07-01-902 AIRWORTHINESS

AIRFRAME744

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL GENERAL VISUAL INSPECTION PASSENGERWINDOW CUTOUT STRUCTURE PASSENGER WINDOW FRAME(FROM STRINGER 4L TO 6L AND STRINGER 4R TO 6R ANDFROM FRAME 10 TO 18)

53 20-08-01-901 AIRWORTHINESS

AIRFRAME745

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL - DETAILED INSPECTION PASSENGER WINDOWCUTOUT STRUCTURE PASSENGER (FROM STRINGER 4L TO6L AND STRINGER 4R TO 6R AND FROM FRAME 10 TO 18)SKIN AT WINDOW AREA.

53 20-08-01-902 AIRWORTHINESS

AIRFRAME746

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION CENTERFUSELAGE-TO-WING LATERAL LINKS.

53 20-10-01-901 AIRWORTHINESS

AIRFRAME747

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION CENTERFUSELAGE-TO-WING LATERAL LINKS MACHINED FRAME(FRAME 14 AND FRAME 18) AND FASTENERS

53 20-10-01-902 AIRWORTHINESS

AIRFRAME748

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL SPECIAL DETAILED INSPECTION CENTERFUSELAGE-TO-WING CONNECTION LINK (EDDY CURRENT)CONNECTION LINK FITTING (LUG AND INNER CAP).

53 20-11-01-901 AIRWORTHINESS

AIRFRAME749

L: 17500 L: 17500 L: 16547

NDT PART 6 53-20-00

INTERNAL DETAILED INSPECTION CENTERFUSELAGE-TO-WING CONNECTION LINK FITTING.

53 20-11-01-902 AIRWORTHINESS

AIRFRAME750

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

INTERNAL DETAILED INSPECTION AFT PRESSUREBULKHEAD.

53 20-12-01-901 AIRWORTHINESS

AIRFRAME751

L: 17500 L: 17500 L: 16547

NDT PART 5 53-20-00

EXTERNAL DETAILED VISUAL INSPECTION OF AFTFUSELAGE SKINS AND ATTACHMENTS

53 30-00-001

AIRFRAME752

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-30-00

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL DETAILED VISUAL INSPECTION OF AFTFUSELAGE UPPER SKIN, JUNCTIONS AND ATTACHEMENTS

53 30-00-002

AIRFRAME753

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-30-00

INTERNAL DETAILED VISUAL INSPECTION OF AFTFUSELAGE SIDE SKIN, CUTOUTS AND ATTACHMENTS

53 30-00-003

AIRFRAME754

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 53-30-00

INTERNAL DETAILED INSPECTION AFT FUSELAGE UPPERSKIN PANEL BEDPLATE AND ITS ATTACHMENTS, BEDPLATESTO STRINGER ATTACHMENTS AND SKIN TO BEDPLATE AREA.

53 30-01-01-901 AIRWORTHINESS

AIRFRAME755

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION AFT FUSELAGE UPPERSKIN PANEL SKIN TO BEDPLATE AREA.

53 30-01-01-902 AIRWORTHINESS

AIRFRAME756

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL GENERAL VISUAL INSPECTION AFT FUSELAGESIDE SKIN PANEL FORWARD MACHINED FRAME (FRAME 22AND FRAME 23)

53 30-02-01-901 AIRWORTHINESS

AIRFRAME757

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION AFT FUSELAGE SIDESKIN PANEL SKIN TO FRAME AREA

53 30-02-01-902 AIRWORTHINESS

AIRFRAME758

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL GENERAL VISUAL INSPECTION AFT FUSELAGESIDE SKIN PANEL AFT MACHINED FRAME (FRAME 25 ANDFR25A)

53 30-02-02-901 AIRWORTHINESS

AIRFRAME759

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION AFT FUSELAGE SIDESKIN PANEL - SKIN TO FRAME AREA

53 30-02-02-902 AIRWORTHINESS

AIRFRAME760

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION AFT FUSELAGELONGITUDINAL AND CIRCUMFERENTIAL SKIN SPLICES AFTFUSELAGE SKIN TO LONGITUDINAL SPLICE.

53 30-04-01-901 AIRWORTHINESS

AIRFRAME761

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL DETAILED INSPECTION AFT FUSELAGELONGITUDINAL AND CIRCUMFERENTIAL SKIN SPLICESLONGITUDINAL SPLICE

53 30-04-01-902 AIRWORTHINESS

AIRFRAME762

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Intervals Tolerance Time At Inst Next DueInstalled

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EXTERNAL - DETAILED INSPECTION AFT FUSELAGELONGITUDINAL AND CIRCUMFERENTIAL SKIN SPLICES TOCIRCUMFERENTIAL SPLICE.

53 30-04-02-901 AIRWORTHINESS

AIRFRAME763

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL DETAILED INSPECTION AFT FUSELAGELONGITUDINAL AND CIRCUMFERENTIAL SKIN SPLICES TOCIRCUMFERENTIAL SPLICE.

53 30-04-02-902 AIRWORTHINESS

AIRFRAME764

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL DETAILED VISUAL INSPECTION OF AFTFUSELAGE BAGGABE DOOR CUTOUT STRUCTURE

53 30-05-00148MOAIRFRAME765

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 53-30-00

INTERNAL GENERAL VISUAL INSPECTION AFT FUSELAGEBAGGAGE DOOR CUTOUT STRUCTURE.

53 30-05-01-901 AIRWORTHINESS

AIRFRAME766

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION AFT FUSELAGEBAGGAGE DOOR CUTOUT STRUCTURE AFT FUSELAGE THESKIN TO BAGGAGE DOOR CUTOUT STRUCTURE.

53 30-05-01-902 AIRWORTHINESS

AIRFRAME767

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL GENERAL VISUAL INSPECTION AFT FUSELAGECUTOUT STRUCTURES - INTERNAL FRAMES, STRINGER,REINFORCEMENT, AND DOUBLER OF AFT FUSELAGE CUTOUTSTRUCTURES.

53 30-06-01-901 AIRWORTHINESS

AIRFRAME768

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

INTERNAL DETAILED VISUAL INSPECTION OF AFTFUSELAGE UPPER FRAMES 29 TO 32

53 30-07-00148MOAIRFRAME769

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 53-30-00

INTERNAL GENERAL VISUAL INSPECTION AFT FUSELAGEUPPER FRAMES (FROM FRAME 29 TO FRAME 32)MACHINED FRAMES.

53 30-07-01-901 AIRWORTHINESS

AIRFRAME770

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL - DETAILED INSPECTION AFT FUSELAGE UPPERFRAMES (FROM FRAME 29 TO FRAME 32) SKIN TO FRAMEAREA.

53 30-07-01-902 AIRWORTHINESS

AIRFRAME771

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL GENERAL VISUAL INSPECTION AFT FUSELAGEUPPER FRAMES (FROM FRAME 29 TO FRAME 32)BEDPLATES AND FASTENERS.

53 30-07-02-901 AIRWORTHINESS

AIRFRAME772

L: 17500 L: 17500 L: 16547

NDT PART 5 53-30-00

EXTERNAL DETAILED VISUAL INSPECTION OF AFTFUSELAGE MACHINED FRAME 32

53 30-08-00196MOAIRFRAME773

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 53-30-00

EXTERNAL GENERAL VISUAL INSPECTION OF THE FORWARDFUSELAGE NOSE SECTION

53 Z210-0016000HR/96MOAIRFRAME774

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

INTERNAL GENERAL VISUAL INSPECTION OF THE FORWARDFUSELAGE NOSE SECTION

53 Z210-002300HR/48MOAIRFRAME775

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

EXTERNAL GENERAL VISUAL INSPECTION OF THE FORWARDFUSELAGE COCKPIT SECTION

53 Z220-001300HR/48MOAIRFRAME776

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

INTERNAL GENERAL VISUAL INSPECTION OF THE FORWARDFUSELAGE COCKPIT SECTION

53 Z220-0024800HR/72MOAIRFRAME777

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF THE CENTERFUSELAGE FRONT SECTION

53 Z230-0014800HR/72MOAIRFRAME778

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

AMM 05-42-00

INTERNAL GENERAL VISUAL INSPECTION OF THE CENTERFUSELAGE FRONT SECTION

53 Z230-0024800HR/72MOAIRFRAME779

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF THE CENTERFUSELAGE REAR SECTION

53 Z240-0016000HR/96MOAIRFRAME780

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

INTERNAL GENERAL VISUAL INSPECTION OF THE CENTERFUSELAGE REAR SECTION

53 Z240-0024800HR/72MOAIRFRAME781

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF THE AFTFUSELAGE FRONT SECTION

53 Z310-0014800HR/72MOAIRFRAME782

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

INTERNAL GENERAL VISUAL INSPECTION OF THE AFTFUSELAGE FRONT SECTION

53 Z310-0024800HR/72MOAIRFRAME783

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF THE AFTFUSELAGE REAR SECTION

53 Z320-0016000HR/96MOAIRFRAME784

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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INTERNAL GENERAL VISUAL INSPECTION OF THE AFTFUSELAGE REAR SECTION

53 Z320-002300HR/48MOAIRFRAME785

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

EXTERNAL GENERAL VISUAL INSPECTION OF PYLONPOLYURETHANE FILMS

54 00-00-00112MOAIRFRAME786

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 54-51-20

INTERNAL DETAILED VISUAL INSPECTION OF PYLON MAINBOX

54 50-00-001

AIRFRAME787

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 54-50-00

INTERNAL DETAILED VISUAL INSPECTION OF FORWARDBEAM

54 50-00-002

AIRFRAME788

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 54-50-00

INTERNAL DETAILED INSPECTION PYLON FORWARD BEAMPYLON SPARS 1 AND 2, UPPER AND LOWER SKIN ANDFASTENERS.

54 50-01-01-901 AIRWORTHINESS

AIRFRAME789

L: 17500 L: 17500 L: 16547

NDT PART 5 54-50-00

INTERNAL DETAILED INSPECTION PYLON AFT BEAM PYLONSPARS 3 AND 4 AND FASTENERS.

54 50-02-01-901 AIRWORTHINESS

AIRFRAME790

L: 17500 L: 17500 L: 16547

NDT PART 5 54-50-00

EXTERNAL GENERAL VISUAL INSPECTION OF PYLON MAINBOX

54 50-03-001

AIRFRAME791

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 54-50-00

EXTERNAL GENERAL VISUAL INSPECTION PYLON MAIN BOXMAIN BOX SKIN AND FASTENERS.

54 50-03-01-901 AIRWORTHINESS

AIRFRAME792

L: 17500 L: 17500 L: 16547

NDT PART 5 54-50-00

INTERNAL DETAILED INSPECTION PYLON-TO-FUSELAGECONNECTIONS OF BOLTS.

54 50-04-01-901 AIRWORTHINESS

AIRFRAME793

L: 17500 L: 17500 L: 16547

NDT PART 5 54-50-00

EXTERNAL DETAILED VISUAL INSPECTION OF PYLONYOKES

54 50-05-00148MOAIRFRAME794

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 54-50-00

INTERNAL DETAILED INSPECTION PYLON YOKES LUGHOLES AT YOKES, YOKES, GUSSETS AND SHIELD.

54 50-05-01-901 AIRWORTHINESS

AIRFRAME795

L: 17500 L: 17500 L: 16547

NDT PART 5 54-50-00

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL DETAILED VISUAL INSPECTION OF AFT MOUNTFITTINGS

54 50-06-00172MOAIRFRAME796

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 54-50-00

INTERNAL DETAILED INSPECTION PYLON AFT FITTINGAFT MOUNT FITTING AND FASTENERS.

54 50-06-01-901 AIRWORTHINESS

AIRFRAME797

L: 17500 L: 17500 L: 16547

NDT PART 5 54-50-00

EXTERNAL GENERAL VISUAL INSPECTION OF THE PYLON54 Z410-0016000HR/96MOAIRFRAME798

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

INTERNAL GENERAL VISUAL INSPECTION OF THE PYLON54 Z410-0024800HR/72MOAIRFRAME799

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF THE NACELLE54 Z430-0016000HR/96MOAIRFRAME800

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

INTERNAL GENERAL VISUAL INSPECTION OF THE NACELLE54 Z430-002300HR/48MOAIRFRAME801

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

EXTERNAL GENERAL VISUAL INSPECTION OF STABILIZERPOLYURETHANE FILMS

55 00-00-00112MOAIRFRAME802

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 55-00-20

HORIZONTAL STABILIZER55 10-00

AIRFRAME803

14-AUG-2009 H: 0

500-10700-405 0000502610

EXTERNAL - DETAILED INSPECTION OFHORIZONTAL-STABILIZER SPARS

55 10-00-00196MOAIRFRAME804

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-10-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF HORIZONTAL-STABILIZER MAIN BOX

55 10-00-00272MOAIRFRAME805

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 55-10-00

EXTERNAL GENERAL VISUAL INSPECTION OFVERTICAL-TO-HORIZONTAL STABILIZER ATTACHMENTS

55 10-01-00148MOAIRFRAME806

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 55-10-00

INTERNAL DETAILED INSPECTION FIN-TO-HORIZONTALSTABILIZER CONNECTIONS IN HORIZONTAL STABILIZERAND FASTENERS.

55 10-01-01-901 AIRWORTHINESS

AIRFRAME807

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL SPECIAL DETAILED INSPECTION HORIZONTALSTABILIZER FRONT SPAR (BORESCOPIC) FRONT SPARAND FASTENERS.

55 10-02-01-901 AIRWORTHINESS

AIRFRAME808

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER FRONT SPAR FRONT SPAR AND FASTENERS.

55 10-02-01-902 AIRWORTHINESS

AIRFRAME809

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

INTERNAL SPECIAL DETAILED INSPECTION HORIZONTALSTABILIZER REAR SPAR (BORESCOPIC) REAR SPAR.

55 10-03-01-901 AIRWORTHINESS

AIRFRAME810

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER REAR SPAR REAR SPAR AND FASTENERS.

55 10-03-01-902 AIRWORTHINESS

AIRFRAME811

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

INTERNAL SPECIAL DETAILED INSPECTION HORIZONTALSTABILIZER MAIN BOX UPPER SKIN (BORESCOPIC)STRINGERS.

55 10-04-01-901 AIRWORTHINESS

AIRFRAME812

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER MAIN BOX UPPER SKIN UPPER SKIN ANDFASTENERS.

55 10-04-01-902 AIRWORTHINESS

AIRFRAME813

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER MAIN BOX LOWER SKIN - LOWER SKIN.

55 10-05-01-901 AIRWORTHINESS

AIRFRAME814

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

INTERNAL DETAILED INSPECTION HORIZONTALSTABILIZER MAIN BOX LOWER SKIN LOWER SKIN AT FIN TO HORIZONTALSTABILIZER LINK AREA AND STRINGERS, INCLUDINGFASTENERS.

55 10-05-01-902 AIRWORTHINESS

AIRFRAME815

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

INTERNAL SPECIAL DETAILED INSPECTION HORIZONTALSTABILIZER COMPOSITE RIBS (BORESCOPIC) COMPOSITE RIBS AND FASTENERS.

55 10-06-01-901 AIRWORTHINESS

AIRFRAME816

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)ON HORIZONTAL-STABILIZER TIP RIBS

55 10-07-001

AIRFRAME817

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-10-00

INTERNAL DETAILED INSPECTION HORIZONTALSTABILIZER METALLIC RIBS ROOT AND TIP METALLIC RIBS, INCLUDING FASTENERS.

55 10-07-01-901 AIRWORTHINESS

AIRFRAME818

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION ON HORIZONTALSTABILIZER ROOT RIBS

55 10-08-001

AIRFRAME819

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-10-00

INTERNAL SPECIAL DETAILED INSPECTION HORIZONTALSTABILIZER LEADING EDGE (BORESCOPIC) HORIZONTALSTABILIZER LEADING EDGE SKIN AND SPAR.

55 10-08-01-901 AIRWORTHINESS

AIRFRAME820

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER LEADING EDGE HORIZONTAL STABILIZER LEADING EDGE SKIN ANDFASTENERS.

55 10-08-01-902 AIRWORTHINESS

AIRFRAME821

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF HORIZONTAL STABILIZER LEADING EDGE

55 10-09-00296MOAIRFRAME822

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER ELEVATOR FITTING HINGE FITTINGS, AND FASTENERS.

55 10-09-01-901 AIRWORTHINESS

AIRFRAME823

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

INTERNAL SPECIAL DETAILED INSPECTION HORIZONTALSTABILIZER ELEVATOR FITTING (EDDY CURRENT) LUGS.

55 10-09-02-901 AIRWORTHINESS

AIRFRAME824

L: 17500 L: 17500 L: 16547

NDT PART 6 55-10-00

INTERNAL DETAILED INSPECTION HORIZONTALSTABILIZER ELEVATOR FITTING TORQUE BOX ANDFASTENERS.

55 10-09-03-901 AIRWORTHINESS

AIRFRAME825

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL GENERAL VISUAL INSPECTION OFHORIZONTAL-STABILIZER HINGE FITTINGS

55 10-10-001

AIRFRAME826

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INTERNAL DETAILED INSPECTION HORIZONTALSTABILIZER TRIM TAB ACTUATOR SUPPORT FITTINGS TRIMTAB SUPPORTING FITTING AND FASTENERS.

55 10-10-01-901 AIRWORTHINESS

AIRFRAME827

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION HORIZONTALSTABILIZER TRIM TAB ACTUATOR SUPPORT FITTINGS TRIMTAB LINK SUPPORT FITTING AND FASTENERS.

55 10-10-02-901 AIRWORTHINESS

AIRFRAME828

L: 17500 L: 17500 L: 16547

NDT PART 5 55-10-00

INTERNAL DETAILED VISUAL INSPECTION OF TRIM-TABSUPPORT FITTINGS

55 10-11-00272MOAIRFRAME829

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 55-10-00

EXTERNAL - DETAILED INSPECTION OF ELEVATORFITTINGS AND TORQUE-TUBE ATTACHMENTS

55 20-00-00172MOAIRFRAME830

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 55-20-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF ELEVATOR MAIN BOX

55 20-01-00296MOAIRFRAME831

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-20-00

INTERNAL SPECIAL DETAILED INSPECTION ELEVATORMAIN BOX (SKIN, SPARS AND RIBS) (BORESCOPIC)SKIN, SPARS, RIBS AND FASTENERS.

55 20-01-01-901 AIRWORTHINESS

AIRFRAME832

L: 17500 L: 17500 L: 16547

NDT PART 5 55-20-00

EXTERNAL - DETAILED INSPECTION ELEVATOR MAIN BOX(SKIN, SPARS AND RIBS) SKIN AND FASTENERS, INCLUDING MAINBOX, TRAILING EDGE, LEADING EDGE AND HORN.

55 20-01-01-902 AIRWORTHINESS

AIRFRAME833

L: 17500 L: 17500 L: 16547

NDT PART 5 55-20-00

INTERNAL SPECIAL DETAILED INSPECTION ELEVATORHINGE FITTINGS (DYE PENETRANT) ELEVATORHINGE PINS.

55 20-02-01-901 AIRWORTHINESS

AIRFRAME834

L: 17500 L: 17500 L: 16547

NDT PART 8 55-20-00

INTERNAL SPECIAL DETAILED INSPECTION ELEVATORHINGE FITTINGS (EDDY CURRENT) ELEVATOR HINGEFITTINGS.

55 20-02-02-901 AIRWORTHINESS

AIRFRAME835

L: 17500 L: 17500 L: 16547

NDT PART 6 55-20-00

INTERNAL DETAILED INSPECTION ELEVATOR HINGEFITTINGS ELEVATOR HINGE FITTINGS.

55 20-02-02-902 AIRWORTHINESS

AIRFRAME836

L: 17500 L: 17500 L: 16547

NDT PART 5 55-20-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL SPECIAL DETAILED INSPECTION ELEVATORTORQUE TUBE ASSY (EDDY CURRENT) ELEVATOR TORQUETUBE FLANGE.

55 20-03-01-901 AIRWORTHINESS

AIRFRAME837

L: 17500 L: 17500 L: 16547

NDT PART 6 55-20-00

INTERNAL SPECIAL DETAILED INSPECTION ELEVATORTORQUE TUBE ASSY (DYE PENETRANT) ELEVATOR TORQUETUBE.

55 20-03-02-901 AIRWORTHINESS

AIRFRAME838

L: 17500 L: 17500 L: 16547

NDT PART 8 55-20-00

EXTERNAL GENERAL VISUAL INSPECTION OF ELEVATORTAB PIANO HINGE

55 22-01-001

AIRFRAME839

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-22-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF ELEVATOR TAB BOX

55 22-02-001

AIRFRAME840

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-22-00

EXTERNAL GENERAL VISUAL INSPECTION OF VERTICALSTABILIZER TO AFT FUSELAGE CONNECTIONS AT VERTICALSTABILIZER

55 30-01-00172MOAIRFRAME841

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 55-30-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF FIN-TO-REAR FUSELAGE CONNECTIONS AT VERTICALSTABILIZER

55 30-01-00248MOAIRFRAME842

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 55-30-00

INTERNAL SPECIAL DETAILED INSPECTION FIN-TO-FUSELAGE CONNECTIONS IN VERTICAL STABILIZER(BORESCOPIC) FITTING, PINS AND SPARS ATTACHMENTS(UPPER PART OF CONNECTIONS).

55 30-01-01-901 AIRWORTHINESS

AIRFRAME843

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL DETAILED INSPECTION FIN-TO-FUSELAGECONNECTIONS IN VERTICAL STABILIZER FITTING, PINSAND SPAR ATTACHMENTS (LOWER PART OFCONNECTIONS), NUT, SEAL AND FASTENERS.

55 30-01-01-902 AIRWORTHINESS

AIRFRAME844

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL DETAILED INSPECTION FIN-TO-FUSELAGECONNECTIONS IN VERTICAL STABILIZER L SHAPE, RIBAND FASTENERS.

55 30-01-02-901 AIRWORTHINESS

AIRFRAME845

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF FIN-TO-HORIZONTAL STABILIZER CONNECTIONS ONVERTICAL STABILIZER

55 30-02-00272MOAIRFRAME846

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 55-30-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL SPECIAL DETAILED INSPECTION FIN-TO-HORIZONTAL STABILIZER CONNECTIONS ONVERTICAL STABILIZER (BORESCOPIC) DOUBLER AND TIPRIB.

55 30-02-01-901 AIRWORTHINESS

AIRFRAME847

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL SPECIAL DETAILED INSPECTION FIN-TO-HORIZONTAL STABILIZER CONNECTIONS ONVERTICAL STABILIZER (EDDY CURRENT) DOUBLER AND TIP RIB AT FRONT ANDREAR FITTING AREA.

55 30-02-01-902 AIRWORTHINESS

AIRFRAME848

L: 17500 L: 17500 L: 16547

NDT PART 6 53-30-00

INTERNAL DETAILED INSPECTION FIN-TO-HORIZONTALSTABILIZER CONNECTIONS ON VERTICAL STABILIZER LSHAPE AND FASTENERS.

55 30-02-02-901 AIRWORTHINESS

AIRFRAME849

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL SPECIAL DETAILED INSPECTION FIN-TO-HORIZONTAL STABILIZER CONNECTIONS ONVERTICAL STABILIZER (BORESCOPIC) L SHAPE ANDFASTENERS.

55 30-02-02-902 AIRWORTHINESS

AIRFRAME850

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL DETAILED INSPECTION FIN-TO-HORIZONTALSTABILIZER CONNECTIONS ON VERTICAL STABILIZERFITTINGS AND FASTENERS.

55 30-02-03-901 AIRWORTHINESS

AIRFRAME851

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL DETAILED INSPECTION FIN-TO-HORIZONTALSTABILIZER CONNECTIONS ON VERTICAL STABILIZERCOMPOSITE PLATES AND FASTENERS.

55 30-02-04-901 AIRWORTHINESS

AIRFRAME852

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF VERTICAL STABILIZER MAIN BOX

55 30-03-00196MOAIRFRAME853

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-30-00

EXTERNAL - DETAILED INSPECTION VERTICALSTABILIZER MAIN BOX (SKIN AND SPARS) SKIN ANDSPAR.

55 30-03-01-901 AIRWORTHINESS

AIRFRAME854

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL SPECIAL DETAILED INSPECTION VERTICALSTABILIZER MAIN BOX (SKIN AND SPARS)(BORESCOPIC) SPAR.

55 30-03-01-902 AIRWORTHINESS

AIRFRAME855

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

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Intervals Tolerance Time At Inst Next DueInstalled

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EXTERNAL DETAILED VISUAL INSPECTION OF VERTICALSTABILIZER-TO-RUDDER FITTING

55 30-05-00148MOAIRFRAME856

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 55-30-00

EXTERNAL - DETAILED INSPECTION RUDDER HINGEFITTINGS HINGE FITTING 1 AND FASTENERS.

55 30-05-01-901 AIRWORTHINESS

AIRFRAME857

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDER HINGEFITTINGS (EDDY CURRENT) HINGE FITTING 2 FLANGES.

55 30-05-02-901 AIRWORTHINESS

AIRFRAME858

L: 17500 L: 17500 L: 16547

NDT PART 6 55-30-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDER HINGEFITTINGS (EDDY CURRENT) RUDDER LUG HINGEFITTINGS 1 AND 2.

55 30-05-03-901 AIRWORTHINESS

AIRFRAME859

L: 17500 L: 17500 L: 16547

NDT PART 6 55-30-00

EXTERNAL DETAILED VISUAL INSPECTION OF RUDDER TABACTUATOR FITTING AND SUPPORT FITTINGS

55 30-06-001

AIRFRAME860

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-30-00

EXTERNAL - DETAILED INSPECTION VERTICALSTABILIZER TAB ACTUATOR AND SUPPORT FITTINGSFITTINGS, LUGS AND FASTENERS.

55 30-06-01-901 AIRWORTHINESS

AIRFRAME861

L: 17500 L: 17500 L: 16547

NDT PART 5 55-30-00

VERTICAL STABILIZER55 33-00

AIRFRAME862

14-AUG-2009 H: 0

500-10100-411 0000501205

EXTERNAL GENERAL VISUAL INSPECTION OF RUDDERASSEMBLY

55 40-01-00196MOAIRFRAME863

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-40-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF RUDDER ASSEMBLY

55 40-01-00296MOAIRFRAME864

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-40-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDER MAINBOX (BORESCOPIC) SKIN, SPARS, RIBS ANDFASTENERS.

55 40-01-01-901 AIRWORTHINESS

AIRFRAME865

L: 17500 L: 17500 L: 16547

NDT PART 5 55-40-00

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Intervals Tolerance Time At Inst Next DueInstalled

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EXTERNAL - DETAILED INSPECTION RUDDER MAIN BOX MAIN BOX, TRAILING EDGE AND LEADINGEDGE SKINS, INCLUDING FASTENERS.

55 40-01-01-902 AIRWORTHINESS

AIRFRAME866

L: 17500 L: 17500 L: 16547

NDT PART 5 55-40-00

EXTERNAL GENERAL VISUAL INSPECTION OF RUDDERHINGE FITTINGS

55 40-02-00196MOAIRFRAME867

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 55-40-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDER HINGEFITTINGS (DYE PENETRANT) RUDDER HINGEFITTINGS PINS.

55 40-02-01-901 AIRWORTHINESS

AIRFRAME868

L: 17500 L: 17500 L: 16547

NDT PART 8 55-40-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDER HINGEFITTINGS (EDDY CURRENT) RUDDER HINGEFITTINGS.

55 40-02-02-901 AIRWORTHINESS

AIRFRAME869

L: 17500 L: 17500 L: 16547

NDT PART 6 55-40-00

INTERNAL DETAILED INSPECTION RUDDER HINGEFITTINGS RUDDER HINGE FITTINGS.

55 40-02-02-902 AIRWORTHINESS

AIRFRAME870

L: 17500 L: 17500 L: 16547

NDT PART 5 55-40-00

EXTERNAL DETAILED VISUAL INSPECTION OF RUDDERTORQUE-TUBE ASSEMBLY

55 40-03-001

AIRFRAME871

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-40-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDERTORQUE TUBE ASSEMBLY (EDDY CURRENT) RUDDER TORQUE TUBE FLANGE.

55 40-03-01-901 AIRWORTHINESS

AIRFRAME872

L: 17500 L: 17500 L: 16547

NDT PART 6 55-40-00

INTERNAL SPECIAL DETAILED INSPECTION RUDDERTORQUE TUBE ASSEMBLY (DYE PENETRANT) RUDDER TORQUE TUBE.

55 40-03-02-901 AIRWORTHINESS

AIRFRAME873

L: 17500 L: 17500 L: 16547

NDT PART 8 55-40-00

RUDDER ASSEMBLY55 41-00

AIRFRAME874

14-AUG-2009 H: 0

PN SN-UNKNOWN

EXTERNAL DETAILED VISUAL INSPECTION OF RUDDER TABPIANO HINGE

55 42-01-001

AIRFRAME875

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 55-42-00

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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EXTERNAL GENERAL VISUAL INSPECTION OF THEVERTICAL STABILIZER

55 Z330-0014800HR/72MOAIRFRAME876

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

INTERNAL GENERAL VISUAL INSPECTION OF THEVERTICAL STABILIZER

55 Z330-0024800HR/72MOAIRFRAME877

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF THEHORIZONTAL STABILIZER

55 Z340-0014800HR/72MOAIRFRAME878

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

INTERNAL GENERAL VISUAL INSPECTION OF THEHORIZONTAL STABILIZER

55 Z340-0024800HR/72MOAIRFRAME879

14-AUG-2009 M: 72H: 4800.00

D: +/-30H: +/-30

14-AUG-2015H: 4800.00

M: 6 D: 11H: 3653.30

EXTERNAL GENERAL VISUAL INSPECTION OF COCKPITSIDE-WINDOWS

56 10-01-00172MOAIRFRAME880

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 56-10-00

EXTERNAL DETAILED VISUAL INSPECTION OF WINDSHIELDAND COCKPIT SIDE WINDOW FRAMES AND FASTENERS

56 10-03-00124MOAIRFRAME881

12-SEP-2013H: 786.90L: 722

M: 24 D: +/-30 12-SEP-2015 M: 7 D: 9

NDT PART 5 56-10-00

EXTERNAL SPECIAL DETAILED INSPECTION WINDSHIELDFRAME AND FASTENERS (EDDY CURRENT) FRAMES AND FASTENERS.

56 10-03-01-901 AIRWORTHINESS

AIRFRAME882

L: 17500 L: 17500 L: 16547

NDT PART 6 56-10-00

COPILOT RH HEATED GLASS WINDSHIELD56 11-00

AIRFRAME883

14-AUG-2009 H: 0

NP-195301-2 09103H6348

PILOT LH HEATED GLASS WINDSHIELD56 11-00

AIRFRAME884

14-AUG-2009 H: 0

NP-195301-1 09024H7813

COPILOT RH ACRYLIC SIDE WINDOW56 12-00

AIRFRAME885

14-AUG-2009 H: 0

NP-195302-4 08288H5378

PILOT LH ACRYLIC SIDE WINDOW56 12-00

AIRFRAME886

14-AUG-2009 H: 0

NP-195302-3 08282H4813

LEFT NO.1 WINDOW TRANSPARENCY56 20-00

AIRFRAME887

14-AUG-2009 H: 0

14024 00876

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LEFT NO.2 WINDOW TRANSPARENCY56 20-00

AIRFRAME888

14-AUG-2009 H: 0

14024 00765

LEFT NO.3 WINDOW TRANSPARENCY56 20-00

AIRFRAME889

14-AUG-2009 H: 0

14024 00740

LEFT NO.4 WINDOW TRANSPARENCY56 20-00

AIRFRAME890

14-AUG-2009 H: 0

14024 00739

RIGHT NO. 1 WINDOW TRANSPARENCY56 20-00

AIRFRAME891

14-AUG-2009 H: 0

14024 00738

RIGHT NO. 2 WINDOW TRANSPARENCY56 20-00

AIRFRAME892

14-AUG-2009 H: 0

14024 00736

RIGHT NO. 3 WINDOW TRANSPARENCY56 20-00

AIRFRAME893

14-AUG-2009 H: 0

14024 00542

RIGHT NO. 4 WINDOW TRANSPARENCY56 20-00

AIRFRAME894

14-AUG-2009 H: 0

14024 00763

EXTERNAL GENERAL VISUAL INSPECTION OF PASSENGERCABIN WINDOWS

56 20-01-00172MOAIRFRAME895

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 56-20-00

EXTERNAL GENERAL VISUAL INSPECTION OF WINGPOLYURETHANE FILMS

57 00-00-00112MOAIRFRAME896

14-SEP-2014H: 1038.80L: 883

M: 12 D: +/-30 14-SEP-2015 M: 7 D: 11

AMM 57-30-20

EXTERNAL DETAILED VISUAL INSPECTION OFWING-TO-FUSELAGE LINKS

57 10-00-001

AIRFRAME897

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-10-00

INTERNAL DETAILED VISUAL INSPECTION OF WING MAINBOX

57 10-00-002

AIRFRAME898

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 57-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INTERNAL DETAILED VISUAL INSPECTION OF WINGMIDDLE AND REAR SPARS

57 10-00-00348MOAIRFRAME899

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LATERAL LINKSTO CENTER FUSELAGE FRONT FITTING, BOLT, NUT AND SEAL.

57 10-01-01-901 AIRWORTHINESS

AIRFRAME900

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LATERAL LINKSTO CENTER FUSELAGE REAR FITTING, BOLT, NUT AND SEAL.

57 10-01-02-901 AIRWORTHINESS

AIRFRAME901

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL SPECIAL DETAILED INSPECTION WING CENTERLINKS-TO-CENTER FUSELAGE (EDDY CURRENT) WING CENTER FITTING AND LUG.

57 10-02-01-901 AIRWORTHINESS

AIRFRAME902

L: 17500 L: 17500 L: 16547

NDT PART 6 57-10-00

INTERNAL DETAILED INSPECTION WING CENTERLINKS-TO-CENTER FUSELAGE WING CENTER FITTING.

57 10-02-01-902 AIRWORTHINESS

AIRFRAME903

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL SPECIAL DETAILED INSPECTION WING CENTERLINKS-TO-CENTER FUSELAGE (EDDY CURRENT) CENTER LINK LUGS.

57 10-02-02-901 AIRWORTHINESS

AIRFRAME904

L: 17500 L: 17500 L: 16547

NDT PART 6 57-10-00

INTERNAL DETAILED INSPECTION WING CENTERLINKS-TO-CENTER FUSELAGE CENTER LINK FITTING, BOLT, NUT AND SEAL.

57 10-02-02-902 AIRWORTHINESS

AIRFRAME905

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL SPECIAL DETAILED INSPECTION WING CENTERLINKS-TO-CENTER FUSELAGE (MAGNETIC PARTICLE)HORIZONTAL LINK BOLTS.

57 10-02-03-901 AIRWORTHINESS

AIRFRAME906

L: 17500 L: 17500 L: 16547

NDT PART 7 57-10-00

INTERNAL DETAILED INSPECTION WING FRONT SPAR FRONT SPAR LOWER CAP BETWEEN RIB 1 AND3 AND WINDOW ACCESS FRAMES, INCLUDING FASTENERS.

57 10-03-01-901 AIRWORTHINESS

AIRFRAME907

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INTERNAL DETAILED INSPECTION WING FRONT SPAR FRONT SPAR LOWER CAP BETWEEN RIB 3AND 6 AND WINDOW ACCESS FRAMES, INCLUDINGFASTENERS.

57 10-03-02-901 AIRWORTHINESS

AIRFRAME908

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL - DETAILED INSPECTION WING FRONT SPAR LOWER SKIN BETWEEN RIB 6 AND 7,INCLUDING FASTENER.

57 10-03-03-901 AIRWORTHINESS

AIRFRAME909

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING FRONT SPAR FRONT SPAR LOWER CAP BETWEEN RIB 7 AND10 AND WINDOW ACCESS FRAMES, INCLUDING FASTENERS.

57 10-03-04-901 AIRWORTHINESS

AIRFRAME910

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL - DETAILED INSPECTION WING FRONT SPAR LOWER SKIN BETWEEN RIB 10 AND 16,INCLUDING FASTENERS.

57 10-03-05-901 AIRWORTHINESS

AIRFRAME911

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING MIDDLE SPAR MIDDLE SPAR LOWER CAP BETWEEN RIB 1 AND3, INCLUDING FASTENERS.

57 10-04-01-901 AIRWORTHINESS

AIRFRAME912

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING MIDDLE SPAR MIDDLE SPAR LOWER CAP BETWEEN RIB 3 AND7, INCLUDING FASTENERS .

57 10-04-02-901 AIRWORTHINESS

AIRFRAME913

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING MIDDLE SPAR MIDDLE SPAR LOWER CAP BETWEEN RIB7 AND 9, INCLUDING SPAR-STRINGER-SPLICE ANDFASTENERS.

57 10-04-03-901 AIRWORTHINESS

AIRFRAME914

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL SPECIAL DETAILED INSPECTION WING MIDDLESPAR (EDDY CURRENT) MLG FRONTTRUNNION (LUG, SURFACE AND RADIUS).

57 10-04-04-901 AIRWORTHINESS

AIRFRAME915

L: 17500 L: 17500 L: 16547

NDT PART 6 57-10-00

INTERNAL DETAILED INSPECTION WING MIDDLE SPAR MLG FRONT TRUNNION AND FASTENERS.

57 10-04-04-902 AIRWORTHINESS

AIRFRAME916

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INTERNAL SPECIAL DETAILED INSPECTION WING MIDDLESPAR (EDDY CURRENT) MLG ACTUATORFITTING (SURFACE AND RADIUS).

57 10-04-05-901 AIRWORTHINESS

AIRFRAME917

L: 17500 L: 17500 L: 16547

NDT PART 6 57-10-00

INTERNAL DETAILED INSPECTION WING MIDDLE SPAR MLG ACTUATOR FITTING AND FASTENERS.

57 10-04-05-902 AIRWORTHINESS

AIRFRAME918

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING REAR SPAR REAR SPAR LOWER CAP BETWEEN RIB 1 AND3 AND WINDOW ACCESS FRAME.

57 10-05-01-901 AIRWORTHINESS

AIRFRAME919

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL - DETAILED INSPECTION WING REAR SPAR REAR SPAR LOWER CAP BETWEEN RIB 3AND 7, INCLUDING FASTENERS.

57 10-05-02-901 AIRWORTHINESS

AIRFRAME920

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING REAR SPAR REAR SPAR LOWER CAP BETWEEN RIB 7 AND10, INCLUDING FASTENERS.

57 10-05-03-901 AIRWORTHINESS

AIRFRAME921

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL - DETAILED INSPECTION WING REAR SPAR LOWER SKIN BETWEEN RIB 10 AND 16,INCLUDING FASTENERS.

57 10-05-04-901 AIRWORTHINESS

AIRFRAME922

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL SPECIAL DETAILED INSPECTION WING REARSPAR (EDDY CURRENT) MLGREAR TRUNNION (LUG, SURFACE AND MACHINEDRADIUS).

57 10-05-05-901 AIRWORTHINESS

AIRFRAME923

L: 17500 L: 17500 L: 16547

NDT PART 6 57-10-00

EXTERNAL - DETAILED INSPECTION WING REAR SPAR MLG REAR TRUNNION AND FASTENERS.

57 10-05-05-902 AIRWORTHINESS

AIRFRAME924

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL DETAILED VISUAL INSPECTION OF WING UPPERPANEL

57 10-06-001

AIRFRAME925

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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EXTERNAL DETAILED VISUAL INSPECTION OF WING LOWERPANEL

57 10-07-00148MOAIRFRAME926

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 57-10-00

INTERNAL DETAILED VISUAL INSPECTION OF WING LOWERPANEL

57 10-07-002

AIRFRAME927

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LOWER PANEL STRINGER 2 AND 3 BETWEEN RIB 1 AND 3 ANDSHEAR CLIPS OF STRINGER 5 AND SHEAR CLIPSFASTENERS.

57 10-07-01-901 AIRWORTHINESS

AIRFRAME928

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LOWER PANEL STRINGER 2 RUN-OUT, STRINGER SHEARCLIPS AT RIB 8 AND WINDOW ACCESS PANEL 9 FRAMES.

57 10-07-02-901 AIRWORTHINESS

AIRFRAME929

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL - DETAILED INSPECTION WING LOWER PANEL LOWER PANEL AND FASTENERS BETWEENRIB 2 AND RIB 10, INCLUDING DOU-BLER AND ITSFASTENERS.

57 10-07-03-901 AIRWORTHINESS

AIRFRAME930

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LOWER PANEL MACHINED RIBS (RIB 1, RIB 3, RIB 3A,RIB 5R, RIB 6R, RIB 7R, RIB 8R).

57 10-08-01-901 AIRWORTHINESS

AIRFRAME931

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LOWER PANEL WING FORMED RIBS (RIB 2, RIB 4F,RIB 5F, RIB 6F, RIB 7F, RIB 8F, RIB 9, RIB 10,RIB11, RIB 12, RIB 13, RIB 14, RIB 15 AND RIB16).

57 10-08-02-901 AIRWORTHINESS

AIRFRAME932

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING LOWER PANEL DRY BAY WALLS AND FASTENERS.

57 10-08-03-901 AIRWORTHINESS

AIRFRAME933

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL DETAILED VISUAL INSPECTION OF WINGCENTER SPLICE

57 10-10-001

AIRFRAME934

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-10-00

INTERNAL GENERAL VISUAL INSPECTION OF WING CENTERSPLICE

57 10-10-00296MOAIRFRAME935

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 57-10-00

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Intervals Tolerance Time At Inst Next DueInstalled

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SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF WING CENTRAL SPLICE

57 10-10-003

AIRFRAME936

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-10-00

EXTERNAL - DETAILED INSPECTION WING CENTRALSPLICES FRONT SPAR SPLICE, LOWER SKINSPLICES, REAR SPAR SPLICES, INCLUDING FASTENERS.

57 10-10-01-901 AIRWORTHINESS

AIRFRAME937

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

INTERNAL DETAILED INSPECTION WING CENTRAL SPLICES WING LOWER SKIN ON SPLICE AREA,BETWEEN RIB1 AND RIB 2, FRONT , REAR AND MIDDLESPAR ON SPLICE AREA AND MIDDLE SPAR SPLICE,INCLUDING FASTENERS.

57 10-10-01-902 AIRWORTHINESS

AIRFRAME938

L: 17500 L: 17500 L: 16547

NDT PART 5 57-10-00

EXTERNAL DETAILED VISUAL INSPECTION OF AILERONTAB ACTUATOR SUPPORT FITTINGS AND TAB HINGEFITTINGS

57 10-11-001

AIRFRAME939

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-10-00

EXTERNAL DETAILED VISUAL INSPECTION OF WINGTRAILING-EDGE INBOARD AND OUTBOARD TORQUE BOXES

57 50-00-00148MOAIRFRAME940

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE INBOARD TORQUE BOX AND FLAP TRACK #1 SUPPORTS (EDDYCURRENT) WING ROOT TRACK.

57 50-01-01-901 AIRWORTHINESS

AIRFRAME941

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEINBOARD TORQUE BOX AND FLAP TRACK # 1 SUPPORTS WING ROOT TRACK.

57 50-01-01-902 AIRWORTHINESS

AIRFRAME942

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE INBOARD TORQUE BOX AND FLAP TRACK #1 SUPPORTS (DYE PENETRANT) WING ROOT ROLLER.

57 50-01-02-901 AIRWORTHINESS

AIRFRAME943

L: 8875 L: 8875 L: 7922

NDT PART 8 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE INBOARD TORQUE BOX AND FLAP TRACK #1 SUPPORTS (EDDYCURRENT) RIB 1.

57 50-01-03-901 AIRWORTHINESS

AIRFRAME944

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

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INTERNAL DETAILED INSPECTION WING TRAILING EDGEINBOARD TORQUE BOX AND FLAP TRACK # 1 SUPPORTS RIB 1 ANDFASTENERS.

57 50-01-03-902 AIRWORTHINESS

AIRFRAME945

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE FLAP TRACK # 2 SUPPORTS (EDDY CURRENT) WING CENTERTRACK.

57 50-02-01-901 AIRWORTHINESS

AIRFRAME946

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEFLAP TRACK # 2 SUPPORTS WING CENTER TRACK.

57 50-02-01-902 AIRWORTHINESS

AIRFRAME947

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE FLAP TRACK # 2 SUPPORTS (EDDY CURRENT) WING CENTERTRACK SUPPORT.

57 50-02-02-901 AIRWORTHINESS

AIRFRAME948

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEFLAP TRACK # 2 SUPPORTS WING CENTER TRACK SUPPORT.

57 50-02-02-902 AIRWORTHINESS

AIRFRAME949

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEFLAP TRACK # 2 SUPPORTS FITTINGS (LUG, ATTACHMENTS, PIN ANDFASTENERS).

57 50-02-03-901 AIRWORTHINESS

AIRFRAME950

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE OUTBOARD TORQUE BOX AND FLAP TRACK #3 SUPPORTS (EDDY CURRENT) WING TIP TRACK.

57 50-03-01-901 AIRWORTHINESS

AIRFRAME951

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEOUTBOARD TORQUE BOX AND FLAP TRACK # 3 SUPPORTS WING TIP TRACK.

57 50-03-01-902 AIRWORTHINESS

AIRFRAME952

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE OUTBOARD TORQUE BOX AND FLAP TRACK #3 SUPPORTS (DYE PENETRANT) WING TIP ROLLER.

57 50-03-02-901 AIRWORTHINESS

AIRFRAME953

L: 8875 L: 8875 L: 7922

NDT PART 8 57-50-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE OUTBOARD TORQUE BOX AND FLAP TRACK #3 SUPPORTS (EDDY CURRENT) RIBS 13 AND 13A WEB AND FLANGE.

57 50-03-03-901 AIRWORTHINESS

AIRFRAME954

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEOUTBOARD TORQUE BOX AND FLAP TRACK # 3 SUPPORTS RIBS 13 AND 13A.

57 50-03-03-902 AIRWORTHINESS

AIRFRAME955

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

EXTERNAL - DETAILED INSPECTION WING TRAILING EDGEOUTBOARD TORQUE BOX AND FLAP TRACK # 3 SUPPORTS TORQUE BOX SKIN ANDFASTENERS.

57 50-03-04-901 AIRWORTHINESS

AIRFRAME956

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

EXTERNAL DETAILED VISUAL INSPECTION OF WINGTRAILING EDGE AILERON HINGE FITTING

57 50-04-00172MOAIRFRAME957

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE AILERON SUPPORT FITTINGS (EDDY CURRENT) AILERONHINGE FITTING 01.

57 50-04-01-901 AIRWORTHINESS

AIRFRAME958

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE AILERON SUPPORT FITTINGS (EDDY CURRENT)AILERON HINGE FITTING 02 .

57 50-04-02-901 AIRWORTHINESS

AIRFRAME959

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEAILERON SUPPORT FITTINGS AILERON HINGE FITTING 02.

57 50-04-02-902 AIRWORTHINESS

AIRFRAME960

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

INTERNAL SPECIAL DETAILED INSPECTION WINGTRAILING EDGE AILERON SUPPORT FITTINGS (EDDY CURRENT) AILERONHINGE FITTING 03.

57 50-04-03-901 AIRWORTHINESS

AIRFRAME961

L: 17500 L: 17500 L: 16547

NDT PART 6 57-50-00

INTERNAL DETAILED INSPECTION WING TRAILING EDGEAILERON SUPPORT FITTINGS AILERON HINGE FITTING 03.

57 50-04-03-902 AIRWORTHINESS

AIRFRAME962

L: 17500 L: 17500 L: 16547

NDT PART 5 57-50-00

EXTERNAL DETAILED VISUAL INSPECTION OF FLAPASSEMBLY

57 51-00-001

AIRFRAME963

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-51-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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EXTERNAL - DETAILED INSPECTION FLAP UPPER SKINPANELS FLAP UPPER SKIN FROM RIB 7TO RIB 9.

57 51-01-01-901 AIRWORTHINESS

AIRFRAME964

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF THE FLAP MAIN BOX

57 51-02-002

AIRFRAME965

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP UPPERSKIN PANELS (BORESCOPIC) FLAP FRONT SPARBETWEEN RIB 5A AND RIB 5B.

57 51-02-01-901 AIRWORTHINESS

AIRFRAME966

L: 7049 L: 7049 L: 6096

NDT PART 5 57-51-00

EXTERNAL - DETAILED INSPECTION FLAP UPPER SKINPANELS FLAP LOWER SKIN FROM RIB 1 TO RIB5A AND FROM RIB 5B TO RIB 10.

57 51-02-03-901 AIRWORTHINESS

AIRFRAME967

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

EXTERNAL SPECIAL DETAILED INSPECTION FLAP UPPERSKIN PANELS (EDDY CURRENT) FLAP LOWERSKIN FROM RIB 4 TO RIB 5A AND FROM RIB 5B TO RIB 6AT FRONT SPAR AREA.

57 51-02-04-901 AIRWORTHINESS

AIRFRAME968

L: 17500 L: 17500 L: 16547

NDT PART 6 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP UPPERSKIN PANELS (BORESCOPIC) AROUND FASTENERSTHAT CONNECT CENTER ROLLERS FITTING TO RIB 5A ANDRIB 5B

57 51-02-05-901 AIRWORTHINESS

AIRFRAME969

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP UPPERSKIN PANELS (EDDY CURRENT) FRONT SPARFROM RIB 5A TO RIB 5B.

57 51-02-06-901 AIRWORTHINESS

AIRFRAME970

L: 17500 L: 17500 L: 16547

NDT PART 6 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP UPPERSKIN PANELS (EDDY CURRENT) RIB 1AND RIB 10.

57 51-02-07-901 AIRWORTHINESS

AIRFRAME971

L: 17500 L: 17500 L: 16547

NDT PART 6 57-51-00

EXTERNAL DETAILED VISUAL INSPECTION OF FLAP TRACKFITTINGS AND ACTUATOR FITTING

57 51-03-00148MOAIRFRAME972

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NDT PART 5 57-51-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL SPECIAL DETAILED INSPECTION FLAP TRACKSSUPPORT FITTINGS (EDDY CURRENT) FLAP ROOT TRACK.

57 51-03-01-901 AIRWORTHINESS

AIRFRAME973

L: 17500 L: 17500 L: 16547

NDT PART 6 57-51-00

INTERNAL DETAILED INSPECTION FLAP TRACKS SUPPORTFITTINGS FLAP ROOT TRACK.

57 51-03-01-902 AIRWORTHINESS

AIRFRAME974

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP TRACKSSUPPORT FITTINGS (EDDY CURRENT) FLAP TIP TRACK.

57 51-03-02-901 AIRWORTHINESS

AIRFRAME975

L: 17500 L: 17500 L: 16547

NDT PART 6 57-51-00

INTERNAL DETAILED INSPECTION FLAP TRACKS SUPPORTFITTINGS FLAP TIP TRACK.

57 51-03-02-902 AIRWORTHINESS

AIRFRAME976

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP TRACKSSUPPORT FITTINGS (DYE PENETRANT) FLAP ROOT ANDTIP ROLLERS.

57 51-03-03-901 AIRWORTHINESS

AIRFRAME977

L: 17500 L: 17500 L: 16547

NDT PART 8 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP TRACKSSUPPORT FITTINGS (DYE PENETRANT) CENTER ROLLERSEXTERNAL PINS.

57 51-03-04-901 AIRWORTHINESS

AIRFRAME978

L: 17500 L: 17500 L: 16547

NDT PART 8 57-51-00

INTERNAL SPECIAL DETAILED INSPECTION FLAP TRACKSSUPPORT FITTINGS (EDDY CURRENT) CENTER ROLLERSFITTING AROUND FASTENERS.

57 51-03-05-901 AIRWORTHINESS

AIRFRAME979

L: 17500 L: 17500 L: 16547

NDT PART 6 57-51-00

INTERNAL DETAILED INSPECTION FLAP ACTUATORSUPPORT FITTING FLAP ACTUATOR SUPPORT PIN.

57 51-04-01-901 AIRWORTHINESS

AIRFRAME980

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

INTERNAL DETAILED INSPECTION FLAP ACTUATORSUPPORT FITTING FLAP ACTUATOR SUPPORT FITTING AND FASTENERS.

57 51-04-02-901 AIRWORTHINESS

AIRFRAME981

L: 17500 L: 17500 L: 16547

NDT PART 5 57-51-00

LH AILERON ASSEMBLY57 60-00

AIRFRAME982

14-AUG-2009 H: 0

PN SN-UNKNOWN

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Intervals Tolerance Time At Inst Next DueInstalled

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RH AILERON ASSEMBLY57 60-00

AIRFRAME983

14-AUG-2009 H: 0

PN SN-UNKNOWN

EXTERNAL DETAILED VISUAL INSPECTION OF AILERONASSEMBLY AND AILERON TAB BOX

57 60-00-00196MOAIRFRAME984

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 57-60-00

SPECIAL DETAILED INSPECTION (BORESCOPE METHOD)OF AILERON MAIN BOX

57 60-01-00296MOAIRFRAME985

14-AUG-2009 M: 96 D: +/-30 14-AUG-2017 M: 30 D: 11

NDT PART 5 57-60-00

INTERNAL SPECIAL DETAILED INSPECTION AILERON MAINBOX (BORESCOPIC) SKIN, SPARS,RIBS AND FASTENERS.

57 60-01-01-901 AIRWORTHINESS

AIRFRAME986

L: 17500 L: 17500 L: 16547

NDT PART 5 57-60-00

EXTERNAL - DETAILED INSPECTION AILERON MAIN BOX SKIN, SPARS, RIBS AND FASTENERS.

57 60-01-01-902 AIRWORTHINESS

AIRFRAME987

L: 17500 L: 17500 L: 16547

NDT PART 5 57-60-00

INTERNAL SPECIAL DETAILED INSPECTION AILERONHINGE FITTINGS (DYE PENETRANT)AILERON HINGE FITTINGS PINS.

57 60-02-01-901 AIRWORTHINESS

AIRFRAME988

L: 17500 L: 17500 L: 16547

NDT PART 8 57-60-00

INTERNAL SPECIAL DETAILED INSPECTION AILERONHINGE FITTINGS (EDDY CURRENT) AILERONHINGE FITTINGS (LUGS, STIFFENERS RADIUS).

57 60-02-02-901 AIRWORTHINESS

AIRFRAME989

L: 17500 L: 17500 L: 16547

NDT PART 6 57-60-00

INTERNAL DETAILED INSPECTION AILERON HINGEFITTINGS AILERON HINGE FITTINGS.

57 60-02-02-902 AIRWORTHINESS

AIRFRAME990

L: 17500 L: 17500 L: 16547

NDT PART 5 57-60-00

EXTERNAL GENERAL VISUAL INSPECTION OF AILERONACTUATOR FITTING, HINGE FITTINGS AND PINS

57 60-03-00172MOAIRFRAME991

14-AUG-2009 M: 72 D: +/-30 14-AUG-2015 M: 6 D: 11

NDT PART 5 57-60-00

INTERNAL SPECIAL DETAILED INSPECTION AILERONCONTROL HINGE AND PIN (DYE PENETRANT) AILERON ACTUATORHINGE FITTINGS PINS.

57 60-03-01-901 AIRWORTHINESS

AIRFRAME992

L: 17500 L: 17500 L: 16547

NDT PART 8 57-60-00

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Intervals Tolerance Time At Inst Next DueInstalled

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INTERNAL SPECIAL DETAILED INSPECTION AILERONCONTROL HINGE AND PIN (EDDY CURRENT) AILERON ACTUATORHINGE FITTINGS (LUGS, STIFFEN-ERS RADIUS).

57 60-03-02-901 AIRWORTHINESS

AIRFRAME993

L: 17500 L: 17500 L: 16547

NDT PART 6 57-60-00

INTERNAL DETAILED INSPECTION AILERON CONTROLHINGE AND PIN AILERON ACTUATOR HINGE FITTINGS.

57 60-03-02-902 AIRWORTHINESS

AIRFRAME994

L: 17500 L: 17500 L: 16547

NDT PART 5 57-60-00

EXTERNAL GENERAL VISUAL INSPECTION OF AILERON TABASSEMBLY

57 63-00-001

AIRFRAME995

14-AUG-2009 M: 120 D: +/-30 14-AUG-2019 M: 54 D: 11

NDT PART 5 57-63-00

EXTERNAL GENERAL VISUAL INSPECTION OF THE WINGS57 Z500-001300HR/48MOAIRFRAME996

12-SEP-2013H: 786.90L: 722

M: 48H: 3000.00

D: +/-30H: +/-30

12-SEP-2017H: 3786.90

M: 31 D: 9H: 2640.20

INTERNAL GENERAL VISUAL INSPECTION OF THE WINGS57 Z500-00248MOAIRFRAME997

12-SEP-2013H: 786.90L: 722

M: 48 D: +/-30 12-SEP-2017 M: 31 D: 9

NO. 1 ENGINE - COMPRESSOR WASH71 0010

ENGINE 11021

01-JUL-2009

NO. 2 ENGINE - COMPRESSOR WASH71 0010

ENGINE 21022

01-JUL-2009

DISCARD LEFT LOWER FORWARD ISOLATOR MOUNT71 20-00-001

AIRFRAME998

31-OCT-2008 M: 240H: 4800.00

D: +/-30H: +/-30

M: 0H: 0

31-OCT-2028H: 4800.00

M: 164 D: 28H: 3653.30

LM-474-SA11 LK0245 AMM 71-20-00

DISCARD LEFT UPPER FORWARD ISOLATOR MOUNT71 20-00-001

AIRFRAME999

31-OCT-2008 M: 240H: 4800.00

D: +/-30H: +/-30

M: 0H: 0

31-OCT-2028H: 4800.00

M: 164 D: 28H: 3653.30

LM-474-SA11 LK0254 AMM 71-20-00

DISCARD LH AFT ISOLATOR MOUNT71 20-00-001

AIRFRAME1000

31-DEC-2008 M: 240H: 4800.00

D: +/-30H: +/-30

M: 0H: 0

31-DEC-2028H: 4800.00

M: 166 D: 28H: 3653.30

LM-474-SA2 LK0329 AMM 71-20-00

DISCARD RH AFT ISOLATOR MOUNT71 20-00-001

AIRFRAME1001

31-DEC-2008 M: 240H: 4800.00

D: +/-30H: +/-30

M: 0H: 0

31-DEC-2028H: 4800.00

M: 166 D: 28H: 3653.30

LM-474-SA2 LK0317 AMM 71-20-00

DISCARD RIGHT LOWER FORWARD ISOLATOR MOUNT71 20-00-001

AIRFRAME1002

31-OCT-2008 M: 240H: 4800.00

D: +/-30H: +/-30

M: 0H: 0

31-OCT-2028H: 4800.00

M: 164 D: 28H: 3653.30

LM-474-SA11 LK0268 AMM 71-20-00

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Intervals Tolerance Time At Inst Next DueInstalled

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DISCARD RIGHT UPPER FORWARD ISOLATOR MOUNT71 20-00-001

AIRFRAME1003

31-OCT-2008 M: 240H: 4800.00

D: +/-30H: +/-30

M: 0H: 0

31-OCT-2028H: 4800.00

M: 164 D: 28H: 3653.30

LM-474-SA11 LK0280 AMM 71-20-00

RIGHT UPPER FORWARD ISOLATOR MOUNT71 21-01

AIRFRAME1007

14-AUG-2009 H: 0

LM-474-SA11 LK0280

LEFT UPPER FORWARD ISOLATOR MOUNT71 21-01

AIRFRAME1005

14-AUG-2009 H: 0

LM-474-SA11 LK0254

RIGHT LOWER FORWARD ISOLATOR MOUNT71 21-01

AIRFRAME1006

14-AUG-2009 H: 0

LM-474-SA11 LK0268

LEFT LOWER FORWARD ISOLATOR MOUNT71 21-01

AIRFRAME1004

14-AUG-2009 H: 0

LM-474-SA11 LK0245

INTERNAL SPECIAL DETAILED INSPECTION ENGINEFORWARD MOUNTING ASSEMBLY (DYE PENETRANT)HOUSING.

71 21-01-01-901 AIRWORTHINESS

AIRFRAME1008

L: 5000 L: 5000 L: 4047

NDT PART 8 71-21-00

INTERNAL DETAILED INSPECTION ENGINE FORWARDMOUNTING ASSEMBLY ENGINE BOLT AND SLEEVE BOLT.

71 21-01-01-902 AIRWORTHINESS

AIRFRAME1009

L: 5000 L: 5000 L: 4047

NDT PART 5 71-21-00

LH AFT ISOLATOR MOUNT71 22-01

AIRFRAME1010

14-AUG-2009 H: 0

LM-474-SA2 LK0329

RH AFT ISOLATOR MOUNT71 22-01

AIRFRAME1011

14-AUG-2009 H: 0

LM-474-SA2 LK0317

INTERNAL SPECIAL DETAILED INSPECTION ENGINE AFTMOUNTING ASSEMBLY (DYE PENETRANT) HOUSING.

71 22-01-01-901 AIRWORTHINESS

AIRFRAME1012

L: 5000 L: 5000 L: 4047

NDT PART 8 71-22-00

INTERNAL DETAILED INSPECTION ENGINE AFT MOUNTINGASSEMBLY PYLON BOLTS, ENGINE BOLTS AND SLEEVEBOLTS.

71 22-01-01-902 AIRWORTHINESS

AIRFRAME1013

L: 1500 L: 1500 L: 547

NDT PART 5 71-22-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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DETAILED VISUAL INSPECTION OF PYLON FIREWALL SEAL71 31-00-0011800HRAIRFRAME1014

14-AUG-2009 H: 1800.00 D: +/-30 H: 1800.00 H: 653.30

AMM 71-31-00

LH ENG W403 HARNESS71 50-00

AIRFRAME1015

14-AUG-2009 H: 0

PN SN-UNKNOWN

RH ENG W404 HARNESS71 50-00

AIRFRAME1016

14-AUG-2009 H: 0

PN SN-UNKNOWN

LH ENG NACELLE AIR INLET ASSEMBLY71 60-01

AIRFRAME1017

14-AUG-2009 H: 0

500-36000-407 00100

RH ENG NACELLE AIR INLET ASSEMBLY71 60-01

AIRFRAME1018

14-AUG-2009 H: 0

500-36000-407 00097

NO. 1 ENGINE71 EN1

AIRFRAME1019

01-JUL-2009 H: 0

PW617F-E PCE-LC0108

NO. 2 ENGINE71 EN2

AIRFRAME1020

01-JUL-2009 H: 0

PW617F-E PCE-LC0111

NO. 1 ENGINE - PERFORM ENGINE OVERHAUL72 0000 OVERHAUL

ENGINE 11036

01-JUL-2009 H: 3500.00 H: +100 H: 3500.00 H: 2353.30

NO. 2 ENGINE - PERFORM ENGINE OVERHAUL72 0000 OVERHAUL

ENGINE 21142

01-JUL-2009 H: 3500.00 H: +100 H: 3500.00 H: 2353.30

VISUAL CHECK OF ENGINE MAINTENANCE PAGE FORENGINE DISPATCH AND EXCEEDANCE INFORMATION

72 00-00-001600HR/12MOAIRFRAME1023

14-SEP-2014H: 1038.80L: 883

M: 12H: 600.00

D: +/-30H: +/-30

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

AMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THELP COMPRESSOR INLET AREA

72 00-00-212-801

ENGINE 21130

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

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NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THELP COMPRESSOR INLET AREA

72 00-00-212-801

ENGINE 11024

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEAGB

72 00-00-212-802

ENGINE 11025

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEAGB

72 00-00-212-802

ENGINE 21131

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEBYPASS DUCT

72 00-00-212-803

ENGINE 21132

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEBYPASS DUCT

72 00-00-212-803

ENGINE 11026

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THETURBINE EXHAUST CASE

72 00-00-212-804

ENGINE 11027

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THETURBINE EXHAUST CASE

72 00-00-212-804

ENGINE 21133

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEFUEL DISTRIBUTION SYSTEM

72 00-00-212-805

ENGINE 21134

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEFUEL DISTRIBUTION SYSTEM

72 00-00-212-805

ENGINE 11028

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

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Intervals Tolerance Time At Inst Next DueInstalled

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NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEOIL DISTRIBUTION SYSTEM

72 00-00-212-806

ENGINE 11029

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEOIL DISTRIBUTION SYSTEM

72 00-00-212-806

ENGINE 21135

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 2 ENGINE - DETAILED INSPECTION OF THE LPCOMPRESSOR INLET AREA

72 00-00-215-801

ENGINE 21136

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - DETAILED INSPECTION OF THE LPCOMPRESSOR INLET AREA

72 00-00-215-801

ENGINE 11030

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - DETAILED INSPECTION OF THECOMPRESSOR CASE ASSEMBLY

72 00-00-215-802

ENGINE 11031

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

LMM 72-00-00

NO. 2 ENGINE - DETAILED INSPECTION OF THECOMPRESSOR CASE ASSEMBLY

72 00-00-215-802

ENGINE 21137

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

LMM 72-00-00

NO. 2 ENGINE - DETAILED INSPECTION OF THE FANCASE EXTERNAL AREA

72 00-00-215-803

ENGINE 21138

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

LMM 72-00-00

NO. 1 ENGINE - DETAILED INSPECTION OF THE FANCASE EXTERNAL AREA

72 00-00-215-803

ENGINE 11032

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

LMM 72-00-00

NO. 1 ENGINE - PERFORM ENGINE OIL SAMPLING ANDANALYSIS

72 00-00-280-801

ENGINE 11033

01-JUL-2009

LMM 72-00-00

NO. 2 ENGINE - PERFORM ENGINE OIL SAMPLING ANDANALYSIS

72 00-00-280-801

ENGINE 21139

01-JUL-2009

LMM 72-00-00

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Intervals Tolerance Time At Inst Next DueInstalled

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Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - SPECIAL DETAILED INSPECTION OF THEEMERGENCY FUEL SHUTOFF VALVE LEVER ASSEMBLY

72 00-00-290-815

ENGINE 21140

01-JUL-2009 H: 1800.00 H: +100 H: 1800.00 H: 653.30

LMM 72-00-00

NO. 1 ENGINE - SPECIAL DETAILED INSPECTION OF THEEMERGENCY FUEL SHUTOFF VALVE LEVER ASSEMBLY

72 00-00-290-815

ENGINE 11034

01-JUL-2009 H: 1800.00 H: +100 H: 1800.00 H: 653.30

LMM 72-00-00

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEENGINE OIL LEVEL

72 00-00-640-803

ENGINE 21141

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEENGINE OIL LEVEL

72 00-00-640-803

ENGINE 11035

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 72-00-00

NO. 1 ENGINE - PERFORM ENGINE HOT SECTIONINSPECTION

72 0001

ENGINE 11037

01-JUL-2009 H: 1750.00 H: +50 H: 1750.00 H: 603.30

NO. 2 ENGINE - PERFORM ENGINE HOT SECTIONINSPECTION

72 0001

ENGINE 21143

01-JUL-2009 H: 1750.00 H: +50 H: 1750.00 H: 603.30

NO. 1 ENGINE - PERFORM EEC FAULT INTERROGATION(TLD/LTD) ENGINE CONTROL SYSTEM

72 0002

ENGINE 11038

12-SEP-2013H: 786.90C: 722.00

LMM 72-00-02Notes: NO LONGER A REQUIRED ITEM.

NO. 2 ENGINE - PERFORM EEC FAULT INTERROGATION(TLD/LTD) ENGINE CONTROL SYSTEM

72 0002

ENGINE 21144

12-SEP-2013H: 786.90C: 722.00

LMM 72-00-02Notes: NO LONGER A REQUIRED ITEM.

NO. 1 ENGINE - INSPECT LOW UTILIZATION ENGINE(IF REQUIRED - SEE NOTES)

72 0003

ENGINE 11039

14-AUG-2009 M: 144 M: +3 14-AUG-2021 M: 78 D: 11

NO. 2 ENGINE - INSPECT LOW UTILIZATION ENGINE(IF REQUIRED - SEE NOTES)

72 0003

ENGINE 21145

14-AUG-2009 M: 144 M: +3 14-AUG-2021 M: 78 D: 11

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - FAN ROTOR72 0010 LIFE LIMIT

ENGINE 11040

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C3881-01 AATPWACK038

NO. 2 ENGINE - FAN ROTOR72 0010 LIFE LIMIT

ENGINE 21146

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C3881-01 AATPWACK001

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OFEXTERIOR SURFACES OF THE NACELLE FOR EVIDENCE OFOIL LEAKS

72 0030

ENGINE 11041

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OFEXTERIOR SURFACES OF THE NACELLE FOR EVIDENCE OFOIL LEAKS

72 0030

ENGINE 21147

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

NO. 1 ENGINE - HP TURBINE DISK72 1010 LIFE LIMIT

ENGINE 11042

01-JUL-2009 C: 5250.00 C: 0 C: 5250.00 C: 4297.00

35C3091-01 CRAZADLZ017

NO. 2 ENGINE - HP TURBINE DISK72 1010 LIFE LIMIT

ENGINE 21148

01-JUL-2009 C: 5250.00 C: 0 C: 5250.00 C: 4297.00

35C3091-01 A002HLT5

NO. 1 ENGINE - HP TURBINE DISK BALANCING ASSEMBLY72 1015

ENGINE 11043

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - HP TURBINE DISK BALANCING ASSEMBLY72 1015

ENGINE 21149

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - LP TURBINE DISK72 1020 LIFE LIMIT

ENGINE 11044

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C5392-01 CRAZADJS261

NO. 2 ENGINE - LP TURBINE DISK72 1020 LIFE LIMIT

ENGINE 21150

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C5392-01 CRAZADJS224

NO. 1 ENGINE - LP TURBINE DISK BALANCING ASSEMBLY72 1025

ENGINE 11045

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - LP TURBINE DISK BALANCING ASSEMBLY72 1025

ENGINE 21151

01-JUL-2009 H: 0

PN SN-UNKNOWN

Page 106 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - IMPELLER AND SHAFT ASSEMBLY72 3010 LIFE LIMIT

ENGINE 11046

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C4716-01 AAPPIAIF2031

NO. 2 ENGINE - IMPELLER AND SHAFT ASSEMBLY72 3010 LIFE LIMIT

ENGINE 21152

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C4716-01 AAPPIAIF2068

NO. 1 ENGINE - LP COMPRESSOR SHAFT72 3015 LIFE LIMIT

ENGINE 11047

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C4620-01 KWA4947117

NO. 2 ENGINE - LP COMPRESSOR SHAFT72 3015 LIFE LIMIT

ENGINE 21153

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C4620-01 KWA4947202

NO. 1 ENGINE - TOWERSHAFT BALL ANNULAR BEARING72 3020

ENGINE 11048

01-JUL-2009 H: 0

35C2168-01 FCN211471

NO. 2 ENGINE - TOWERSHAFT BALL ANNULAR BEARING72 3020

ENGINE 21154

01-JUL-2009 H: 0

35C2168-01 FCN201019

NO. 1 ENGINE - HIGH COMPRESSOR ROTOR BALANCINGASSEMBLY BALL ANNULAR BEARING

72 3025

ENGINE 11049

01-JUL-2009 H: 0

35C4832-01 FCN297052

NO. 2 ENGINE - HIGH COMPRESSOR ROTOR BALANCINGASSEMBLY BALL ANNULAR BEARING

72 3025

ENGINE 21155

01-JUL-2009 H: 0

35C4832-01 FCN297084

NO. 1 ENGINE - LP SHAFT BALL ANNULAR BEARING72 3030

ENGINE 11050

01-JUL-2009 H: 0

35C5051-01 FCN294070

NO. 2 ENGINE - LP SHAFT BALL ANNULAR BEARING72 3030

ENGINE 21156

01-JUL-2009 H: 0

35C5051-01 FCN294076

NO. 1 ENGINE - LP SHAFT BALL FLANGED BEARING72 3035

ENGINE 11051

01-JUL-2009 H: 0

35C4831-01 FCN296265

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - LP SHAFT BALL FLANGED BEARING72 3035

ENGINE 21157

01-JUL-2009 H: 0

35C4831-01 FCN296245

NO. 1 ENGINE - TOWERSHAFT ROLLER BEARING72 3040

ENGINE 11052

01-JUL-2009 H: 0

3107496-01 FCN283065

NO. 2 ENGINE - TOWERSHAFT ROLLER BEARING72 3040

ENGINE 21158

01-JUL-2009 H: 0

3107496-01 FCN221493

NO. 1 ENGINE - HIGH COMPRESSOR ROTOR ROLLERBEARING

72 3045

ENGINE 11053

01-JUL-2009 H: 0

35C4534-01 FCN289524

NO. 2 ENGINE - HIGH COMPRESSOR ROTOR ROLLERBEARING

72 3045

ENGINE 21159

01-JUL-2009 H: 0

35C4534-01 FCN289533

NO. 1 ENGINE - FAN CASE ASSEMBLY72 3050

ENGINE 11054

01-JUL-2009 H: 0

35C5325-01 NYAB00004196

NO. 2 ENGINE - FAN CASE ASSEMBLY72 3050

ENGINE 21160

01-JUL-2009 H: 0

35C5325-01 NYAB00004458

NO. 1 ENGINE - COMPRESSOR CASE ASSEMBLY72 3055

ENGINE 11055

01-JUL-2009 H: 0

35C4935-01 RWA36C296

NO. 2 ENGINE - COMPRESSOR CASE ASSEMBLY72 3055

ENGINE 21161

01-JUL-2009 H: 0

35C4935-01 RWA42C211

NO. 1 ENGINE - HIGH PRESSURE DIFFUSER CASEASSEMBLY

72 3060

ENGINE 11056

01-JUL-2009 H: 0

35C4860-01 RWA45C133

NO. 2 ENGINE - HIGH PRESSURE DIFFUSER CASEASSEMBLY

72 3060

ENGINE 21162

01-JUL-2009 H: 0

35C4860-01 RWA36C552

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - LOWER SPIRAL BEVEL GEARBOX DRIVEGEAR SHAFT

72 3065

ENGINE 11057

01-JUL-2009 H: 0

35C5334-01 PKAAA247065

NO. 2 ENGINE - LOWER SPIRAL BEVEL GEARBOX DRIVEGEAR SHAFT

72 3065

ENGINE 21163

01-JUL-2009 H: 0

35C5334-01 PKAAA257737

NO. 1 ENGINE - UPPER SPIRAL BEVEL GEARBOX DRIVEGEAR SHAFT

72 3070

ENGINE 11058

01-JUL-2009 H: 0

35C3627-01 PKAAA246876

NO. 2 ENGINE - UPPER SPIRAL BEVEL GEARBOX DRIVEGEAR SHAFT

72 3070

ENGINE 21164

01-JUL-2009 H: 0

35C3627-01 PKAAA246891

NO. 1 ENGINE - SPIRAL BEVEL GEARBOX DRIVE GEAR72 3075

ENGINE 11059

01-JUL-2009 H: 0

35C3628-01 PKAAA266288

NO. 2 ENGINE - SPIRAL BEVEL GEARBOX DRIVE GEAR72 3075

ENGINE 21165

01-JUL-2009 H: 0

35C3628-01 PKAAA266291

NO. 1 ENGINE - IMPELLER CENTRIFUGAL ASSEMBLY72 3080

ENGINE 11060

01-JUL-2009 H: 0

35C4714-01 AAPPIAIF2031

NO. 2 ENGINE - IMPELLER CENTRIFUGAL ASSEMBLY72 3080

ENGINE 21166

01-JUL-2009 H: 0

35C4714-01 AAPPIAIF2068

NO. 1 ENGINE - FRONT NO. 4 SEAL BEARING RUNNER72 3085

ENGINE 11061

01-JUL-2009 H: 0

35C5326-01 EYA16775

NO. 2 ENGINE - FRONT NO. 4 SEAL BEARING RUNNER72 3085

ENGINE 21167

01-JUL-2009 H: 0

35C5326-01 EYA17285

NO. 1 ENGINE - REAR NO. 4 SEAL BEARING RUNNER72 3090

ENGINE 11062

01-JUL-2009 H: 0

35C4623-01 EYA17305

Page 109 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - REAR NO. 4 SEAL BEARING RUNNER72 3090

ENGINE 21168

01-JUL-2009 H: 0

35C4623-01 EYA17164

NO. 1 ENGINE - COMPRESSOR STATOR ASSEMBLY72 3095

ENGINE 11063

01-JUL-2009 H: 0

35C5330-01 PKAAA265767

NO. 2 ENGINE - COMPRESSOR STATOR ASSEMBLY72 3095

ENGINE 21169

01-JUL-2009 H: 0

35C5330-01 PKAAA265769

NO. 1 ENGINE - HOUSING IMPELLER ASSEMBLY72 3110

ENGINE 11064

01-JUL-2009 H: 0

35C5211-01 RWA34C574

NO. 2 ENGINE - HOUSING IMPELLER ASSEMBLY72 3110

ENGINE 21170

01-JUL-2009 H: 0

35C5211-01 RWA31C740

NO. 1 ENGINE - INNER COMBUSTOR CHAMBER LINERASSEMBLY

72 4010

ENGINE 11065

01-JUL-2009 H: 0

35C5050-01 A002LK24

NO. 2 ENGINE - INNER COMBUSTOR CHAMBER LINERASSEMBLY

72 4010

ENGINE 21171

01-JUL-2009 H: 0

35C5050-01 A002LL1A

NO. 1 ENGINE - OUTER COMBUSTOR CHAMBER LINERASSEMBLY

72 4015

ENGINE 11066

01-JUL-2009 H: 0

35C5053-01 A002LL1E

NO. 2 ENGINE - OUTER COMBUSTOR CHAMBER LINERASSEMBLY

72 4015

ENGINE 21172

01-JUL-2009 H: 0

35C5053-01 A002LP90

NO. 1 ENGINE - HP COMPRESSOR ROTOR72 5010 LIFE LIMIT

ENGINE 11067

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C4781-01 AATPWACG020

NO. 2 ENGINE - HP COMPRESSOR ROTOR72 5010 LIFE LIMIT

ENGINE 21173

01-JUL-2009 C:10500.00

C: 0 C: 10500.00 C: 9547.00

35C4781-01 AATPWACJ019

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - BALL ROLLER ANNULAR BEARING72 5015

ENGINE 11068

01-JUL-2009 H: 0

35C0590-02 FCN222434

NO. 2 ENGINE - BALL ROLLER ANNULAR BEARING72 5015

ENGINE 21174

01-JUL-2009 H: 0

35C0590-02 FCN223303

NO. 1 ENGINE - HIGH PRESSURE TURBINE CASE ASSEMBLY72 5020

ENGINE 11069

01-JUL-2009 H: 0

35C4726-01 RWA17C140

NO. 2 ENGINE - HIGH PRESSURE TURBINE CASE ASSEMBLY72 5020

ENGINE 21175

01-JUL-2009 H: 0

35C4726-01 RWA34C143

NO. 1 ENGINE - TURBINE EXHAUST CASE ASSEMBLY72 5025

ENGINE 11070

01-JUL-2009 H: 0

35C4755-01 DYA328926

NO. 2 ENGINE - TURBINE EXHAUST CASE ASSEMBLY72 5025

ENGINE 21176

01-JUL-2009 H: 0

35C4755-01 DYA331428

NO. 1 ENGINE - NO. 5 SEAL BEARING RUNNER72 5030

ENGINE 11071

01-JUL-2009 H: 0

35C4886-01 EYA17089

NO. 2 ENGINE - NO. 5 SEAL BEARING RUNNER72 5030

ENGINE 21177

01-JUL-2009 H: 0

35C4886-01 EYA17338

NO. 1 ENGINE - HIGH PRESSURE TURBINE TIE SHAFT72 5035

ENGINE 11072

01-JUL-2009 H: 0

35C5549-01 UNA020823

NO. 2 ENGINE - HIGH PRESSURE TURBINE TIE SHAFT72 5035

ENGINE 21178

01-JUL-2009 H: 0

35C5549-01 UNA020774

NO. 1 ENGINE - HIGH PRESSURE TURBINE VANE-RING72 5040

ENGINE 11073

01-JUL-2009 H: 0

35C5501CL01 PDAHDDCW01

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - HIGH PRESSURE TURBINE VANE-RING72 5040

ENGINE 21179

01-JUL-2009 H: 0

35C5501CL01 PDAHB6EB01

NO. 1 ENGINE - LOW PRESSURE TURBINE VANE-RING72 5045

ENGINE 11074

01-JUL-2009 H: 0

35C4622CL01 HLA062AA254

NO. 2 ENGINE - LOW PRESSURE TURBINE VANE-RING72 5045

ENGINE 21180

01-JUL-2009 H: 0

35C4622CL01 HLA062AA297

NO. 1 ENGINE - NO.1 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11075

01-JUL-2009 H: 0

35C5521-01 HWCM2649

NO. 1 ENGINE - NO.10 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11076

01-JUL-2009 H: 0

35C5521-01 HWCM2694

NO. 1 ENGINE - NO.11 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11077

01-JUL-2009 H: 0

35C5521-01 HWCM2702

NO. 1 ENGINE - NO.12 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11078

01-JUL-2009 H: 0

35C5521-01 HWCM2706

NO. 1 ENGINE - NO.13 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11079

01-JUL-2009 H: 0

35C5521-01 HWCM9854

NO. 1 ENGINE - NO.14 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11080

01-JUL-2009 H: 0

35C5521-01 HWCM9885

NO. 1 ENGINE - NO.15 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11081

01-JUL-2009 H: 0

35C5521-01 HWCN5922

NO. 1 ENGINE - NO.16 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11082

01-JUL-2009 H: 0

35C5521-01 HWCN5930

Page 112 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 113: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - NO.17 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11083

01-JUL-2009 H: 0

35C5521-01 HWCN5932

NO. 1 ENGINE - NO.18 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11084

01-JUL-2009 H: 0

35C5521-01 HWCN5937

NO. 1 ENGINE - NO.19 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11085

01-JUL-2009 H: 0

35C5521-01 HWCN5993

NO. 1 ENGINE - NO.2 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11086

01-JUL-2009 H: 0

35C5521-01 HWCM2652

NO. 1 ENGINE - NO.20 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11087

01-JUL-2009 H: 0

35C5521-01 HWCN6022

NO. 1 ENGINE - NO.21 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11088

01-JUL-2009 H: 0

35C5521-01 HWCN6026

NO. 1 ENGINE - NO.22 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11089

01-JUL-2009 H: 0

35C5521-01 HWCN6035

NO. 1 ENGINE - NO.23 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11090

01-JUL-2009 H: 0

35C5521-01 HWCN6040

NO. 1 ENGINE - NO.24 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11091

01-JUL-2009 H: 0

35C5521-01 HWCN6046

NO. 1 ENGINE - NO.25 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11092

01-JUL-2009 H: 0

35C5521-01 HWCN6052

NO. 1 ENGINE - NO.26 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11093

01-JUL-2009 H: 0

35C5521-01 HWCN6055

Page 113 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 114: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - NO.27 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11094

01-JUL-2009 H: 0

35C5521-01 HWCN6065

NO. 1 ENGINE - NO.28 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11095

01-JUL-2009 H: 0

35C5521-01 HWCN6069

NO. 1 ENGINE - NO.29 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11096

01-JUL-2009 H: 0

35C5521-01 HWCN6071

NO. 1 ENGINE - NO.3 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11097

01-JUL-2009 H: 0

35C5521-01 HWCM2659

NO. 1 ENGINE - NO.30 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11098

01-JUL-2009 H: 0

35C5521-01 HWCN6072

NO. 1 ENGINE - NO.31 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11099

01-JUL-2009 H: 0

35C5521-01 HWCN6076

NO. 1 ENGINE - NO.32 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11100

01-JUL-2009 H: 0

35C5521-01 HWCN6083

NO. 1 ENGINE - NO.33 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11101

01-JUL-2009 H: 0

35C5521-01 HWCN6085

NO. 1 ENGINE - NO.34 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11102

01-JUL-2009 H: 0

35C5521-01 HWCN6093

NO. 1 ENGINE - NO.35 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11103

01-JUL-2009 H: 0

35C5521-01 HWCN6094

NO. 1 ENGINE - NO.36 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11104

01-JUL-2009 H: 0

35C5521-01 HWCN6098

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - NO.37 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11105

01-JUL-2009 H: 0

35C5521-01 HWCN6109

NO. 1 ENGINE - NO.38 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11106

01-JUL-2009 H: 0

35C5521-01 HWCN6111

NO. 1 ENGINE - NO.39 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11107

01-JUL-2009 H: 0

35C5521-01 HWCN6112

NO. 1 ENGINE - NO.4 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11108

01-JUL-2009 H: 0

35C5521-01 HWCM2663

NO. 1 ENGINE - NO.40 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11109

01-JUL-2009 H: 0

35C5521-01 HWCN6118

NO. 1 ENGINE - NO.41 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11110

01-JUL-2009 H: 0

35C5521-01 HWCN6128

NO. 1 ENGINE - NO.42 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11111

01-JUL-2009 H: 0

35C5521-01 HWCN6141

NO. 1 ENGINE - NO.43 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11112

01-JUL-2009 H: 0

35C5521-01 HWCN6142

NO. 1 ENGINE - NO.44 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11113

01-JUL-2009 H: 0

35C5521-01 HWCN6216

NO. 1 ENGINE - NO.45 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11114

01-JUL-2009 H: 0

35C5521-01 HWCN6221

NO. 1 ENGINE - NO.46 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11115

01-JUL-2009 H: 0

35C5521-01 HWCN6560

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - NO.47 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11116

01-JUL-2009 H: 0

35C5521-01 HWCN6564

NO. 1 ENGINE - NO.48 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11117

01-JUL-2009 H: 0

35C5521-01 HWCN6657

NO. 1 ENGINE - NO.49 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11118

01-JUL-2009 H: 0

35C5521-01 HWCN7048

NO. 1 ENGINE - NO.5 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11119

01-JUL-2009 H: 0

35C5521-01 HWCM2670

NO. 1 ENGINE - NO.50 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11120

01-JUL-2009 H: 0

35C5521-01 HWCN7077

NO. 1 ENGINE - NO.6 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11121

01-JUL-2009 H: 0

35C5521-01 HWCM2675

NO. 1 ENGINE - NO.7 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11122

01-JUL-2009 H: 0

35C5521-01 HWCM2681

NO. 1 ENGINE - NO.8 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11123

01-JUL-2009 H: 0

35C5521-01 HWCM2689

NO. 1 ENGINE - NO.9 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 11124

01-JUL-2009 H: 0

35C5521-01 HWCM2691

NO. 2 ENGINE - NO.1 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21181

01-JUL-2009 H: 0

35C5521-01 HWCN6212

NO. 2 ENGINE - NO.10 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21182

01-JUL-2009 H: 0

35C5521-01 HWCN6261

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - NO.11 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21183

01-JUL-2009 H: 0

35C5521-01 HWCN6268

NO. 2 ENGINE - NO.12 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21184

01-JUL-2009 H: 0

35C5521-01 HWCN6545

NO. 2 ENGINE - NO.13 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21185

01-JUL-2009 H: 0

35C5521-01 HWCN6550

NO. 2 ENGINE - NO.14 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21186

01-JUL-2009 H: 0

35C5521-01 HWCN6558

NO. 2 ENGINE - NO.15 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21187

01-JUL-2009 H: 0

35C5521-01 HWCN6563

NO. 2 ENGINE - NO.16 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21188

01-JUL-2009 H: 0

35C5521-01 HWCN6566

NO. 2 ENGINE - NO.17 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21189

01-JUL-2009 H: 0

35C5521-01 HWCN6577

NO. 2 ENGINE - NO.18 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21190

01-JUL-2009 H: 0

35C5521-01 HWCN6579

NO. 2 ENGINE - NO.19 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21191

01-JUL-2009 H: 0

35C5521-01 HWCN6581

NO. 2 ENGINE - NO.2 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21192

01-JUL-2009 H: 0

35C5521-01 HWCN6213

NO. 2 ENGINE - NO.20 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21193

01-JUL-2009 H: 0

35C5521-01 HWCN6583

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - NO.21 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21194

01-JUL-2009 H: 0

35C5521-01 HWCN6639

NO. 2 ENGINE - NO.22 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21195

01-JUL-2009 H: 0

35C5521-01 HWCN6644

NO. 2 ENGINE - NO.23 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21196

01-JUL-2009 H: 0

35C5521-01 HWCN6645

NO. 2 ENGINE - NO.24 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21197

01-JUL-2009 H: 0

35C5521-01 HWCN6646

NO. 2 ENGINE - NO.25 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21198

01-JUL-2009 H: 0

35C5521-01 HWCN6647

NO. 2 ENGINE - NO.26 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21199

01-JUL-2009 H: 0

35C5521-01 HWCN6666

NO. 2 ENGINE - NO.27 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21200

01-JUL-2009 H: 0

35C5521-01 HWCN6674

NO. 2 ENGINE - NO.28 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21201

01-JUL-2009 H: 0

35C5521-01 HWCN6678

NO. 2 ENGINE - NO.29 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21202

01-JUL-2009 H: 0

35C5521-01 HWCN6679

NO. 2 ENGINE - NO.3 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21203

01-JUL-2009 H: 0

35C5521-01 HWCN6226

NO. 2 ENGINE - NO.30 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21204

01-JUL-2009 H: 0

35C5521-01 HWCN6683

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - NO.31 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21205

01-JUL-2009 H: 0

35C5521-01 HWCN6686

NO. 2 ENGINE - NO.32 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21206

01-JUL-2009 H: 0

35C5521-01 HWCN6697

NO. 2 ENGINE - NO.33 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21207

01-JUL-2009 H: 0

35C5521-01 HWCN6701

NO. 2 ENGINE - NO.34 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21208

01-JUL-2009 H: 0

35C5521-01 HWCN6755

NO. 2 ENGINE - NO.35 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21209

01-JUL-2009 H: 0

35C5521-01 HWCN6758

NO. 2 ENGINE - NO.36 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21210

01-JUL-2009 H: 0

35C5521-01 HWCN7045

NO. 2 ENGINE - NO.37 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21211

01-JUL-2009 H: 0

35C5521-01 HWCN7047

NO. 2 ENGINE - NO.38 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21212

01-JUL-2009 H: 0

35C5521-01 HWCN7050

NO. 2 ENGINE - NO.39 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21213

01-JUL-2009 H: 0

35C5521-01 HWCN7053

NO. 2 ENGINE - NO.4 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21214

01-JUL-2009 H: 0

35C5521-01 HWCN6228

NO. 2 ENGINE - NO.40 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21215

01-JUL-2009 H: 0

35C5521-01 HWCN7056

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - NO.41 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21216

01-JUL-2009 H: 0

35C5521-01 HWCN7062

NO. 2 ENGINE - NO.42 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21217

01-JUL-2009 H: 0

35C5521-01 HWCN7067

NO. 2 ENGINE - NO.43 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21218

01-JUL-2009 H: 0

35C5521-01 HWCN7071

NO. 2 ENGINE - NO.44 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21219

01-JUL-2009 H: 0

35C5521-01 HWCN7072

NO. 2 ENGINE - NO.45 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21220

01-JUL-2009 H: 0

35C5521-01 HWCN7073

NO. 2 ENGINE - NO.46 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21221

01-JUL-2009 H: 0

35C5521-01 HWCN7427

NO. 2 ENGINE - NO.47 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21222

01-JUL-2009 H: 0

35C5521-01 HWCN7432

NO. 2 ENGINE - NO.48 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21223

01-JUL-2009 H: 0

35C5521-01 HWCN7443

NO. 2 ENGINE - NO.49 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21224

01-JUL-2009 H: 0

35C5521-01 HWCN7447

NO. 2 ENGINE - NO.5 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21225

01-JUL-2009 H: 0

35C5521-01 HWCN6240

NO. 2 ENGINE - NO.50 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21226

01-JUL-2009 H: 0

35C5521-01 HWCN8829

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - NO.6 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21227

01-JUL-2009 H: 0

35C5521-01 HWCN6247

NO. 2 ENGINE - NO.7 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21228

01-JUL-2009 H: 0

35C5521-01 HWCN6251

NO. 2 ENGINE - NO.8 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21229

01-JUL-2009 H: 0

35C5521-01 HWCN6257

NO. 2 ENGINE - NO.9 HIGH PRESSURE TURBINE BLADE72 5050

ENGINE 21230

01-JUL-2009 H: 0

35C5521-01 HWCN6260

NO. 1 ENGINE - FLANGED ROLLER BEARING72 6010

ENGINE 11125

01-JUL-2009 H: 0

3107449-01 FCN283963

NO. 2 ENGINE - FLANGED ROLLER BEARING72 6010

ENGINE 21231

01-JUL-2009 H: 0

3107449-01 FCN283970

NO. 1 ENGINE - STARTER GEARSHAFT BALL FLANGEDBEARING

72 6015

ENGINE 11126

01-JUL-2009 H: 0

35C3615-01 FCN288079

NO. 2 ENGINE - STARTER GEARSHAFT BALL FLANGEDBEARING

72 6015

ENGINE 21232

01-JUL-2009 H: 0

35C3615-01 FCN294952

NO. 1 ENGINE - ACCESSORY DRIVE GEAR SHAFT72 6020

ENGINE 11127

01-JUL-2009 H: 0

35C5333-01 PKAAA243160

NO. 2 ENGINE - ACCESSORY DRIVE GEAR SHAFT72 6020

ENGINE 21233

01-JUL-2009 H: 0

35C5333-01 PKAAA251503

NO. 1 ENGINE - ACCESSORY GEARBOX HOUSING ASSEMBLY72 6025

ENGINE 11128

01-JUL-2009 H: 0

35C5141-01 RWA37C637

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - ACCESSORY GEARBOX HOUSING ASSEMBLY72 6025

ENGINE 21234

01-JUL-2009 H: 0

35C5141-01 RWA41C044

NO. 1 ENGINE - BYPASS DUCT ASSEMBLY72 7010

ENGINE 11129

01-JUL-2009 H: 0

35C5332-01 FDA5584380

NO. 2 ENGINE - BYPASS DUCT ASSEMBLY72 7010

ENGINE 21235

01-JUL-2009 H: 0

35C5332-01 FDA5584408

NO. 1 ENGINE - FUEL TO OIL HEAT EXCHANGER73 1002

ENGINE 11256

01-JUL-2009 H: 0

35C4540-01 WA36062

NO. 2 ENGINE - FUEL TO OIL HEAT EXCHANGER73 1002

ENGINE 21269

01-JUL-2009 H: 0

35C4540-01 WA36089

NO. 2 ENGINE - DISCARD THE FUEL FILTER73 10-05-000-801

ENGINE 21263

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

NO. 1 ENGINE - DISCARD THE FUEL FILTER73 10-05-000-801

ENGINE 11250

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

NO. 1 ENGINE - DETAILED INSPECTION FUEL FILTER73 10-05-220-801

ENGINE 11251

14-SEP-2014H: 1038.80C: 883.00

M: 12 14-SEP-2015 M: 7 D: 11

LMM 73-10-05

NO. 2 ENGINE - DETAILED INSPECTION FUEL FILTER73 10-05-220-801

ENGINE 21264

14-SEP-2014H: 1038.80C: 883.00

M: 12 14-SEP-2015 M: 7 D: 11

LMM 73-10-05

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEFSOV CABLE

73 10-07-212-801

ENGINE 21265

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-10-07

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEFSOV CABLE

73 10-07-212-801

ENGINE 11252

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-10-07

NO. 1 ENGINE - FUEL MANIFOLD73 1111

ENGINE 11257

01-JUL-2009 H: 0

35C4916-01 DE1BDF0656

NO. 2 ENGINE - FUEL MANIFOLD73 1111

ENGINE 21270

01-JUL-2009 H: 0

35C4916-01 DE1BCP0847

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEENGINE WIRING HARNESS

73 20-02-212-801

ENGINE 11253

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-20-02

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEENGINE WIRING HARNESS

73 20-02-212-801

ENGINE 21266

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-20-02

NO. 1 ENGINE - FUEL METERING UNIT73 2101

ENGINE 11258

13-SEP-2011H: 504.20C: 504.00

H: 0

1009000-4 F70328

RH ENG FULL AUTHORITY DIGITAL FADEC73 21-01

AIRFRAME1237

14-AUG-2009 H: 0

35C4812-02 2008050011

NO. 2 ENGINE - FUEL METERING UNIT73 2101

ENGINE 21271

13-SEP-2011H: 504.20C: 504.00

H: 0

1009000-4 F70886

LH ENG FULL AUTHORITY DIGITAL FADEC73 21-01

AIRFRAME1236

14-AUG-2009 H: 0

35C4812-02 2008110757

NO.1 W205 FADEC CH B FUS CTRL HARNESS73 21-02

AIRFRAME1238

14-AUG-2009 H: 0

PN SN-UNKNOWN

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO.2 W205 FADEC CH B FUS CTRL HARNESS73 21-02

AIRFRAME1239

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.1 W203 FADEC CH A FUS CTRL HARNESS73 21-03

AIRFRAME1240

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.2 W203 FADEC CH A FUS CTRL HARNESS73 21-03

AIRFRAME1241

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - ELECTRICAL WIRING HARNESS73 2108

ENGINE 11259

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - ELECTRICAL WIRING HARNESS73 2108

ENGINE 21272

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO.1 W307 FADEC CH B HARNESS73 21-09

AIRFRAME1242

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.2 W307 FADEC CH B HARNESS73 21-09

AIRFRAME1243

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.2 W305 FADEC CH A HARNESS73 21-10

AIRFRAME1245

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO.1 W305 FADEC CH A HARNESS73 21-10

AIRFRAME1244

14-AUG-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - ENGINE ELECTRONIC CONTROL73 2244

ENGINE 11260

13-SEP-2011H: 504.20C: 504.00

H: 0

1009211-2-004 2009110013

NO. 2 ENGINE - ENGINE ELECTRONIC CONTROL73 2244

ENGINE 21273

13-SEP-2011H: 504.20C: 504.00

H: 0

1009211-2-004 2009110020

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - FUEL FILTER BYPASS INDICATOR73 3002

ENGINE 21274

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - FUEL FILTER BYPASS INDICATOR73 3002

ENGINE 11261

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - VISUAL CHECK OF THE FUEL FILTERBYPASS INDICATOR POPUP BUTTON

73 30-02-212-801

ENGINE 21267

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-30-02

NO. 1 ENGINE - VISUAL CHECK OF THE FUEL FILTERBYPASS INDICATOR POPUP BUTTON

73 30-02-212-801

ENGINE 11254

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-30-02

NO. 1 ENGINE - DETAILED INSPECTION OF THE FUELFILTER BYPASS INDICATOR

73 30-02-215-801

ENGINE 11255

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-30-02

NO. 2 ENGINE - DETAILED INSPECTION OF THE FUELFILTER BYPASS INDICATOR

73 30-02-215-801

ENGINE 21268

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 73-30-02

NO. 1 ENGINE - FUEL FILTER IMPENDING BYPASS SWITCH73 3010

ENGINE 11262

13-SEP-2011H: 504.20C: 504.00

M: 4

35C5593-01 8003818876

NO. 2 ENGINE - FUEL FILTER IMPENDING BYPASS SWITCH73 3010

ENGINE 21275

13-SEP-2011H: 504.20C: 504.00

M: 4

35C5593-01 8003809120

LH ENG FUEL FLOW METER73 33-01

AIRFRAME1246

14-AUG-2009 H: 0

8TJ300AAF2 21243

RH ENG FUEL FLOW METER73 33-01

AIRFRAME1247

14-AUG-2009 H: 0

8TJ300AAF2 21242

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

GENERAL VISUAL INSPECTION LEFT L/HIRF PROTECTIONON THE FADEC

73H73-01-240-001 6000HR/96MO

AIRFRAME1248

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 73-21-01

GENERAL VISUAL INSPECTION RIGHT L/HIRF PROTECTIONON THE FADEC

73H73-01-240-001 6000HR/96MO

AIRFRAME1249

14-AUG-2009 M: 96H: 6000.00

D: +/-30H: +/-30

14-AUG-2017H: 6000.00

M: 30 D: 11H: 4853.30

AMM 73-21-01

NO. 2 ENGINE - IGNITION EXCITER74 1001

ENGINE 21285

01-JUL-2009 H: 0

35C5472-01 WDA108679

NO. 1 ENGINE - IGNITION EXCITER74 1001

ENGINE 11278

01-JUL-2009 H: 0

35C5472-01 WDA108732

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEIGNITION EXCITER

74 10-01-212-801

ENGINE 11276

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 74-10-01

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEIGNITION EXCITER

74 10-01-212-801

ENGINE 21283

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 74-10-01

NO. 1 ENGINE - LEFT IGNITER CABLE74 1002

ENGINE 11279

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - LEFT IGNITER CABLE74 1002

ENGINE 21286

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - RIGHT IGNITER CABLE74 1003

ENGINE 11280

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - RIGHT IGNITER CABLE74 1003

ENGINE 21287

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - INBOARD SPARK IGNITER74 1004 DISCARD

ENGINE 11281

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 0 H: 1638.80 H: 492.10

35C2353-02 SN-UNKNOWN

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - INBOARD SPARK IGNITER74 1004 DISCARD

ENGINE 21288

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 0 H: 1638.80 H: 492.10

35C2353-02 SN-UNKNOWN

NO. 1 ENGINE - OUTBOARD SPARK IGNITER74 1005 DISCARD

ENGINE 11282

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 0 H: 1638.80 H: 492.10

35C2353-02 SN-UNKNOWN

NO. 2 ENGINE - OUTBOARD SPARK IGNITER74 1005 DISCARD

ENGINE 21289

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 0 H: 1638.80 H: 492.10

35C2353-02 SN-UNKNOWN

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEIGNITION CABLES

74 20-01-212-801

ENGINE 11277

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 74-20-01

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEIGNITION CABLES

74 20-01-212-801

ENGINE 21284

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 74-20-01

NO. 1 ENGINE - BLEED VALVE ACTUATOR75 1003

ENGINE 11291

01-JUL-2009 H: 0

35C2851-02 16539914

NO. 2 ENGINE - BLEED VALVE ACTUATOR75 1003

ENGINE 21293

01-JUL-2009 H: 0

35C2851-02 16543570

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THEBVA

75 30-01-212-801

ENGINE 11290

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 75-30-01

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THEBVA

75 30-01-212-801

ENGINE 21292

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 75-30-01

THROTTLE CONTROL QUADRANT ASSEMBLY76 11-03

AIRFRAME1294

14-AUG-2009 H: 0

6990010-11 1079

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - T6 THERMOCOUPLE HARNESS ASSEMBLY77 2002

ENGINE 11297

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - T6 THERMOCOUPLE HARNESS ASSEMBLY77 2002

ENGINE 21301

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - GENERAL VISUAL INSPECTION OF THET6 TEMPERATURE INDICATING SYSTEM

77 20-02-212-801

ENGINE 11295

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 77-20-02

NO. 2 ENGINE - GENERAL VISUAL INSPECTION OF THET6 TEMPERATURE INDICATING SYSTEM

77 20-02-212-801

ENGINE 21299

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 77-20-02

NO. 1 ENGINE - OPERATIONAL CHECK OF THE T6TEMPERATURE INDICATING SYSTEM

77 20-02-710-801

ENGINE 11296

20-SEP-2012H: 662.00C: 637.00

M: 36H: 1800.00

D: +30H: +100

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

LMM 77-20-02

NO. 2 ENGINE - OPERATIONAL CHECK OF THE T6TEMPERATURE INDICATING SYSTEM

77 20-02-710-801

ENGINE 21300

20-SEP-2012H: 662.00C: 637.00

M: 36H: 1800.00

D: +30H: +100

20-SEP-2015H: 2462.00

M: 7 D: 17H: 1315.30

LMM 77-20-02

NO. 1 ENGINE - DATA COLLECTION UNIT77 2103

ENGINE 11298

01-JUL-2009 H: 0

35C5571-01 DP09-1178

NO. 2 ENGINE - DATA COLLECTION UNIT77 2103

ENGINE 21302

01-JUL-2009 H: 0

35C5571-01 DP09-1407

NO. 1 ENGINE - DISCARD OIL FILTER79 20-01-000-801

ENGINE 11305

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

NO. 2 ENGINE - DISCARD OIL FILTER79 20-01-000-801

ENGINE 21313

14-SEP-2014H: 1038.80C: 883.00

H: 600.00 H: +10% H: 1638.80 H: 492.10

NO. 1 ENGINE - AIR COOLED OIL COOLER79 2007

ENGINE 11309

01-JUL-2009 H: 0

35C2495-05 WA35998

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - AIR COOLED OIL COOLER79 2007

ENGINE 21317

01-JUL-2009 H: 0

35C2495-05 WA36010

NO. 1 ENGINE - P3 AIR COOLER ASSEMBLY79 2010

ENGINE 11310

01-JUL-2009 H: 0

35C5545-01 TYAB0930

NO. 2 ENGINE - P3 AIR COOLER ASSEMBLY79 2010

ENGINE 21318

01-JUL-2009 H: 0

35C5545-01 TYAB0907

NO. 2 ENGINE - CHIP DETECTOR79 3001

ENGINE 21319

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - CHIP DETECTOR79 3001

ENGINE 11311

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - OPERATIONAL CHECK OF THE CHIPDETECTOR

79 30-01-720-801

ENGINE 21314

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 79-30-01

NO. 1 ENGINE - OPERATIONAL CHECK OF THE CHIPDETECTOR

79 30-01-720-801

ENGINE 11306

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 79-30-01

NO. 2 ENGINE - OIL FILTER IMPENDING BYPASSINDICATOR

79 3002

ENGINE 21320

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 1 ENGINE - OIL FILTER IMPENDING BYPASSINDICATOR

79 3002

ENGINE 11312

01-JUL-2009 H: 0

PN SN-UNKNOWN

NO. 2 ENGINE - VISUAL CHECK OF THE OIL FILTERIMPENDING BYPASS INDICATOR POPUP BUTTON

79 30-02-210-802

ENGINE 21315

01-JUL-2009

LMM 79-30-02

NO. 1 ENGINE - VISUAL CHECK OF THE OIL FILTERIMPENDING BYPASS INDICATOR POPUP BUTTON

79 30-02-210-802

ENGINE 11307

01-JUL-2009

LMM 79-30-02

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - DETAILED INSPECTION OF THE OILFILTER IMPENDING BYPASS INDICATOR

79 30-02-215-801

ENGINE 11308

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 79-30-02

NO. 2 ENGINE - DETAILED INSPECTION OF THE OILFILTER IMPENDING BYPASS INDICATOR

79 30-02-215-801

ENGINE 21316

14-SEP-2014H: 1038.80C: 883.00

M: 12H: 600.00

D: +30H: +10%

14-SEP-2015H: 1638.80

M: 7 D: 11H: 492.10

LMM 79-30-02

RH ENG OIL TEMPERATURE PRESSURE SENSOR79 31-01

AIRFRAME1304

14-AUG-2009 H: 0

PT9903-275-40012 0808-2231

LH ENG OIL TEMPERATURE PRESSURE SENSOR79 31-01

AIRFRAME1303

14-AUG-2009 H: 0

PT9903-275-40012 0209-2349

ELECTRICAL POWER - REPLACEMENT OF THE STARTERGENERATORS ALERT SERVICE BULLETIN

ASB 500-24-A007 N/A

AIRFRAME1383Notes: NOT APPLICABLE - SUPERSEDED BY SB 500-24-A007/01

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT OF LEFT-HAND (LH)STARTER GENERATOR

ASB 500-24-A007PART I

N/A

AIRFRAME1384

Notes: NOT APPLICABLE - SUPERSEDED BY SB 500-24-A007/01

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT OF RIGHT-HAND (RH)STARTER GENERATOR

ASB 500-24-A007PART II

N/A

AIRFRAME1385

Notes: NOT APPLICABLE - SUPERSEDED BY SB 500-24-A007/01

ELECTRICAL POWER - REPLACEMENT OF THE STARTERGENERATORS ALERT SERVICE BULLETIN.

ASB 500-24-A007R1

COMPLIED WITH

AIRFRAME1386

27-APR-2011H: 409.30L: 435

Notes: COMPLIED WITH - SB COMPLIED WITH.

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT OF LEFT-HAND (LH)STARTER GENERATOR.

ASB 500-24-A007R1 PART I

COMPLIED WITH

AIRFRAME1387

27-APR-2011H: 409.30L: 435

Notes: COMPLIED WITH - SB COMPLIED WITH.

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT OF RIGHT-HAND (RH)STARTER GENERATOR.

ASB 500-24-A007R1 PII

COMPLIED WITH

AIRFRAME1388

27-APR-2011H: 409.30L: 435

Notes: COMPLIED WITH - SB COMPLIED WITH.

ELECTRICAL POWER - REPLACEMENT OF THE STARTERGENERATORS ALERT SERVICE BULLETIN..

ASB 500-24-A007R2

OPEN

AIRFRAME1389

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT LEFT-HAND (LH) STARTERGENERATOR

ASB 500-24-A007R2 PART I

OPEN

AIRFRAME1390

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT RIGHT-HAND (RH) STARTERGENERATOR

ASB 500-24-A007R2 PII

OPEN

AIRFRAME1391

INSPECTION ELECTRICAL POWER - REPLACEMENT OF THESTARTER GENERATORS ALERT CLAMP PN MS21919WCH6INSTALLATION ON THE LH ENGINE FUEL SYSTEM

ASB 500-24-A007R2 PIII

COMPLIED WITH

AIRFRAME1392

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

NO. 2 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - INSPECTION OF ALERTSERVICE BULLETIN

ASB A66019 OPEN

ENGINE 21800

NO. 1 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - INSPECTION OF ALERTSERVICE BULLETIN

ASB A66019 OPEN

ENGINE 11726

NO. 1 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - INSPECTION OF ALERTSERVICE BULLETIN.

ASB A66019 R1 OPEN

ENGINE 11727

NO. 2 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - INSPECTION OF ALERTSERVICE BULLETIN.

ASB A66019 R1 OPEN

ENGINE 21801

NO. 2 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - MODIFICATION OF ALERTSERVICE BULLETIN

ASB A66021 N/A

ENGINE 21802

Notes: NOT APPLICABLE - SUPERSEDED BY REV. 1

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - MODIFICATION OF ALERTSERVICE BULLETIN

ASB A66021 N/A

ENGINE 11728

Notes: NOT APPLICABLE - SUPERSEDED BY REV. 1

NO. 2 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - MODIFICATION OF ALERTSERVICE BULLETIN.

ASB A66021 R1 COMPLIED WITH

ENGINE 21803

16-DEC-2009H: 44.10C: 49.00

Notes: COMPLIED WITH - SB ACCOMPLISHED WITH NO PROBLEMS TEST PERFORMED, NO DEFECT FOUND

NO. 1 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE - MODIFICATION OF ALERTSERVICE BULLETIN.

ASB A66021 R1 COMPLIED WITH

ENGINE 11729

16-DEC-2009H: 44.10C: 49.00

Notes: COMPLIED WITH - SB ACCOMPLISHED WITH NO PROBLEMS TEST PERFORMED, NO DEFECT FOUND

GENERAL - INSPECTION /INSTALLATION OF CABLE GUARDPINS ON CONTROL CABLES SERVICE BULLETIN

SB 500-00-0001 N/A

AIRFRAME1393

24-JUN-2011

Notes: NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT SN

PERFORM GENERAL - INSPECTION /INSTALLATION OFCABLE GUARD PINS ON CONTROL CABLES FLIGHT CONTROLSYSTEM - CABLE GUARD/COTTER PIN INSPECTION

SB 500-00-0001PART I

N/A

AIRFRAME1394

24-JUN-2011

Notes: NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT SN

PERFORM GENERAL - INSPECTION /INSTALLATION OFCABLE GUARD PINS ON CONTROL CABLES AUTOPILOT SERVOCABLES - COTTER PIN INSPECTION

SB 500-00-0001PART II

N/A

AIRFRAME1395

24-JUN-2011

Notes: NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT SN

PERFORM GENERAL - INSPECTION /INSTALLATION OFCABLE GUARD PINS ON CONTROL CABLES PARKING BRAKESYSTEM - CABLE GUARD PIN INSPECTION

SB 500-00-0001PART III

N/A

AIRFRAME1396

24-JUN-2011

Notes: NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT SN

GENERAL - RECONFIGURATION FROM EASA TO ANACCERTIFICATION REQUIREMENTS SERVICE BULLETIN

SB 500-00-0002 OPEN

AIRFRAME1397

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

GENERAL - RECONFIGURATION FROM ANAC TO FAACERTIFICATION REQUIREMENTS SERVICE BULLETIN

SB 500-00-0003 N/A

AIRFRAME1398

24-JUN-2011

Notes: NOT APPLICABLE - NOT APPLICABLE BY AIRCRAFT SN

GENERAL - RECONFIGURATION FROM ANAC TO FAACERTIFICATION REQUIREMENTS SERVICE BULLETIN.

SB 500-00-0003R1

OPEN

AIRFRAME1399

Notes: OPERATORS DISCRETION

GENERAL - RECONFIGURATION FROM FAA TO EASACERTIFICATION REQUIREMENTS SERVICE BULLETIN

SB 500-00-0004 OPEN

AIRFRAME1400

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) SERVICE BULLETIN

SB 500-00-0005 N/A

AIRFRAME1401Notes: NOT APPLICABLE

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) (REV. 5)

SB500-00-0005/05

OPEN

AIRFRAME1906

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) (REV. 6)

SB500-00-0005/06

OPEN

AIRFRAME1953

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) (REV. 8)

SB500-00-0005/08

OPEN

AIRFRAME2006

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) SERVICE BULLETIN.

SB 500-00-0005R1

N/A

AIRFRAME1402Notes: NOT APPLICABLE

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) SERVICE BULLETIN..

SB 500-00-0005R2

N/A

AIRFRAME1403Notes: NOT APPLICABLE

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) SERVICE BULLETIN...

SB 500-00-0005R3

N/A

AIRFRAME1404Notes: NOT APPLICABLE

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

GENERAL - INCREASE OF THE MZFW (MAXIMUM ZERO FUELWEIGHT) SERVICE BULLETIN....

SB 500-00-0005R4

N/A

AIRFRAME1405Notes: NOT APPLICABLE

GENERAL - RECONFIGURATION FROM EASA TO TCCACERTIFICATION REQUIREMENTS SERVICE BULLETIN

SB 500-00-0006 OPEN

AIRFRAME1406

GENERAL - CONVERSION FROM EASA TO FAACERTIFICATION BASIS REQUIREMENTS SERVICE BULLETIN

SB 500-00-0007 COMPLIED WITH

AIRFRAME1407

26-FEB-2013H: 684.70L: 651

Notes: COMPLIED WITH

GENERAL - CONVERSION FROM EASA TO FAACERTIFICATION BASIS REQUIREMENTS (REV. 1)

SB500-00-0007/01

OPEN

AIRFRAME1991

GENERAL - INSPECTION OF THE TURNBUCKLES SERVICEBULLETIN

SB 500-00-0008 COMPLIED WITH

AIRFRAME1408

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

GENERAL - INSTALLATION OF THE GROUND SPOILER /SPEED BRAKE FUNCTION AND NEW HYDRAULIC SYSTEM

SB500-00-0009/00

OPEN

AIRFRAME2014

GENERAL - RECONFIGURATION FROM FAA TO TCCACERTIFICATION REQUIREMENTS SERVICE BULLETIN

SB 500-00-0010 N/A

AIRFRAME1409

Notes: NOT APPLICABLE

GENERAL - CONVERSION FROM EASA TO FAACERTIFICATION BASIS REQUIREMENTS

SB 500-00-0011 OPEN

AIRFRAME1882

GENERAL - RECONFIGURATION FROM FAA TO TCCACERTIFICATION REQUIREMENTS

SB500-00-0012/00

OPEN

AIRFRAME1918

AIR CONDITIONING - REPLACEMENT OF THE FLOW CONTROLSHUTOFF VALVE (FCSOV) SERVICE BULLETIN

SB 500-21-0001 COMPLIED WITH

AIRFRAME1410

10-FEB-2010H: 500.00L: 500

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

AIR CONDITIONING - REPLACEMENT OF THE FLOW CONTROLSHUTOFF VALVE (FCSOV) SERVICE BULLETIN.

SB 500-21-0001R1

N/A BY SN

AIRFRAME1411

01-DEC-2010H: 557.00L: 500

AIR CONDITIONING - COMPRESSOR DRIVE MODULE (CDM)TRAY REPLACEMENT SERVICE BULLETIN

SB 500-21-0002 N/A

AIRFRAME1412Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

AIR CONDITIONING - REPLACEMENT OF THE ECSTEMPERATURE CONTROLLER FROM PN 1300650-9 TO PN1300650-10 SERVICE BULLETIN

SB 500-21-0003 COMPLIED WITH

AIRFRAME1413

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

AIR CONDITIONING - CPCS CONTROLLER (ECMU)HARDWARE CORRECTION SERVICE BULLETIN

SB 500-21-0004 OPEN

AIRFRAME1414

AIR CONDITIONING - CPCS CONTROLLER (ECMU)HARDWARE CORRECTION SERVICE BULLETIN.

SB 500-21-0004R1

COMPLIED WITH

AIRFRAME1415

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

AIR CONDITIONING - COMPRESSOR DRIVE MODULE (CDM)REWORK SERVICE BULLETIN

SB 500-21-0005 OPEN

AIRFRAME1416

COMPRESSOR DRIVE MODULE (CDM) REWORK SERVICEBULLETIN

SB 500-21-0005R1

OPEN

AIRFRAME1417

AIR CONDITIONING - COMPRESSOR DRIVE MODULE (CDM)REWORK SERVICE BULLETIN.

SB 500-21-0005R2

COMPLIED WITH

AIRFRAME1418

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

AIR CONDITIONING - REWORK OF FLOW CONTROL SHUT OFFVALVE (FCSOV) -15/25 SERVICE BULLETIN

SB 500-21-0006 OPEN

AIRFRAME1419

AIR CONDITIONING - REPLACEMENT OF THE ECSTEMPERATURE CONTROLLER SERVICE BULLETIN

SB 500-21-0007 OPEN

AIRFRAME1420

AIR CONDITIONING - REPLACEMENT OF THE ECSTEMPERATURE CONTROLLER SERVICE BULLETIN.

SB 500-21-0007R1

OPEN

AIRFRAME1421

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

AIR CONDITIONING - GROUND COOLING FAN REPLACEMENTSERVICE BULLETIN

SB 500-21-0008 OPEN

AIRFRAME1422

AIR CONDITIONING - REPLACEMENT OF THE ECSTEMPERATURE CONTROLLER SERVICE BULLETIN..

SB 500-21-0009 COMPLIED WITH

AIRFRAME1423

26-MAR-2012H: 587.40L: 584

Notes: COMPLIED WITH

AIR CONDITIONING - REPLACEMENT OF THE ECSTEMPERATURE CONTROLLER SERVICE BULLETIN...

SB 500-21-0009R1

OPEN

AIRFRAME1424

COMMUNICATIONS - VHF1 WIRING INSPECTION ANDMODIFICATION SERVICE BULLETIN

SB 500-23-0001 N/A

AIRFRAME1425Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

PERFORM COMMUNICATIONS - VHF1 WIRING INSPECTIONAND MODIFICATION WIRING INSPECTION

SB 500-23-0001PART I

OPEN

AIRFRAME1426

PERFORM COMMUNICATIONS - VHF1 WIRING INSPECTIONAND MODIFICATION WIRING MODIFICATION

SB 500-23-0001PART II

OPEN

AIRFRAME1427

COMMUNICATIONS - ACTIVATION OF THE DATALINKMANAGEMENT SYSTEM SERVICE BULLETIN

SB 500-23-0002 N/A

AIRFRAME1428

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

COMMUNICATIONS - INSTALLATION OF THE DATA LINKMANAGEMENT SYSTEM (DLMS) WITHOUT HANDSET SERVICEBULLETIN

SB 500-23-0003 OPEN

AIRFRAME1429

COMMUNICATIONS - REMOVAL OF THE HF AND SELCALSYSTEMS TO COMPLY WITH TCCA REQUIREMENTS SERVICEBULLETIN

SB 500-23-0004 N/A

AIRFRAME1430

Notes: NOT APPLICABLE

COMMUNICATIONS - COMPLEMENTATION AND ACTIVATION OFTHE CPDLC (CONTROLLER-TO-PILOT DATA LINKCOMMUNICATION)

SB500-23-0005/00

OPEN

AIRFRAME1963

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ELECTRICAL POWER - PROTECTION TO PREVENTINTERFERENCES WITH HARNESS W101 IN THE FORWARDREGION SERVICE BULLETIN

SB 500-24-0002 COMPLIED WITH

AIRFRAME1431

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

PERFORM ELECTRICAL POWER - PROTECTION TO PREVENTINTERFERENCES WITH HARNESS W101 IN THE FORWARDREGION INSTALLATION OF CLAMPS TO HARNESS W101 ANDOXYGEN TUBE (GROUP 1)

SB 500-24-0002PART I

COMPLIED WITH

AIRFRAME1432

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

PERFORM ELECTRICAL POWER - PROTECTION TO PREVENTINTERFERENCES WITH HARNESS W101 IN THE FORWARDREGION INSTALLATION OF CLAMPS TO HARNESS W101(GROUPS 1 E 2)

SB 500-24-0002PART II

COMPLIED WITH

AIRFRAME1433

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

ELECTRICAL POWER - PDU CONTACTORS INSPECTION ANDREPLACEMENT (THIS SB WAS SUPERSEDED BYSB500-24-0010) SERVICE BULLETIN

SB 500-24-0003 N/A

AIRFRAME1434

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NO

ELECTRICAL POWER - PROTECTION TO PREVENTINTERFERENCE BETWEEN HARNESS W201 AND THE OXYGENTUBE SERVICE BULLETIN

SB 500-24-0004 N/A

AIRFRAME1435

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

ELECTRICAL POWER - SPACER INSTALLATION FORHARNESSES W314 AND W601 SERVICE BULLETIN

SB 500-24-0005 COMPLIED WITH

AIRFRAME1436

26-MAR-2012H: 587.40L: 584

Notes: COMPLIED WITH

ELECTRICAL POWER - PYLON CONNECTOR - MISSINGSCREWS SERVICE BULLETIN

SB 500-24-0006 OPEN

AIRFRAME1437

ELECTRICAL POWER - PYLON CONNECTOR - MISSINGSCREWS SERVICE BULLETIN.

SB 500-24-0006R1

OPEN

AIRFRAME1438

ELECTRICAL POWER - PYLON CONNECTOR - MISSINGSCREWS SERVICE BULLETIN..

SB 500-24-0006R2

COMPLIED WITH

AIRFRAME1439

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ELECTRICAL POWER - REPLACEMENT OF THE STARTERGENERATORS

SB500-24-0007/00

COMPLIED WITH

AIRFRAME1975

14-SEP-2014H: 1038.80L: 833

ELECTRICAL POWER - REPLACEMENT OF THE STARTERGENERATORS (REV. 1)

SB500-24-0007/01

OPEN

AIRFRAME1986

14-SEP-2014H: 1038.80L: 833

ELECTRICAL POWER - REPLACEMENT OF THE LPDU, RPDUAND EPDU CONTACTORS (THIS SB WAS SUPERSEDED BYSB500-24-0010) SERVICE BULLETIN

SB 500-24-0008 COMPLIED WITH

AIRFRAME1440

Notes: SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

ELECTRICAL POWER ELECTRICAL POWER - REPLACEMENTOF THE LPDU, RPDU AND EPDU CONTACTORS (THIS SBWAS SUPERSEDED BY SB500-24-0010) REPLACEMENT OFTHE CONTACTORS PN SM400D117 IN THE LPDU

SB 500-24-0008PART I

COMPLIED WITH

AIRFRAME1441

26-MAR-2012H: 587.30L: 587

Notes: SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

ELECTRICAL POWER ELECTRICAL POWER - REPLACEMENTOF THE LPDU, RPDU AND EPDU CONTACTORS (THIS SBWAS SUPERSEDED BY SB500-24-0010) REPLACEMENT OFTHE CONTACTORS PN SM400D117 IN THE RPDU

SB 500-24-0008PART II

COMPLIED WITH

AIRFRAME1442

26-MAR-2012H: 587.30L: 587

Notes: SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

ELECTRICAL POWER ELECTRICAL POWER - REPLACEMENTOF THE LPDU, RPDU AND EPDU CONTACTORS (THIS SBWAS SUPERSEDED BY SB500-24-0010) REPLACEMENT OFTHE CONTACTORS PN SM400D117 IN THE EPDU

SB 500-24-0008PART III

COMPLIED WITH

AIRFRAME1443

26-MAR-2012H: 587.30L: 587

Notes: SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

ELECTRICAL POWER - MODIFICATION OF THE EMERGENCYBUS CONTACTOR (EBC) 1 GROUND WIRE SERVICEBULLETIN

SB 500-24-0009 OPEN

AIRFRAME1444

ELECTRICAL POWER - MODIFICATION OF THE EMERGENCYBUS CONTACTOR (EBC) 1 GROUND WIRE (REV. 1)

SB500-24-0009/01 OPEN

AIRFRAME1886

ELECTRICAL POWER - REPLACEMENT OF THE LPDU, RPDUAND EPDU SERVICE BULLETIN

SB 500-24-0010 N/A

AIRFRAME1445

26-MAR-2012H: 587.30L: 587

Notes: N/A IF SB500-24-0008 HAS BEEN ACCOMPLISHED. SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ELECTRICAL POWER - REPLACEMENT OF THE LPDU, RPDUAND EPDU (REV. 2)

SB500-24-0010/02

OPEN

AIRFRAME1985

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THELPDU, RPDU AND EPDU - OF THE LEFT POWERDISTRIBUTION UNIT (LPDU) PN SX7EG16-1 ORSX7EG16-1A.

SB 500-24-0010PART I

N/A

AIRFRAME1446

26-MAR-2012H: 587.30L: 587

Notes: N/A IF SB500-24-0008 HAS BEEN ACCOMPLISHED. SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THELPDU, RPDU AND EPDU - OF THE RIGHT POWERDISTRIBUTION UNIT (RPDU) PN SX7EG17-1 ORSX7EG17-1A.

SB 500-24-0010PART II

N/A

AIRFRAME1447

26-MAR-2012H: 587.30L: 587

Notes: N/A IF SB500-24-0008 HAS BEEN ACCOMPLISHED. SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

REPLACEMENT ELECTRICAL POWER - REPLACEMENT OF THELPDU, RPDU AND EPDU OF THE EMERGENCY POWERDISTRIBUTION UNIT (EPDU) PN SX7EG18-1 ORSX7EG18-1A.

SB 500-24-0010PART III

N/A

AIRFRAME1448

26-MAR-2012H: 587.30L: 587

Notes: N/A IF SB500-24-0008 HAS BEEN ACCOMPLISHED. SB500-24-0008 WAS ACCOMPLISHED 3/28/2012 @ 587.3 TTAF.

ELECTRICAL POWER - REPLACEMENT OF THE LPDU, RPDUAND EPDU

SB 500-24-0010R1

OPEN

AIRFRAME1880

ELECTRICAL POWER - RE-ROUTE OF THE W102 IN THEPASSENGER CABIN SERVICE BULLETIN

SB 500-24-0011 N/A

AIRFRAME1449Notes: NOT APPLICABLE

ELECTRICAL POWER - INSPECTION/REPAIR OF THEHARNESS W201 WITH MAIN PANEL STRUCTURE SERVICEBULLETIN

SB 500-24-0012 OPEN

AIRFRAME1450

ELECTRICAL POWER - MAIN BATTERY REPLACEMENTSB500-24-0014/00

OPEN

AIRFRAME2011

EQUIPMENT/FURNISHINGS - EMERGENCY-DOOR WATER-DRIPPREVENTION SERVICE BULLETIN

SB 500-25-0001 COMPLIED WITH

AIRFRAME1451

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

EQUIPMENT/FURNISHINGS - EMERGENCY-DOOR WATER-DRIPPREVENTION SERVICE BULLETIN.

SB 500-25-0001REV 01

OPEN

AIRFRAME1452

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THEPASSENGER SEATS SERVICE BULLETIN

SB 500-25-0003 COMPLIED WITH

AIRFRAME1453

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

EQUIPMENT/FURNISHINGS - INTERIOR CONFIGURATIONCONVERSION FROM CITRINE TO TOPAZ PATTERN SERVICEBULLETIN

SB 500-25-0004 N/A

AIRFRAME1454

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

EQUIPMENT/FURNISHINGS - COCKPIT SUNSHADE ANDSUNVISOR INSTALLATION SERVICE BULLETIN

SB 500-25-0005 OPEN

AIRFRAME1455

Notes: OPERATORS DISCRETION

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SERVICE BULLETIN

SB 500-25-0006 OPEN

AIRFRAME1456

Notes: OPERATORS DISCRETION

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR (REV. 5)

SB500-25-0006/05

OPEN

AIRFRAME1977

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR (REV. 6)

SB500-25-0006/06

OPEN

AIRFRAME1988

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND DECAL INSTALLATION FOR S/N 50000007

SB 500-25-0006PART I

OPEN

AIRFRAME1457

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR, DECAL ANDSUBWOOFER INSTALLATION FOR S/N 50000120

SB 500-25-0006PART II

OPEN

AIRFRAME1458

Notes: OPERATORS DISCRETION

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR AND DECALINSTALLATION FOR S/N 50000096

SB 500-25-0006PART III

OPEN

AIRFRAME1459

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR, DECAL ANDSUBWOOFER INSTALLATION FOR S/N 50000088

SB 500-25-0006PART IV

OPEN

AIRFRAME1460

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND DECAL INSTALLATION FOR S/N 50000007.

SB 500-25-0006R02 PART I

OPEN

AIRFRAME1462

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND DECAL INSTALLATION FOR S/N 50000169,50000188

SB 500-25-0006R02 PART V

OPEN

AIRFRAME1466

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND DECAL INSTALLATION FOR S/N 50000120

SB 500-25-0006R02 PII

OPEN

AIRFRAME1463

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND DECAL INSTALLATION FOR S/N 50000096

SB 500-25-0006R02 PIII

OPEN

AIRFRAME1464

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND DECAL INSTALLATION FOR S/N 50000088

SB 500-25-0006R02 PIV

OPEN

AIRFRAME1465

Notes: OPERATORS DISCRETION

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SIDELEDGE, DADOPANEL AND FLOOR PANEL REWORK, LAVATORY RIGID DOORAND PLACARD INSTALLATION S/N: 50000007

SB 500-25-0006R1 PART I

OPEN

AIRFRAME1468

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SIDELEDGE ANDDADO PANEL REWORK, LAVATORY RIGID DOOR, PLACARDAND SUBWOOFER BOX INSTALLATION S/N: 50000120

SB 500-25-0006R1 PART II

OPEN

AIRFRAME1469

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SIDELEDGE ANDDADO PANEL REWORK, LAVATORY RIGID DOOR, PLACARDAND SUBWOOFER BOX INSTALLATION S/N: 50000088

SB 500-25-0006R1 PART IV

OPEN

AIRFRAME1471

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SIDELEDGE ANDDADO PANEL , LAVATORY RIGID DOOR AND PLACARDINSTALLATION S/N: 50000188

SB 500-25-0006R1 PART V

OPEN

AIRFRAME1472

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SIDELEDGE ANDDADO PANEL REWORK, LAVATORY RIGID DOOR AND PLACARDINSTALLATION S/N: 50000096

SB 500-25-0006R1 PIII

OPEN

AIRFRAME1470

Notes: OPERATORS DISCRETION

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIGID DOORAND PLACARD INSTALLATION FOR S/N 50000007

SB 500-25-0006R3 PART I

OPEN

AIRFRAME1474

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR, PLACARD ANDSUBWOOFER BOX INSTALLATION FOR S/N 50000120

SB 500-25-0006R3 PART II

OPEN

AIRFRAME1475

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR, PLACARD ANDSUBWOOFER BOX INSTALLATION FOR S/N 50000088

SB 500-25-0006R3 PART IV

OPEN

AIRFRAME1477

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR AND PLACARDINSTALLATION FOR S/N 50000169 AND 50000188

SB 500-25-0006R3 PART V

OPEN

AIRFRAME1478

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR AND PLACARDINSTALLATION FOR S/N 50000096 AND 50000234

SB 500-25-0006R3 PIII

OPEN

AIRFRAME1476

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE,DADO PANEL AND FLOOR PANEL, LAVATORY RIDGE DOORAND PLACARD INSTALLATION FOR S/N 50000007

SB 500-25-0006R4 PART I

OPEN

AIRFRAME1480

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR, PLACARD ANDSUBWOOFER BOX INSTALLATION FOR S/N 500000120

SB 500-25-0006R4 PART II

OPEN

AIRFRAME1481

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIDGE DOOR, PLACARD ANDSUBWOOFER BOX INSTALLATION FOR S/N 50000088

SB 500-25-0006R4 PART IV

OPEN

AIRFRAME1483

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEGE ANDDADO PANEL, LAVATORY RIGID DOOR AND PLACARDINSTALLATION FOR S/N 50000169 AND 50000188

SB 500-25-0006R4 PART V

OPEN

AIRFRAME1484

REWORK EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR OF SIDELEDGE ANDDADO PANEL, LAVATORY RIGID DOOR AND PLACARDINSTALLATION FOR S/N 50000096 AND 50000234.

SB 500-25-0006R4 PIII

OPEN

AIRFRAME1482

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SERVICE BULLETIN.

SB 500-25-0006REV 02

OPEN

AIRFRAME1461

Notes: OPERATORS DISCRETION

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SERVICEBULLETIN..

SB 500-25-0006REV 1

OPEN

AIRFRAME1467

Notes: OPERATORS DISCRETION

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

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EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SERVICEBULLETIN...

SB 500-25-0006REV 3

OPEN

AIRFRAME1473

EQUIPMENT/FURNISHINGS - REPLACEMENT OF THELAVATORY DIVIDER WITH RIGID DOOR SERVICEBULLETIN....

SB 500-25-0006REV 4

OPEN

AIRFRAME1479

EQUIPMENT/FURNISHINGS - BELTED TOILET SERVICEBULLETIN

SB 500-25-0007 OPEN

AIRFRAME1485

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATION(REV. 6)

SB500-25-0007/06

OPEN

AIRFRAME1925

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATION(REV. 7)

SB500-25-0007/07

OPEN

AIRFRAME1998

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATION(REV. 8)

SB500-25-0007/08

OPEN

AIRFRAME2009

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILET AIRCRAFT EQUIPPED WITH LAVATORY RIGID DOOR (LRD)

SB 500-25-0007PART I

OPEN

AIRFRAME1486

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILET AIRCRAFT EQUIPPED WITH LAVATORY CURTAIN

SB 500-25-0007PART II

OPEN

AIRFRAME1487

EQUIPMENT/FURNISHINGS - BELTED TOILET SERVICEBULLETIN.

SB 500-25-0007R1

OPEN

AIRFRAME1488

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILET AIRCRAFT EQUIPPED WITH LAVATORY CURTAIN.

SB 500-25-0007R1 PART II

OPEN

AIRFRAME1490

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILET AIRCRAFT EQUIPPED WITHLAVATORY RIGID DOOR (LRD)

SB 500-25-0007R1 PI

OPEN

AIRFRAME1489

EQUIPMENT/FURNISHINGS - BELTED TOILET SERVICEBULLETIN..

SB 500-25-0007R2

OPEN

AIRFRAME1491

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILET AIRCRAFT EQUIPPED WITH LAVATORY CURTAIN..

SB 500-25-0007R2 PART II

OPEN

AIRFRAME1493

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILET AIRCRAFT EQUIPPED WITHLAVATORY RIGID DOOR (LRD).

SB 500-25-0007R2 PI

OPEN

AIRFRAME1492

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONSERVICE BULLETIN

SB 500-25-0007R3

OPEN

AIRFRAME1494

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILETINSTALLATION AIRCRAFT EQUIPPED WITH LAVATORYCURTAIN

SB 500-25-0007R3 PART II

OPEN

AIRFRAME1496

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILETINSTALLATION AIRCRAFT EQUIPPEDWITH LAVATORY RIGIDDOOR (LRD)

SB 500-25-0007R3 PI

OPEN

AIRFRAME1495

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILETINSTALLATION AIRCRAFT EQUIPPED WITH LAVATORYRIGID DOOR (LRD)

SB 500-25-0007R4 PART I

OPEN

AIRFRAME1498

Notes: OPERATORS DISCRETION

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILETINSTALLATION AIRCRAFT EQUIPPED WITH LAVATORYCURTAIN.

SB 500-25-0007R4 PART II

OPEN

AIRFRAME1499

Notes: OPERATORS DISCRETION

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONSB 500-25-0007R5

OPEN

AIRFRAME1883

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONSERVICE BULLETIN.

SB 500-25-0007REV 4

OPEN

AIRFRAME1497Notes: OPERATORS DISCRETION

EQUIPMENT/FURNISHINGS - SIDE FACING SEATINSTALLATION (FIFTH SEAT INSTALLATION)

SB500-25-0008/00

OPEN

AIRFRAME1960

EQUIPMENT/FURNISHINGS - SIDE FACING SEATINSTALLATION (FIFTH SEAT INSTALLATION) (REV.1)

SB500-25-0008/01

OPEN

AIRFRAME1961

EQUIPMENT/FURNISHINGS - SIDE FACING SEATINSTALLATION (FIFTH SEAT INSTALLATION) (REV.2)

SB500-25-0008/02

OPEN

AIRFRAME2010

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

EQUIPMENT/FURNISHINGS - PLACARD INSTALLATION TOTHE ELT REMOTE CONTROL PANEL SERVICE BULLETIN

SB 500-25-0009 OPEN600HR/12MOAIRFRAME1500

14-SEP-2014H: 1038.80L: 883

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONFOR PROVISIONED AIRCRAFT SERVICE BULLETIN

SB 500-25-0010 OPEN

AIRFRAME1501

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONFOR PROVISIONED AIRCRAFT (REV. 3)

SB500-25-0010/03

OPEN

AIRFRAME2001

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONFOR PROVISIONED AIRCRAFT SERVICE BULLETIN.

SB 500-25-0010R1

OPEN

AIRFRAME1502

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILETINSTALLATION FOR PROVISIONED AIRCRAFT AIRCRAFTEQUIPPED WITH LAVATORY CURTAIN

SB 500-25-0010R1 PART II

OPEN

AIRFRAME1504

ACCOMPLISH EQUIPMENT/FURNISHINGS - BELTED TOILETINSTALLATION FOR PROVISIONED AIRCRAFTSERVICEBULLETIN AIRCRAFT EQUIPPED WITH LAVATORYRIGID DOOR (LRD)

SB 500-25-0010R1 PI

OPEN

AIRFRAME1503

EQUIPMENT/FURNISHINGS - BELTED TOILET INSTALLATIONFOR PROVISIONED AIRCRAFT

SB 500-25-0010R2

OPEN

AIRFRAME1884

EQUIPMENT/FURNISHINGS - PREMIUM SEAT INSTALLATIONSB 500-25-0012 OPEN

AIRFRAME1971

EQUIPMENT/FURNISHINGS - PREMIUM SEAT INSTALLATION(REV. 1)

SB500-25-0012/01

OPEN

AIRFRAME1980

EQUIPMENT/FURNISHINGS - PREMIUM SEAT INSTALLATION(REV. 2)

SB500-25-0012/02 OPEN

AIRFRAME1993

EQUIPMENT/FURNISHINGS - SINGLE SIDE FACING SEAT(FIFTH SEAT) INSTALLATION FOR AIRCRAFT WITHSTRUCTURAL PROVISION

SB500-25-0014/00

OPEN

AIRFRAME1995

EQUIPMENT/FURNISHINGS - SINGLE SIDE FACING SEAT(FIFTH SEAT) INSTALLATION FOR AIRCRAFT WITHSTRUCTURAL PROVISION

SB500-25-0014/01

OPEN

AIRFRAME2003

EQUIPMENT/FURNISHINGS - EQUIPMENT/FURNISHINGS -SINGLE SIDE FACING SEAT (FIFTH SEAT)INSTALLATION FOR AIRCRAFT WITH STRUCTURALPROVISION (REV. 2)

SB500-25-0014/02

OPEN

AIRFRAME2004

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

FIRE PROTECTION - ENGINE FIRE DETECTOR REROUTINGSERVICE BULLETIN

SB 500-26-0001 OPEN

AIRFRAME1505

FIRE PROTECTION - ENGINE FIRE DETECTOR REROUTINGSERVICE BULLETIN.

SB 500-26-0001R1

OPEN

AIRFRAME1506

FIRE PROTECTION - ENGINE FIRE DETECTOR REROUTINGSERVICE BULLETIN..

SB 500-26-0001R2

OPEN

AIRFRAME1507

FIRE PROTECTION - ADDITIONAL FIRE EXTINGUISHER FOR7 PASSENGERS CONFIGURATION

SB500-26-0002/00

OPEN

AIRFRAME1958

FIRE PROTECTION - ADDITIONAL FIRE EXTINGUISHER FOR7 PASSENGERS CONFIGURATION (REV. 1)

SB500-26-0002/01

OPEN

AIRFRAME1989

FIRE PROTECTION - PORTABLE FIRE EXTINGUISHERREPLACEMENT

SB500-26-0003/00

OPEN

AIRFRAME1928

FIRE PROTECTION - PORTABLE FIRE EXTINGUISHER REPLACEMENT (REV. 1)

SB500-26-0003/01

OPEN

AIRFRAME1990

FIRE PROTECTION - PORTABLE FIRE EXTINGUISHERREPLACEMENT (REV. 2)

SB500-26-0003/02

OPEN

AIRFRAME1996

FLIGHT CONTROLS - REPLACEMENT OF THE SWPC AND FSCUWOW FUNCTION ACTIVATION SERVICE BULLETIN

SB 500-27-0001 N/A

AIRFRAME1508

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

PERFORM FLIGHT CONTROLS - REPLACEMENT OF THE SWPCAND FSCU WOW FUNCTION ACTIVATION REPLACEMENT OFTHE STALL WARNING AND PROTECTION COMPUTER (SWPC)

SB 500-27-0001PART I

N/A

AIRFRAME1509

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

PERFORM FLIGHT CONTROLS - REPLACEMENT OF THE SWPCAND FSCU WOW FUNCTION ACTIVATION FLAP SYSTEMCONTROL UNIT (FSCU) WEIGHT-ON-WHEELS (WOW)FUNCTION ACTIVATION

SB 500-27-0001PART II

N/A

AIRFRAME1510

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

FLIGHT CONTROLS - REPLACEMENT OF THE FLAP SYSTEMCONTROL UNIT (FSCU) SERVICE BULLETIN

SB 500-27-0002 N/A

AIRFRAME1511

Notes: NOT APPLICABLE - SUPERSEDED BY R1

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

FLIGHT CONTROLS - REPLACEMENT OF THE FLAP SYSTEMCONTROL UNIT (FSCU) SERVICE BULLETIN.

SB 500-27-0002R1

N/A

AIRFRAME1512

Notes: NOT APPLICABLE - SUPERSEDED BY R2

FLIGHT CONTROLS - REPLACEMENT OF THE FLAP SYSTEMCONTROL UNIT (FSCU) SERVICE BULLETIN..

SB 500-27-0002R2

COMPLIED WITH

AIRFRAME1513

12-AUG-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

FLIGHT CONTROLS - REMOVAL OF THE FLAP LIMITATIONSERVICE BULLETIN

SB 500-27-0003 COMPLIED WITH

AIRFRAME1514

25-JUN-2010H: 186.70L: 213

Notes: COMPLIED WITH - SB COMPLIED WITH

FLIGHT CONTROLS - REMOVAL OF THE FLAP LIMITATIONSERVICE BULLETIN.

SB 500-27-0003R1

COMPLIED WITH

AIRFRAME1515

PERFORM FLIGHT CONTROLS - REMOVAL OF THE FLAPLIMITATION REMOVAL OF THE FLAP POSITION FULLLIMITATION

SB 500-27-0003R1 PART II

COMPLIED WITH

AIRFRAME1517

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

PERFORM FLIGHT CONTROLS - REMOVAL OF THE FLAPLIMITATION REMOVAL OF THE FLAPPOSITION 3LIMITATION

SB 500-27-0003R1 PI

COMPLIED WITH

AIRFRAME1516

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

PERFORM FLIGHT CONTROLS - REMOVAL OF THE FLAPLIMITATION REPLACEMENT OF THE FLAP SYSTEM CONTROLUNIT (FSCU-05/07 TO FSCU-08)

SB 500-27-0003R1 PIII

COMPLIED WITH

AIRFRAME1518

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

FLIGHT CONTROLS - REPLACEMENT OF THE FLAP SYSTEMCONTROL UNIT (FSCU-3/4 TO FSCU-5) SERVICEBULLETIN

SB 500-27-0005 COMPLIED WITH

AIRFRAME1519

25-JUN-2010H: 186.70L: 213

Notes: COMPLIED WITH - SB COMPLIED WITH

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

FLIGHT CONTROLS - REPLACEMENT OF THE FLAP SYSTEMCONTROL UNIT (FSCU- 3/4 TO FSCU-5) (THISBULLETIN IS SUPERSEDED BY SB500-27-0003) SERVICEBULLETIN

SB 500-27-0005R1

N/A

AIRFRAME1520

Notes: NOT APPLICABLE

FLIGHT CONTROLS - CHANGE OF ANGLE OF ATTACK(AOA) SENSOR FROM PN C-100117-2 TO PN C-100117-3SERVICE BULLETIN

SB 500-27-0006 OPEN

AIRFRAME1521

FLIGHT CONTROLS - CHANGE OF ANGLE OF ATTACK(AOA) SENSOR FROM PN C-100117-2 TO PN C-100117-3(REV. 3)

SB500-27-0006/03

OPEN

AIRFRAME1947

FLIGHT CONTROLS - CHANGE OF ANGLE OF ATTACK(AOA) SENSOR FROM PN C-100117-2 TO PN C-100117-3SERVICE BULLETIN.

SB 500-27-0006R1

OPEN

AIRFRAME1522

FLIGHT CONTROLS - CHANGE OF ANGLE OF ATTACK(AOA) SENSOR FROM PN C-100117-2 TO PN C-100117-3SERVICE BULLETIN..

SB 500-27-0006R2

COMPLIED WITH

AIRFRAME1523

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH - SB COMPLIED WITH ON NAYAK WO 131197/J1.

ACCOMPLISH FLIGHT CONTROLS - CHANGE OF ANGLE OFATTACK (AOA) SENSOR FROM PN C-100117-2 TO PNC-100117-3 INSPECTION OF THE AOA SENSOR, ANDSEALANT APPLYING

SB 500-27-0006R2 PART II

COMPLIED WITH

AIRFRAME1525

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

ACCOMPLISH FLIGHT CONTROLS - CHANGE OF ANGLE OFATTACK (AOA) SENSOR FROM PN C-100117-2 TOPNC-100117-3 CHANGE OF ANGLE OF ATTACK (AOA)SENSOR FROM PN C-100117-2 TO PN C-100117-3

SB 500-27-0006R2 PI

COMPLIED WITH

AIRFRAME1524

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

FLIGHT CONTROLS - PILOT CONTROL-YOKE ASSEMBLYINSTALLATION SERVICE BULLETIN

SB 500-27-0007 N/A

AIRFRAME1526

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - SUPERSEDED

FLIGHT CONTROLS - PILOT CONTROL-YOKE ASSEMBLYINSTALLATION SERVICE BULLETIN.

SB 500-27-0007R1

COMPLIED WITH

AIRFRAME1527

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

PERFORM FLIGHT CONTROLS - PILOT CONTROL-YOKEASSEMBLY INSTALLATION CORRECTIVE ACTION ON PILOTCONTROL YOKE GUST-LOCK FITTING HOLE

SB 500-27-0007R1 PART II

COMPLIED WITH

AIRFRAME1529

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

PERFORM FLIGHT CONTROLS - PILOT CONTROL-YOKEASSEMBLY INSTALLATION CORRECTIVE ACTION ON PILOTCONTROL YOKE INSTALLATION

SB 500-27-0007R1 PART IV

COMPLIED WITH

AIRFRAME1531

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

PERFORM FLIGHT CONTROLS - PILOT CONTROL-YOKEASSEMBLY INSTALLATION INSPECTIONOF HOLE OF PILOTCONTROL YOKE GUST-LOCK FITTING

SB 500-27-0007R1 PI

COMPLIED WITH

AIRFRAME1528

H: 260.50L: 312

Notes: COMPLIED WITH

PERFORM FLIGHT CONTROLS - PILOT CONTROL-YOKEASSEMBLY INSTALLATION PILOT CONTROL YOKE ASSEMBLYINSPECTION

SB 500-27-0007R1 PIII

COMPLIED WITH

AIRFRAME1530

H: 260.50L: 312

Notes: COMPLIED WITH

FLIGHT CONTROLS - GROUND SPOILER SYSTEMINSTALLATION SERVICE BULLETIN

SB 500-27-0008 OPEN

AIRFRAME1532

FLIGHT CONTROLS - CONTROL YOKE REPLACEMENT SERVICEBULLETIN

SB 500-27-0009 COMPLIED WITH

AIRFRAME1533

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

FLIGHT CONTROLS - CONTROL YOKE MAP HOLDERREPLACEMENT SERVICE BULLETIN

SB 500-27-0010 OPEN

AIRFRAME1534

FLIGHT CONTROLS - CONTROL YOKE MAP HOLDERREPLACEMENT SERVICE BULLETIN.

SB 500-27-0010R1

OPEN

AIRFRAME1535

FLIGHT CONTROLS - REPLACEMENT OF TRIM ACTUATORCONTROLLER SERVICE BULLETIN

SB 500-27-0011 OPEN

AIRFRAME1536

FLIGHT CONTROLS - REPLACEMENT OF TRIM ACTUATORCONTROLLER SERVICE BULLETIN.

SB 500-27-0011R1

COMPLIED WITH

AIRFRAME1537

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

FLIGHT CONTROLS - MODIFICATION OF THE PEDALPOSITION TRANSDUCER STOPS SERVICE BULLETIN

SB 500-27-0013 COMPLIED WITH

AIRFRAME1538

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

FLIGHT CONTROLS - MODIFICATION OF THE PEDALPOSITION TRANSDUCER STOPS SERVICE BULLETIN.

SB 500-27-0013REV 1

OPEN

AIRFRAME1539

Notes: OPERATORS DISCRETION

REPLACEMENT OF THE BOLT THAT ATTACHES THE LINK ARMTO THE FLAP POSITION SENSOR SERVICE BULLETIN

SB 500-27-0015 COMPLIED WITH

AIRFRAME1540

26-MAR-2012H: 587.40L: 584

Notes: COMPLIED WITH

REPLACEMENT FLIGHT CONTROLS - REPLACEMENT OF THEBOLT THAT ATTACHES THE LINK ARM TO THE FLAPPOSITION SENSOR OF BOLT THAT ATTACHES THE LINKARM FROM PN NAS6303-11 TO PN NAS1801-3-16

SB 500-27-0015R1 PART I

COMPLIED WITH

AIRFRAME1542

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

REPLACEMENT FLIGHT CONTROLS - REPLACEMENT OF THEBOLT THAT ATTACHES THE LINK ARM TO THE FLAPPOSITION SENSOR OF BOLT THAT ATTACHES THE LINKARM FROM PN NAS1801-3-15 TO PN NAS1801-3-16

SB 500-27-0015R1 PART II

COMPLIED WITH

AIRFRAME1543

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

FLIGHT CONTROLS - REPLACEMENT OF THE BOLT THATATTACHES THE LINK ARM TO THE FLAP POSITION SENSORSERVICE BULLETIN

SB 500-27-0015REV 1

COMPLIED WITH

AIRFRAME1541

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

FLIGHT CONTROLS - ELECTRICAL WIRING MODIFICATIONIN THE COPILOT CONTROL WHEEL CONNECTOR 2J0505

SB 500-27-0016 OPEN

AIRFRAME1881

FLIGHT CONTROLS - ELECTRICAL WIRING MODIFICATIONIN THE COPILOT CONTROL WHEEL CONNECTOR 2J0505 (REV. 1)

SB 500-27-0016/1 OPEN

AIRFRAME2023

FLIGHT CONTROLS - CONTROL PEDAL ASSEMBLYMODIFICATION SERVICE BULLETIN

SB 500-27-0017 OPEN

AIRFRAME1544

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

FLIGHT CONTROLS - PILOT CONTROL PEDAL ASSEMBLYREWORK SERVICE BULLETIN

SB 500-27-0017R1

OPEN

AIRFRAME1545

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK OF LIMITER BOLT ASSEMBLY

SB 500-27-0017R1 PART II

OPEN

AIRFRAME1547

FLIGHT CONTROLS - PILOT CONTROL PEDAL ASSEMBLYREWORK OF BOLT PINASSEMBLY

SB 500-27-0017R1 PI INST

OPEN

AIRFRAME1546

FLIGHT CONTROLS - PILOT CONTROL PEDAL ASSEMBLYREWORK SERVICE BULLETIN.

SB 500-27-0017R2

COMPLIED WITH

AIRFRAME1548

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK OF LIMITER BOLT ASSEMBLY.

SB 500-27-0017R2 PART II

COMPLIED WITH

AIRFRAME1550

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK OF ADJUSTABLE STOP SCREWASSEMBLY AND ROLLERS STANDARDIZATION

SB 500-27-0017R2 PART IV

COMPLIED WITH

AIRFRAME1552

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK OF ADJUSTABLE STOP SCREWASSEMBLY

SB 500-27-0017R2 PIII

COMPLIED WITH

AIRFRAME1551

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

FLIGHT CONTROLS - PILOT CONTROL PEDAL ASSEMBLYREWORK OF BOLT PINASSEMBLY.

SB 500-27-0017R2 PI INST

COMPLIED WITH

AIRFRAME1549

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

FLIGHT CONTROLS - PILOT CONTROL PEDAL ASSEMBLYREWORK SERVICE BULLETIN..

SB 500-27-0017R3

OPEN

AIRFRAME1553

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK - OF LIMITER BOLT ASSEMBLY

SB 500-27-0017R3 PART II

N/A

AIRFRAME1555

Notes: NOT APPLICABLE

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK - OF ADJUSTABLE STOP SCREWASSEMBLY AND ROLLERS STANDARDIZATION

SB 500-27-0017R3 PART IV

OPEN

AIRFRAME1557

INSTALLATION FLIGHT CONTROLS - PILOT CONTROLPEDAL ASSEMBLY REWORK - OF ADJUSTABLE STOP SCREWASSEMBLY

SB 500-27-0017R3 PIII

OPEN

AIRFRAME1556

FLIGHT CONTROLS - PILOT CONTROL PEDAL ASSEMBLYREWORK - OF BOLT PINASSEMBLY

SB 500-27-0017R3 PI INST

OPEN

AIRFRAME1554

FLIGHT CONTROLS - CHECK OF LOCK WIRE FOR PROPERROUTING

SB500-27-0019/00

OPEN

AIRFRAME1911

FLIGHT CONTROLS - CHECK OF LOCK WIRE FOR PROPERROUTING (REV. 1)

SB500-27-0019/01

OPEN

AIRFRAME1917

FLIGHT CONTROLS - CHECK OF LOCK WIRE FOR PROPERROUTING (REV. 2)

SB500-27-0019/02

OPEN

AIRFRAME1983

FLIGHT CONTROLS - REPLACEMENT OF THE FLAP SYSTEMCONTROL UNIT (FSCU) SERVICE BULLETIN...

SB 500-27-0020 OPEN

AIRFRAME1558

FLIGHT CONTROLS - REPLACEMENT OF FLAP LINEARACTUATORS SERVICE BULLETIN

SB 500-27-0021 OPEN

AIRFRAME1559

FLIGHT CONTROLS - REPLACEMENT OF FLAP LINEARACTUATORS SERVICE BULLETIN.

SB 500-27-0021R1

OPEN

AIRFRAME1560

FLIGHT CONTROLS - ANGLE OF ATTACK (AOA) SENSORREPLACEMENT

SB500-27-0022/00

COMPLIED WITH

AIRFRAME1944

14-SEP-2014H: 1038.80L: 833

FUEL - REPLACEMENT OF THE ENGINE-FEED EJECTOR PUMPSB500-28-0001/00

OPEN

AIRFRAME1912

HYDRAULIC POWER - TORQUE VERIFICATION IN THEHYDRAULIC FITTINGS SERVICE BULLETIN

SB 500-29-0001 N/A

AIRFRAME1561

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NUMBER

HYDRAULIC POWER - HYDRAULIC POWER PACK REPLACEMENTSERVICE BULLETIN

SB 500-29-0002 OPEN

AIRFRAME1562

Page 153 of 193

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

HYDRAULIC POWER - HYDRAULIC POWER PACK REPLACEMENTSERVICE BULLETIN.

SB 500-29-0002REV 1

OPEN

AIRFRAME1563

HYDRAULIC POWER - REDUCTION OF RESERVOIR FULLFLUID LEVEL INDICATION OF POWER-PACK

SB500-29-0004/00 COMPLIED WITH

AIRFRAME1994

14-SEP-2014H: 1038.80L: 833

HYDRAULIC POWER - REDUCTION OF RESERVOIR FULLFLUID LEVEL INDICATION OF POWER-PACK (REV. 1)

SB500-29-0004/01

OPEN

AIRFRAME2012

ICE AND RAIN PROTECTION - REPLACEMENT OF THE WHCUSERVICE BULLETIN

SB 500-30-0001 N/A

AIRFRAME1564Notes: NOT APPLICABLE - SUPERSEDED BY REV 1

ICE AND RAIN PROTECTION - REPLACEMENT OF THE WHCUSERVICE BULLETIN.

SB 500-30-0001R1

N/A

AIRFRAME1565

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - IMPLEMENTED 18 DEC 09

ICE AND RAIN PROTECTION - TORQUE ON WINDSHIELDHEATING GROUND STUD SERVICE BULLETIN

SB 500-30-0002 COMPLIED WITH

AIRFRAME1566

25-JUN-2010H: 186.70L: 213

Notes: COMPLIED WITH - SB COMPLIED WITH

ICE AND RAIN PROTECTION - DE-ICE LINE MODIFICATIONSERVICE BULLETIN

SB 500-30-0004 OPEN

AIRFRAME1567

ICE AND RAIN PROTECTION - DE-ICE LINE MODIFICATIONSERVICE BULLETIN.

SB 500-30-0004R1

OPEN

AIRFRAME1568

ICE AND RAIN PROTECTION - DE-ICE LINE MODIFICATIONSERVICE BULLETIN..

SB 500-30-0004R2

OPEN

AIRFRAME1569

ICE AND RAIN PROTECTION - DE-ICE LINE MODIFICATIONSERVICE BULLETIN...

SB 500-30-0004R3

COMPLIED WITH

AIRFRAME1570

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

ICE AND RAIN PROTECTION - WATER SEPARATORINSTALLATION SERVICE BULLETIN

SB 500-30-0005 OPEN

AIRFRAME1571

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ICE AND RAIN PROTECTION - WATER SEPARATORINSTALLATION (REV.3)

SB500-30-0005/03

OPEN

AIRFRAME1926

ICE AND RAIN PROTECTION - WATER SEPARATORINSTALLATION SERVICE BULLETIN.

SB 500-30-0005R1

OPEN

AIRFRAME1572

ADDITIONAL ACTION ICE AND RAIN PROTECTION - WATERSEPARATOR INSTALLATION - REPLACEMENT OF THEDOWNSTREAM HOSE

SB 500-30-0005R1 PART II

N/A

AIRFRAME1574

Notes: NOT APPLICABLE

INSTALLATION ICE AND RAIN PROTECTION - WATERSEPARATOR INSTALLATION - OF WATERSEPARATORASSEMBLY

SB 500-30-0005R1 PI

OPEN

AIRFRAME1573

ICE AND RAIN PROTECTION - WATER SEPARATORINSTALLATION SERVICE BULLETIN..

SB 500-30-0005R2

OPEN

AIRFRAME1575

ADDITIONAL ACTION ICE AND RAIN PROTECTION - WATERSEPARATOR INSTALLATION - REPLACEMENT OF THEDOWNSTREAM HOSE

SB 500-30-0005R2 PART II

N/A

AIRFRAME1577

Notes: NOT APPLICABLE

INSTALLATION ICE AND RAIN PROTECTION - WATERSEPARATOR INSTALLATION OF WATERSEPARATOR ASSEMBLY

SB 500-30-0005R2 PI

OPEN

AIRFRAME1576

INSTALLATION ICE AND RAIN PROTECTION - WATERSEPARATOR INSTALLATION OF TUBES AND HOSES

SB 500-30-0005R2 PIII

N/A

AIRFRAME1578

Notes: NOT APPLICABLE

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 25.30 AVIONICS SOFTWARE AND CMC LOAD 6SOFTWARE SERVICE BULLETIN

SB 500-31-0001 COMPLIED WITH

AIRFRAME1579

18-DEC-2009H: 44.10L: 49

Notes: COMPLIED WITH

INDICATING/RECORDING SYSTEMS - ACTIVATION OF THECVDR SYSTEM SERVICE BULLETIN

SB 500-31-0002 COMPLIED WITH

AIRFRAME1580

18-DEC-2009H: 44.10L: 49

Notes: COMPLIED WITH

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 36 AVIONICS SOFTWARE AND CMC LOAD 7SOFTWARE SERVICE BULLETIN

SB 500-31-0003 N/A

AIRFRAME1581

Notes: NOT APPLICABLE - SUPERCEDED BY SB 500-21-0003/01

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 36 AVIONICS SOFTWARE AND CMC LOAD 7SOFTWARE SERVICE BULLETIN.

SB 500-31-0003R1

COMPLIED WITH

AIRFRAME1582

25-JUN-2010H: 186.70L: 213

Notes: COMPLIED WITH - SB COMPLIED WITH

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICE BULLETIN

SB 500-31-0004 N/A

AIRFRAME1583

Notes: NOT APPLICABLE - SUPERSEDED

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) (REV. 9)

SB500-31-00040/09

OPEN

AIRFRAME1931

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) (REV. 8)

SB500-31-0004/08

OPEN

AIRFRAME1913

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) (REV. 10)

SB500-31-0004/10

OPEN

AIRFRAME1942

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) (REV. 11)

SB500-31-0004/11

OPEN

AIRFRAME1952

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) (REV. 12)

SB500-31-0004/12

OPEN

AIRFRAME1976

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICE BULLETIN.

SB 500-31-0004R1

N/A

AIRFRAME1584

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - NA BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICE BULLETIN..

SB 500-31-0004R2

N/A

AIRFRAME1585

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

Page 156 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICE BULLETIN...

SB 500-31-0004R3

N/A

AIRFRAME1586

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICE BULLETIN....

SB 500-31-0004R4

OPEN

AIRFRAME1587

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICE BULLETIN.....

SB 500-31-0004R5

OPEN

AIRFRAME1588

INDICATING/RECORDING SYSTEMS - INSTALLATION OFELECTRONIC CHECKLIST (ECL) SERVICEBULLETIN......

SB 500-31-0004R6

OPEN

AIRFRAME1589

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN

SB 500-31-0005 N/A

AIRFRAME1590

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION (REV. 15)

SB500-31-0005/15 OPEN

AIRFRAME1887

INDICATING/RECORDING SYSTEMS- INSTALLATION OF THESYNTHETIC VISION (REV. 16)

SB500-31-0005/16

OPEN

AIRFRAME1916

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION (REV. 17)

SB500-31-0005/17

OPEN

AIRFRAME1927

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION (REV. 18)

SB500-31-0005/18

OPEN

AIRFRAME1959

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION (REV. 19)

SB500-31-0005/19

OPEN

AIRFRAME1979

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION (REV. 20)

SB500-31-0005/20

OPEN

AIRFRAME1987

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION (REV. 21)

SB500-31-0005/21

OPEN

AIRFRAME2007

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN.

SB 500-31-0005R1

N/A

AIRFRAME1591

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN..

SB 500-31-0005R10

OPEN

AIRFRAME1592

INSTALLATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION

SB 500-31-0005R10 PART I

OPEN

AIRFRAME1593

ACTIVATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION

SB 500-31-0005R10 PII

OPEN

AIRFRAME1594

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN...

SB 500-31-0005R11

OPEN

AIRFRAME1595

Notes: OPERATORS DISCRETION

INSTALLATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION.

SB 500-31-0005R11 PART I

OPEN

AIRFRAME1596

ACTIVATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION.

SB 500-31-0005R11 PII

OPEN

AIRFRAME1597

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN....

SB 500-31-0005R12

OPEN

AIRFRAME1598

INSTALLATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION..

SB 500-31-0005R12 PARTI

OPEN

AIRFRAME1599

ACTIVATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION..

SB 500-31-0005R12 PARTII

OPEN

AIRFRAME1600

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN.....

SB 500-31-0005R13

OPEN

AIRFRAME1601

Page 158 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INSTALLATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION...

SB 500-31-0005R13 PART I

OPEN

AIRFRAME1602

ACTIVATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION...

SB 500-31-0005R13 PII

OPEN

AIRFRAME1603

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN......

SB 500-31-0005R14

N/A

AIRFRAME1604

Notes: NOT APPLICABLE

INSTALLATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION....

SB 500-31-0005R14 PART I

N/A

AIRFRAME1605

Notes: NOT APPLICABLE

ACTIVATION INDICATING/RECORDING SYSTEMS -INSTALLATION OF THE SYNTHETIC VISION OF THESYNTHETIC VISION....

SB 500-31-0005R14 PII

N/A

AIRFRAME1606

Notes: NOT APPLICABLE

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN.......

SB 500-31-0005R2

N/A

AIRFRAME1607

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN........

SB 500-31-0005R3

N/A

AIRFRAME1608

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN.........

SB 500-31-0005R4

N/A

AIRFRAME1609

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN..........

SB 500-31-0005R5

OPEN

AIRFRAME1610

Page 159 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN...........

SB 500-31-0005R6

OPEN

AIRFRAME1611

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN............

SB 500-31-0005R7

OPEN

AIRFRAME1612

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN.............

SB 500-31-0005R8

OPEN

AIRFRAME1613

INDICATING/RECORDING SYSTEMS - INSTALLATION OF THESYNTHETIC VISION SERVICE BULLETIN..............

SB 500-31-0005R9

OPEN

AIRFRAME1614

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 43 AVIONICS OFTWARE AND CMC LOAD 8SOFTWARE SERVICE BULLETIN

SB 500-31-0006 COMPLIED WITH

AIRFRAME1615

19-APR-2011H: 374.00L: 408

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 43 AVIONICS SOFTWARE AND CMC LOAD 8SOFTWARE SERVICE BULLETIN

SB 500-31-0006R1

OPEN

AIRFRAME1616

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 43.5 AVIONICS SOFTWARE AND CMC LOAD 9SOFTWARE SERVICE BULLETIN

SB 500-31-0007 OPEN

AIRFRAME1617

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 43.5 AVIONICS SOFTWARE AND CMC LOAD 9SOFTWARE SERVICE BULLETIN.

SB 500-31-0007R1

COMPLIED WITH

AIRFRAME1618

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

INDCIATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 54 AVIONICS SOFTWARE AND CMC SOFTWARELOAD 10 SERVICE BULLETIN

SB 500-31-0008 OPEN

AIRFRAME1619

IINDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 63.7 AVIONICS SOFTWARE AND CMC LOAD 11

SB 500-31-0009 COMPLIED WITH

AIRFRAME1950

14-SEP-2014H: 1038.80L: 833

IINDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 63.7 AVIONICS SOFTWARE AND CMC LOAD 11(REV. 1)

SB500-31-0009/01

OPEN

AIRFRAME1951

14-SEP-2014H: 1038.80L: 833

Page 160 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 63.7 AVIONICS SOFTWARE AND CMC LOAD 11(REV. 2)

SB500-31-0009/02

OPEN

AIRFRAME1972

14-SEP-2014H: 1038.80L: 833

INDICATING/RECORDING SYSTEMS - G1000 AVIONICS -DOWNGRADE FROM LOAD 63.7 AVIONICS SOFTWARE AND CMCLOAD 11 SOFTWARE TO LOAD 55 AVIONICS SOFTWARE ANDCMC LOAD 10.1 SOFTWARE

SB500-31-0010/00

OPEN

AIRFRAME1968

INDICATING/RECORDING SYSTEMS - G1000 AVIONICS -DOWNGRADE FROM LOAD 63.7 AVIONICS SOFTWARE AND CMCLOAD 11 SOFTWARE TO LOAD 55 AVIONICS SOFTWARE ANDCMC LOAD 10.1 SOFTWARE (REV. 1)

SB500-31-0010/01

OPEN

AIRFRAME1970

INDICATING/RECORDING SYSTEMS - G1000 AVIONICS -DOWNGRADE FROM LOAD 63.7 AVIONICS SOFTWARE AND CMCLOAD 11 SOFTWARE TO LOAD 55 AVIONICS SOFTWARE ANDCMC LOAD 10.1 SOFTWARE (REV. 2)

SB500-31-0010/02

OPEN

AIRFRAME1974

INDICATING/RECORDING SYSTEMS - G1000 AVIONICS -DOWNGRADE FROM LOAD 63.7 AVIONICS SOFTWARE AND CMCLOAD 11 SOFTWARE TO LOAD 55 AVIONICS SOFTWARE ANDCMC LOAD 10.1 SOFTWARE (REV. 3)

SB500-31-0010/03

OPEN

AIRFRAME2008

INDICATING/RECORDING SYSTEMS - INSTALLATION OFG1000 LOAD 72.1 AVIONICS SOFTWARE AND CMC LOAD12.4

SB500-31-0011/00

OPEN

AIRFRAME2015

INDICATING/RECORDING SYSTEMS - TAWS-A (TERRAINAWARENESS AND WARNING SYSTEM) ELECTRICAL WIRINGINSTALLATION.

SB500-31-0012/00

OPEN

AIRFRAME2013

LANDING GEAR - REPLACEMENT OF BRAKE CONTROL UNIT( BCU-1/2 TO BCU-3) SERVICE BULLETIN

SB 500-32-0001 N/A

AIRFRAME1620

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - SUPERSEDED

LANDING GEAR - REPLACEMENT OF BRAKE CONTROL UNIT( BCU-1/2 TO BCU-3) SERVICE BULLETIN.

SB 500-32-0001R1

COMPLIED WITH

AIRFRAME1621

25-JUN-2010H: 186.70L: 213

Notes: COMPLIED WITH - SB COMPLIED WITH EEJC W474

LANDING GEAR - REPLACEMENT OF BRAKE CONTROL UNIT( BCU-1/2 TO BCU-3) SERVICE BULLETIN..

SB 500-32-0001R2

OPEN

AIRFRAME1622

Page 161 of 193

PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A

COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LANDING GEAR - CONVERSION OF BRAKE ASSEMBLY90005025 TO 90005025-2 SERVICE BULLETIN

SB 500-32-0002 N/A

AIRFRAME1623

Notes: NOT APPLICABLE - SUPERSEDED

LANDING GEAR - CONVERSION OF BRAKE ASSEMBLY90005025 TO 90005025-2 SERVICE BULLETIN.

SB 500-32-0002R1

OPEN

AIRFRAME1624

LANDING GEAR - CONVERSION OF BRAKE ASSEMBLY90005025 TO 90005025-2 SERVICE BULLETIN..

SB 500-32-0002R2

COMPLIED WITH

AIRFRAME1625

14-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

LANDING GEAR - MLG LOCKING ACTUATOR REWORK SERVICEBULLETIN

SB 500-32-0003 OPEN

AIRFRAME1626

LANDING GEAR - BRAKE CONTROL VALVE REPLACEMENTSERVICE BULLETIN

SB 500-32-0004 OPEN

AIRFRAME1627

LANDING GEAR - BRAKE CONTROL VALVE REPLACEMENTSERVICE BULLETIN.

SB 500-32-0004R1

COMPLIED WITH

AIRFRAME1628

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

LANDING GEAR - REPLACEMENT OF EPBV (EMERGENCY/PARKING BRAKE VALVE) SERVICE BULLETIN

SB 500-32-0005 COMPLIED WITH

AIRFRAME1629

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

LANDING GEAR - MLG SHOCK ABSORBER UPDATE SERVICEBULLETIN

SB 500-32-0006 OPEN

AIRFRAME1630

LANDING GEAR - MLG SHOCK ABSORBER UPDATE (REV.3)

SB500-32-0006/03

OPEN

AIRFRAME1889

LANDING GEAR - MLG SHOCK ABSORBER UPDATE SERVICEBULLETIN.

SB 500-32-0006R1

OPEN

AIRFRAME1631

LANDING GEAR - MLG SHOCK ABSORBER UPDATE SERVICEBULLETIN..

SB 500-32-0006R2

OPEN

AIRFRAME1632

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LANDING GEAR - LANDING GEAR MANIFOLD REPLACEMENTSERVICE BULLETIN

SB 500-32-0007IN

N/A

AIRFRAME1633Notes: NOT APPLICABLE - SUPERCEDED BY REV 1

LANDING GEAR - LANDING GEAR MANIFOLD REPLACEMENTSERVICE BULLETIN.

SB 500-32-0007R1

COMPLIED WITH

AIRFRAME1634

20-JUN-2011H: 464.30L: 481

Notes: COMPLIED WITH

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT SERVICE BULLETIN

SB 500-32-0008 OPEN

AIRFRAME1635

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT (REV.4)

SB500-32-0008/04

OPEN

AIRFRAME1936

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT SERVICE BULLETIN.

SB 500-32-0008R1

OPEN

AIRFRAME1636

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT SERVICE BULLETIN..

SB 500-32-0008R2

COMPLIED WITH

AIRFRAME1637

20-SEP-2012H: 662.00L: 637

Notes: COMPLIED WITH

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT SERVICE BULLETIN...

SB 500-32-0008R3

OPEN

AIRFRAME1638

LANDING GEAR - NLG SHOCK STRUT BEARING REPLACEMENTSERVICE BULLETIN

SB 500-32-0010 OPEN

AIRFRAME1639

LANDING GEAR - NLG SHOCK STRUT BEARING REPLACEMENTSERVICE BULLETIN.

SB 500-32-0010R1

OPEN

AIRFRAME1640

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT

SB500-32-0011/00

OPEN

AIRFRAME1935

14-SEP-2014H: 1038.80L: 833

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT (REV. 1)

SB500-32-0011/01

OPEN

AIRFRAME1957

14-SEP-2014H: 1038.80L: 833

LANDING GEAR - BRAKE CONTROL UNIT (BCU)REPLACEMENT (REV. 2)

SB500-32-0011/02

OPEN

AIRFRAME1982

14-SEP-2014H: 1038.80L: 833

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

LANDING GEAR - REWORK OF THE MLG SHOCK STRUTSB500-32-0012/00

OPEN

AIRFRAME1890

LANDING GEAR - REWORK OF THE MLG SHOCK STRUT(REV. 1)

SB500-32-0012/01

OPEN

AIRFRAME1969

LANDING GEAR - CORRECTION OF THE WHEEL AXLE TORQUEOF MLG AND NLG

SB 500-32-0013 COMPLIED WITH

AIRFRAME1949

14-SEP-2014H: 1038.80L: 833

LIGHTS - REPLACEMENT OF THE LIGHTS CONTROL PANELSERVICE BULLETIN

SB 500-33-0001 OPEN

AIRFRAME1641

LIGHTS - REPLACEMENT OF THE LIGHTS CONTROL PANELSERVICE BULLETIN.

SB 500-33-0001REV 1

RECURRING

AIRFRAME1642

M: 48 29-OCT-2016 M: 20 D: 26

LIGHTS - ELECTRICAL CONNECTOR P0030 AND P0031KEY-WAY RE-ORIENTATION FOR NAV/STROBE LIGHTS PNS84056-8 AND 84056-7 SERVICE BULLETIN

SB 500-33-0002 OPEN

AIRFRAME1643

LIGHTS - ASSISTANCE TO REPLACE NAV/STROBE LIGHTSPN 84056-3/ 84056-4 WITH PN 84056-7/84056-8SERVICE BULLETIN

SB 500-33-0002R1

N/A

AIRFRAME1644

Notes: NOT APPLICABLE

NAVIGATION - INSPECTION/CORRECTION OF THEINSTALLATION POSITION OF THE DUAL STATIC PORTSSERVICE BULLETIN

SB 500-34-0001 COMPLIED WITH

AIRFRAME1645

13-SEP-2011H: 504.20

Notes: COMPLIED WITH

PERFORM NAVIGATION - INSPECTION/CORRECTION OF THEINSTALLATION POSITION OF THE DUAL STATIC PORTS INSPECTION OF THE DUAL STATIC PORTS PNINSTALLATION

SB 500-34-0001PART I

COMPLIED WITH

AIRFRAME1646

15-SEP-2011H: 504.20

Notes: COMPLIED WITH

PERFORM NAVIGATION - INSPECTION/CORRECTION OF THEINSTALLATION POSITION OF THE DUAL STATIC PORTS REINSTALLATION OF THE DUAL STATIC PORTS

SB 500-34-0001PART II

COMPLIED WITH

AIRFRAME1647

13-SEP-2011H: 504.20

Notes: COMPLIED WITH

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN

SB 500-34-0002 N/A

AIRFRAME1648Notes: NOT APPLICABLE - CHARTVIEW NOT INSTALLED ON THIS AIRCRAFT

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NAVIGATION - ACTIVATION OF THE CHARTVIEW (REV.11)

SB500-34-0002/11 OPEN

AIRFRAME1888

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN.

SB 500-34-0002R1

N/A

AIRFRAME1649Notes: NOT APPLICABLE - CHARTVIEW NOT INSTALLED ON THIS AIRCRAFT

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN..

SB 500-34-0002R2

N/A

AIRFRAME1650

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN...

SB 500-34-0002R3

N/A

AIRFRAME1651

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN....

SB 500-34-0002R4

N/A

AIRFRAME1652

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN.....

SB 500-34-0002R5

OPEN

AIRFRAME1653

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN......

SB 500-34-0002R6

OPEN

AIRFRAME1654

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN.......

SB 500-34-0002R7

OPEN

AIRFRAME1655

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN........

SB 500-34-0002R8

OPEN

AIRFRAME1656

NAVIGATION - ACTIVATION OF THE CHARTVIEW SERVICEBULLETIN.........

SB 500-34-0002R9

N/A

AIRFRAME1657Notes: NOT APPLICABLE

NAVIGATION - ACTIVATION OF THE FLITECHART SERVICEBULLETIN

SB 500-34-0003 N/A

AIRFRAME1658Notes: NOT APPLICABLE - FLITECHART NOT INSTALLED ON THIS AIRCRAFT

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NAVIGATION - ACTIVATION OF THE FLITECHART SERVICEBULLETIN.

SB 500-34-0003R1

OPEN

AIRFRAME1659

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN

SB 500-34-0004 N/A

AIRFRAME1660

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - NA BY S/N

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) (REV. 7)

SB500-34-0004/07

OPEN

AIRFRAME1932

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I (REV. 8)

SB500-34-0004/08

OPEN

AIRFRAME1962

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN.

SB 500-34-0004R1

N/A

AIRFRAME1661

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN..

SB 500-34-0004R2

N/A

AIRFRAME1662

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

PERFORM NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I REWORK OF THE UPPER FUSELAGE AND INSTALLATION OFTHE HARNESS SUPPORTS

SB 500-34-0004R2 PART II

N/A

AIRFRAME1664

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

PERFORM NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I INSTALLATION OF THE ELECTRICAL HARNESS

SB 500-34-0004R2 PART IV

N/A

AIRFRAME1666

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

PERFORM NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I INSTALLATION OF THE ANTENNA CABLES, POWERAMPLIFIER (PA/LNA), AND TCAS UNIT

SB 500-34-0004R2 PART V

N/A

AIRFRAME1667

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

PERFORM NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCESYSTEM (TCAS) I REWORK OF THE WING-TO-FUSELAGE FAIRING

SB 500-34-0004R2 PI

N/A

AIRFRAME1663

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

PERFORM NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I REWORK OF THE PALMER PANEL

SB 500-34-0004R2 PIII

N/A

AIRFRAME1665

14-SEP-2010H: 260.50L: 312

Notes: NOT APPLICABLE - N/A BY S/N

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN...

SB 500-34-0004R3

OPEN

AIRFRAME1668

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE UPPER FUSELAGE AND INSTALLATION OF THEHARNESS SUPPORTS

SB 500-34-0004R3 PART II

OPEN

AIRFRAME1670

INSTALLATION NAVIGATION - INSTALLATION OF THETRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM(TCAS) I OF THE ELECTRICAL HARNESS

SB 500-34-0004R3 PART IV

OPEN

AIRFRAME1672

INSTALLATION NAVIGATION - INSTALLATION OF THETRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM(TCAS) I OF THE ANTENNA CABLES, POWER AMPLIFIER(PA/LNA), AND TCAS UNIT

SB 500-34-0004R3 PART V

OPEN

AIRFRAME1673

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OFTHE WING-TO-FUSELAGE FAIRING

SB 500-34-0004R3 PI

OPEN

AIRFRAME1669

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE PALMER PANEL

SB 500-34-0004R3 PIII

OPEN

AIRFRAME1671

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN....

SB 500-34-0004R4

OPEN

AIRFRAME1674

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I ON THE WFF AND STRUCTURE; ELECTRICAL AND TCASEQUIPMENT INSTALLATION.

SB 500-34-0004R4 PART II

OPEN

AIRFRAME1676

REMOVAL NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE BOTTOM ANTENNA AND TCAS II TOP ANTENNACOVERS AND TCAS EQUIPMENT INSTALLATION

SB 500-34-0004R4 PART IV

OPEN

AIRFRAME1678

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I ONTHE WFF, STRUCTURE AND PALMER, ELECTRICAL AND TCASEQUIPMENT INSTALLATION.

SB 500-34-0004R4 PI

OPEN

AIRFRAME1675

REMOVAL NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE ANTENNA COVERS AND TCAS EQUIPMENTINSTALLATION

SB 500-34-0004R4 PIII

OPEN

AIRFRAME1677

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN.....

SB 500-34-0004R5

OPEN

AIRFRAME1679

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I ON THE WFF AND STRUCTURE; ELECTRICAL AND TCASEQUIPMENT INSTALLATION

SB 500-34-0004R5 PART II

OPEN

AIRFRAME1681

REMOVAL NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE BOTTOM ANTENNA AND TCAS II TOP ANTENNACOVERS AND TCAS EQUIPMENT INSTALLATION

SB 500-34-0004R5 PART IV

OPEN

AIRFRAME1683

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I ONTHE WFF, STRUCTURE AND PALMER, ELECTRICAL AND TCASEQUIPMENT INSTALLATION

SB 500-34-0004R5 PI

OPEN

AIRFRAME1680

REMOVAL NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE ANTENNA COVERS AND TCAS EQUIPMENTINSTALLATION

SB 500-34-0004R5 PIII

OPEN

AIRFRAME1682

NAVIGATION - INSTALLATION OF THE TRAFFIC ALERT ANDCOLLISION AVOIDANCE SYSTEM (TCAS) I SERVICEBULLETIN......

SB 500-34-0004R6

N/A

AIRFRAME1684

Notes: NOT APPLICABLE

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I ON THE WFF AND STRUCTURE; ELECTRICAL AND TCASEQUIPMENT INSTALLATION..

SB 500-34-0004R6 PART II

N/A

AIRFRAME1686

Notes: NOT APPLICABLE

REMOVAL NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE BOTTOM ANTENNA AND TCAS II TOP ANTENNACOVERS AND TCAS EQUIPMENT INSTALLATION.

SB 500-34-0004R6 PART IV

N/A

AIRFRAME1688

Notes: NOT APPLICABLE

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

REWORK NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I ONTHE WFF, STRUCTURE AND PALMER, ELECTRICAL AND TCASEQUIPMENT INSTALLATION..

SB 500-34-0004R6 PI

N/A

AIRFRAME1685

Notes: NOT APPLICABLE

REMOVAL NAVIGATION - INSTALLATION OF THE TRAFFICALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) I OF THE ANTENNA COVERS AND TCAS EQUIPMENTINSTALLATION.

SB 500-34-0004R6 PIII

N/A

AIRFRAME1687

Notes: NOT APPLICABLE

NAVIGATION - REPLACEMENT OF THE DUAL STATIC PORTSSERVICE BULLETIN

SB 500-34-0006 OPEN

AIRFRAME1689

NAVIGATION - REPLACEMENT OF THE DUAL STATIC PORTSSERVICE BULLETIN.

SB 500-34-0006R1

OPEN

AIRFRAME1690

NAVIGATION - REPLACEMENT OF THE DUAL STATIC PORTSSERVICE BULLETIN..

SB 500-34-0006R2

COMPLIED WITH

AIRFRAME1691

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

NAVIGATION - REPLACEMENT OF THE PITOT-STATIC PROBESERVICE BULLETIN

SB 500-34-0007 COMPLIED WITH

AIRFRAME1692

09-MAY-2011H: 417.20L: 442

Notes: COMPLIED WITH - SB COMPLIED WITH

NAVIGATION - REPLACEMENT OF THE PITOT-STATIC PROBESERVICE BULLETIN.

SB 500-34-0007R1

COMPLIED WITH

AIRFRAME1693

12-MAY-2011H: 417.00L: 442

Notes: COMPLIED WITH

NAVIGATION - REPLACEMENT OF THE TRANSPONDERS 1/2WITH ADS-B OUT FUNCTIONALITY

SB 500-34-0010 OPEN

AIRFRAME1956

NAVIGATION - REPLACEMENT OF THE TRANSPONDERS 1/2WITH ADS-B OUT FUNCTIONALITY (REV. 1)

SB500-34-0010/01

OPEN

AIRFRAME1973

NAVIGATION - DME (DISTANCE MEASURING EQUIPMENT)1 INSTALLATION

SB500-34-0011/00

OPEN

AIRFRAME1992

OXYGEN - REPLACEMENT OF THE ALTITUDE COMPENSATINGREGULATOR (ACR) SERVICE BULLETIN

SB 500-35-0001 OPEN

AIRFRAME1694

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

OXYGEN - REPLACEMENT OF THE ALTITUDE COMPENSATINGREGULATOR (ACR) SERVICE BULLETIN.

SB 500-35-0001R1

OPEN

AIRFRAME1695

OXYGEN - REPLACEMENT OF THE ALTITUDE COMPENSATINGREGULATOR (ACR) SERVICE BULLETIN..

SB 500-35-0001R2

OPEN

AIRFRAME1696

OXYGEN - REPLACEMENT OF THE ALTITUDE COMPENSATINGREGULATOR (ACR) SERVICE BULLETIN...

SB 500-35-0001R3

OPEN600HR/12MOAIRFRAME1697

14-SEP-2014H: 1038.80L: 883

OXYGEN - REPLACEMENT OF THE ALTITUDE COMPENSATINGREGULATOR (ACR) SERVICE BULLETIN....

SB 500-35-0001R4

OPEN

AIRFRAME1698

PNEUMATIC - PRESSURE REGULATING SHUTOFF VALVE(PRSOV) REPLACEMENT (REV. 1)

SB500-36-0001/01

COMPLIED WITH

AIRFRAME1948

14-SEP-2014H: 1038.80L: 833

PNEUMATIC - PRESSURE REGULATING SHUTOFF VALVE(PRSOV) REPLACEMENT (REV. 1) REPLACEMENT(REV. 2)

SB500-36-0001/02

OPEN

AIRFRAME1954

14-SEP-2014H: 1038.80L: 833

PNEUMATIC - PRESSURE REGULATING SHUTOFF VALVE(PRSOV) REPLACEMENT (REV. 3)

SB500-36-0001/03

OPEN

AIRFRAME1981

14-SEP-2014H: 1038.80L: 833

DOORS - MODIFICATION FROM STANDARD MAIN DOOR TOPREMIUM MAIN DOOR SERVICE BULLETIN

SB 500-52-0001 OPEN

AIRFRAME1699

DOORS - MODIFICATION FROM STANDARD MAIN DOOR TOPREMIUM MAIN DOOR SERVICE BULLETIN.

SB 500-52-0001R1

OPEN

AIRFRAME1700

DOORS - MODIFICATION FROM STANDARD MAIN DOOR TOPREMIUM MAIN DOOR SERVICE BULLETIN..

SB 500-52-0001R2

OPEN

AIRFRAME1701

DOORS - MODIFICATION FROM STANDARD MAIN DOOR TOPREMIUM MAIN DOOR SERVICE BULLETIN...

SB 500-52-0001R3

OPEN

AIRFRAME1702

DOORS - MODIFICATION FROM STANDARD MAIN DOOR TOPREMIUM MAIN DOOR SERVICE BULLETIN....

SB 500-52-0001R4

OPEN

AIRFRAME1703

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

DOORS - MODIFICATION FROM STANDARD MAIN DOOR TOPREMIUM MAIN DOOR SERVICE BULLETIN.....

SB 500-52-0001R5

OPEN

AIRFRAME1704

DOORS - IMPROVEMENT ON THE BATTERY LOCK CAM DOORSERVICE BULLETIN

SB 500-52-0002 OPEN

AIRFRAME1705

FUSELAGE - PROTECTION TO PREVENT INTERFERENCEBETWEEN RUDDER CABLE AND AILERON QUADRANT SERVICEBULLETIN

SB 500-53-0001 N/A

AIRFRAME1706

Notes: NOT APPLICABLE - N/A BY AIRCRAFT SERIAL NO

FUSELAGE - REPLACEMENT OF THE LATERAL WINDSHIELDLOWER-BEAM

SB500-53-0002/00

OPEN

AIRFRAME1885

FUSELAGE - REPLACEMENT OF UPPER FITTINGSATTACHMENT PINS OF FRAME 16A, FOR AIRCRAFTPROVISIONED TO INSTALL THE BELTED TOILET SERVICEBULLETIN

SB 500-53-0003 OPEN

AIRFRAME1707

STABILIZERS - REPLACEMENT OF THE NUTS OF THEELEVATOR MASS BALANCE FASTENERS SERVICE BULLETIN

SB 500-55-0001 COMPLIED WITH

AIRFRAME1708

STABILIZERS-INSPECTION AND REPLACEMENT OF THEBARREL SELF-LOCKING NUT.

SB500-55-A004/00

OPEN

AIRFRAME1997

STABILIZERS-INSPECTION AND REPLACEMENT OF THEBARREL SELF-LOCKING NUT. (REV. 1)

SB500-55-A004/01

OPEN

AIRFRAME2000

STABILIZERS-INSPECTION AND REPLACEMENT OF THEBARREL SELF-LOCKING NUT. (REV. 2)

SB500-55-A004/02

OPEN

AIRFRAME2002

WINGS - DRAIN HOLES IN CONTROL SURFACES SERVICEBULLETIN

SB 500-57-0001 COMPLIED WITH

AIRFRAME1709

22-OCT-2010H: 260.00L: 312

Notes: COMPLIED WITH

WINGS - DRAIN HOLES IN CONTROL SURFACES SERVICEBULLETIN.

SB 500-57-0001R1

COMPLIED WITH

AIRFRAME1710

12-SEP-2013H: 786.90L: 722

WINGS - ELIMINATION OF INTERFERENCE IN THE AILERONTAB FITTING BOLT SERVICE BULLETIN

SB 500-57-0003 RECURRING

AIRFRAME1711

12-SEP-2013H: 786.90L: 722

M: 24 12-SEP-2015 M: 7 D: 9

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

WINGS - ELIMINATION OF INTERFERENCE IN THE AILERONTAB FITTING BOLT (REV. 1)

SB500-57-0003/01

OPEN

AIRFRAME1978

WINGS - MISSING BLUE VARNISH IN FUEL COMPONENTSINSTALLATION SERVICE BULLETIN

SB 500-57-0004 OPEN

AIRFRAME1712

VISUAL INSPECTION WINGS - MISSING BLUE VARNISH INFUEL COMPONENTS INSTALLATION FOR CORROSION ON THESTRUCTURE WHERE THE FUEL COMPONENTS ARE INSTALLED.

SB 500-57-0004PART I

RECURRING

AIRFRAME1713

M: 48 03-OCT-2015 M: 8 D: 0

REWORK WINGS - MISSING BLUE VARNISH IN FUELCOMPONENTS INSTALLATION THE STRUCTURE WHERE THEFUEL COMPONENTS WERE INSTALLED, IF NECESSARY.

SB 500-57-0004PART II

RECURRING

AIRFRAME1714

M: 48 03-OCT-2015 M: 8 D: 0

WINGS - REINFORCEMENT OF LOWER SKIN IN MLG BAYSERVICE BULLETIN

SB 500-57-0005 OPEN

AIRFRAME1715

WINGS - REINFORCEMENT OF LOWER SKIN IN MLG BAYSERVICE BULLETIN.

SB 500-57-0005R1

OPEN

AIRFRAME1716

WINGS - REINFORCEMENT OF LOWER SKIN IN MLG BAYSERVICE BULLETIN..

SB 500-57-0005R2

OPEN

AIRFRAME1879

WINGS - LH WING AILERON MECHANISM ATTACHMENT -CHECK FOR PROPER INSTALLATION OF SHIM AND BOLTS

SB500-57-0006/00

OPEN

AIRFRAME1939

POWERPLANT - REPLACEMENT OF FUEL-FILTER IMPENDINGBYPASS SWITCH SERVICE BULLETIN

SB 500-71-0001 COMPLIED WITH

AIRFRAME1717

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

POWERPLANT - AIR BAFFLE INSTALLATION SERVICEBULLETIN

SB 500-71-0002 OPEN

AIRFRAME1718

POWERPLANT - AIR BAFFLE INSTALLATION SERVICEBULLETIN.

SB 500-71-0002R1

OPEN

AIRFRAME1719

POWERPLANT - AIR BAFFLE INSTALLATION SERVICEBULLETIN..

SB 500-71-0002R2

OPEN

AIRFRAME1720

POWERPLANT - VISUAL INSPECTION OF THE RIVETEDJUNCTION LINE OF THE INLET INNER BARREL AND LIPSKIN

SB 500-71-0003 OPEN

AIRFRAME1878

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

ENGINE FUEL AND CONTROL - NEW FADEC (FULLAUTHORITY DIGITAL ENGINE CONTROL) SOFTWAREUPGRADE - VERSION 4.0 SERVICE BULLETIN

SB 500-73-0001 COMPLIED WITH

AIRFRAME1721

12-AUG-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

ENGINE FUEL AND CONTROL - NEW FADEC (FULLAUTHORITY DIGITAL ENGINE CONTROL) SOFTWAREUPGRADE - VERSION 5.3 SERVICE BULLETIN

SB 500-73-0002 OPEN

AIRFRAME1722

ENGINE FUEL AND CONTROL - NEW FADEC (FULLAUTHORITY DIGITAL ENGINE CONTROL) SOFTWAREUPGRADE - VERSION 5.3 SERVICE BULLETIN.

SB 500-73-0002R1

COMPLIED WITH

AIRFRAME1723

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH

ENGINE FUEL AND CONTROL - NEW FADEC (FULLAUTHORITY DIGITAL ENGINE CONTROL) SOFTWAREREPLACEMENT - VERSION 5.5

SB500-73-0003/00

OPEN

AIRFRAME1943

14-SEP-2014H: 1038.80L: 833

ENGINE FUEL AND CONTROL - NEW FADEC (FULLAUTHORITY DIGITAL ENGINE CONTROL) SOFTWAREREPLACEMENT - VERSION 5.5 REPLACEMENT (REV. 1)

SB500-73-0003/01

OPEN

AIRFRAME1955

14-SEP-2014H: 1038.80L: 833

ENGINE FUEL AND CONTROL - NEW FADEC (FULLAUTHORITY DIGITAL ENGINE CONTROL) SOFTWAREVERSION 5.5 REPLACEMENT (REV. 2)

SB500-73-0003/02

OPEN

AIRFRAME1984

14-SEP-2014H: 1038.80L: 833

NO. 1 ENGINE - IGNITION EXCITER - REPLACEMENT OFSERVICE BULLETIN

SB 66001 COMPLIED WITH

ENGINE 11730

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 2 ENGINE - IGNITION EXCITER - REPLACEMENT OFSERVICE BULLETIN

SB 66001 COMPLIED WITH

ENGINE 21804

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH-PRESSURE-COMPRESSOR (HPC)ROTOR-BALANCING-ASSEMBLY ADJUSTING SPACERS -REPLACEMENT OF SERVICE BULLETIN

SB 66002 COMPLIED WITH

ENGINE 11731

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - HIGH-PRESSURE-COMPRESSOR (HPC)ROTOR-BALANCING-ASSEMBLY ADJUSTING SPACERS -REPLACEMENT OF SERVICE BULLETIN

SB 66002 COMPLIED WITH

ENGINE 21805

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 2 ENGINE - HIGH-PRESSURE-TURBINE (HPT) TIESHAFT - MODIFICATION/REPLACEMENT OF SERVICEBULLETIN

SB 66003 OPEN

ENGINE 21806

NO. 1 ENGINE - HIGH-PRESSURE-TURBINE (HPT) TIESHAFT - MODIFICATION/REPLACEMENT OF SERVICEBULLETIN

SB 66003 OPEN

ENGINE 11732

NO. 2 ENGINE - HIGH-PRESSURE-TURBINE (HPT) TIESHAFT - MODIFICATION/REPLACEMENT OF SERVICEBULLETIN.

SB 66003 R1 COMPLIED WITH

ENGINE 21807

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH-PRESSURE-TURBINE (HPT) TIESHAFT - MODIFICATION/REPLACEMENT OF SERVICEBULLETIN.

SB 66003 R1 COMPLIED WITH

ENGINE 11733

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 2 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66004 OPEN

ENGINE 21808

NO. 1 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66004 OPEN

ENGINE 11734

NO. 2 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN.

SB 66004 R1 OPEN

ENGINE 21809

NO. 1 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN.

SB 66004 R1 OPEN

ENGINE 11735

NO. 2 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN..

SB 66004 R2 COMPLIED WITH

ENGINE 21810

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN..

SB 66004 R2 COMPLIED WITH

ENGINE 11736

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - DATA COLLECTION UNIT (DCU) -REPLACEMENT OF SERVICE BULLETIN

SB 66005 COMPLIED WITH

ENGINE 11737

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 2 ENGINE - DATA COLLECTION UNIT (DCU) -REPLACEMENT OF SERVICE BULLETIN

SB 66005 COMPLIED WITH

ENGINE 21811

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH PRESSURE TURBINE (HPT) DISCBALANCING ASSEMBLY - MODIFICATION/REPLACEMENT OFSERVICE BULLETIN

SB 66006 COMPLIED WITH

ENGINE 11738

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 2 ENGINE - HIGH PRESSURE TURBINE (HPT) DISCBALANCING ASSEMBLY - MODIFICATION/REPLACEMENT OFSERVICE BULLETIN

SB 66006 COMPLIED WITH

ENGINE 21812

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN...

SB 66007 N/A

ENGINE 11739

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 2 ENGINE - FUEL METERING UNIT (FMU) -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN...

SB 66007 N/A

ENGINE 21813

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 2 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66008 OPEN

ENGINE 21814

NO. 1 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66008 OPEN

ENGINE 11740

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN.

SB 66008 R1 COMPLIED WITH

ENGINE 21815

14-MAY-2010

Notes: COMPLIED WITH - NEW UNIT INSTALLED WHEN ENGINE INSTALLED

NO. 1 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN.

SB 66008 R1 COMPLIED WITH

ENGINE 11741

14-MAY-2010

Notes: COMPLIED WITH - NEW UNIT INSTALLED WHEN ENGINE INSTALLED

NO. 2 ENGINE - HIGH-PRESSURE-TURBINE (HPT) VANERING ANTI-ROTATION PIN - INTRODUCTION OF SERVICEBULLETIN

SB 66009 COMPLIED WITH

ENGINE 21816

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH-PRESSURE-TURBINE (HPT) VANERING ANTI-ROTATION PIN - INTRODUCTION OF SERVICEBULLETIN

SB 66009 COMPLIED WITH

ENGINE 11742

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH-PRESSURE-TURBINE (HPT) VANERING ANTI-ROTATION PIN - INTRODUCTION OF SERVICEBULLETIN.

SB 66009 R1 OPEN

ENGINE 11743

NO. 2 ENGINE - HIGH-PRESSURE-TURBINE (HPT) VANERING ANTI-ROTATION PIN - INTRODUCTION OF SERVICEBULLETIN.

SB 66009 R1 OPEN

ENGINE 21817

NO. 2 ENGINE - SPECIFIC ENGINE MAINTENANCE PROGRAM- INTRODUCTION OF SERVICE BULLETIN

SB 66010 N/A

ENGINE 21818

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 1 ENGINE - SPECIFIC ENGINE MAINTENANCE PROGRAM- INTRODUCTION OF SERVICE BULLETIN

SB 66010 N/A

ENGINE 11744

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 1 ENGINE - SPECIFIC ENGINE MAINTENANCE PROGRAM- INTRODUCTION OF SERVICE BULLETIN.

SB 66011 N/A

ENGINE 11745

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - SPECIFIC ENGINE MAINTENANCE PROGRAM- INTRODUCTION OF SERVICE BULLETIN.

SB 66011 N/A

ENGINE 21819

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 2 ENGINE - SPECIFIC ENGINE MAINTENANCE PROGRAM- INTRODUCTION OF SERVICE BULLETIN..

SB 66011 R1 OPEN

ENGINE 21820

NO. 1 ENGINE - SPECIFIC ENGINE MAINTENANCE PROGRAM- INTRODUCTION OF SERVICE BULLETIN..

SB 66011 R1 OPEN

ENGINE 11746

NO. 1 ENGINE - OIL PUMP PLAIN SEAL - REPLACEMENTOF SERVICE BULLETIN

SB 66012 OPEN

ENGINE 11747

NO. 2 ENGINE - OIL PUMP PLAIN SEAL - REPLACEMENTOF SERVICE BULLETIN

SB 66012 COMPLIED WITH

ENGINE 21821

18-JUN-2009

Notes: COMPLIED WITH - CATEGORY 6 P&WC RECOMMENDS TO DO THIS SB WHEN THE SUBASSEMBBLY (I.E MODULE, ACCESSORIES, COMPONENTS OR BUILD GROUPS) ISDISASSEMBLED AND ACCESS IS AVAILABLE TO THE NECESSARY PART. DO ALL SPARE SUBASSEMBLIES. INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN

SB 66013 COMPLIED WITH

ENGINE 11748

15-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 2 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN

SB 66013 COMPLIED WITH

ENGINE 21822

18-JUN-2009

Notes: COMPLIED WITH - INCORPORATED AT PRODUCTION

NO. 1 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN.

SB 66013 R1 N/A

ENGINE 11749

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 2 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN.

SB 66013 R1 N/A

ENGINE 21823

14-MAY-2010

Notes: NOT APPLICABLE - N/A BY ENGINE SERIAL NUMBER

NO. 1 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN..

SB 66013 R2 OPEN

ENGINE 11750

NO. 2 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN..

SB 66013 R2 OPEN

ENGINE 21824

NO. 1 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN...

SB 66013 R3 OPEN

ENGINE 11751

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN...

SB 66013 R3 OPEN

ENGINE 21825

NO. 2 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN....

SB 66013 R4 OPEN

ENGINE 21826

NO. 1 ENGINE - HIGH PRESSURE TURBINE (HPT) NUT -REPLACEMENT OF SERVICE BULLETIN....

SB 66013 R4 OPEN

ENGINE 11752

NO. 2 ENGINE - N0. 4 BEARING OIL PRESSURE TUBEASSEMBLY - REPLACEMENT/MODIFICATION OF SERVICEBULLETIN

SB 66014 OPEN

ENGINE 21827

NO. 1 ENGINE - N0. 4 BEARING OIL PRESSURE TUBEASSEMBLY - REPLACEMENT/MODIFICATION OF SERVICEBULLETIN

SB 66014 OPEN

ENGINE 11753

NO. 2 ENGINE - FUEL MANIFOLD ASSEMBLY -REPLACEMENT OF SERVICE BULLETIN

SB 66015 OPEN

ENGINE 21828

NO. 1 ENGINE - FUEL MANIFOLD ASSEMBLY -REPLACEMENT OF SERVICE BULLETIN

SB 66015 OPEN

ENGINE 11754

NO. 1 ENGINE - IGNITER - REPLACEMENT OF SERVICEBULLETIN

SB 66016 OPEN

ENGINE 11755

NO. 2 ENGINE - IGNITER - REPLACEMENT OF SERVICEBULLETIN

SB 66016 OPEN

ENGINE 21829

NO. 1 ENGINE - BYPASS-DUCT FUEL FAIRING ASSEMBLY -REPLACEMENT OF SERVICE BULLETIN

SB 66017 OPEN

ENGINE 11756

NO. 2 ENGINE - BYPASS-DUCT FUEL FAIRING ASSEMBLY -REPLACEMENT OF SERVICE BULLETIN

SB 66017 OPEN

ENGINE 21830

NO. 2 ENGINE - FRONT AND REAR BLEED VALVE ACTUATOR(BVA) BRACKETS - REPLACEMENT OF SERVICE BULLETIN

SB 66018 OPEN

ENGINE 21831

NO. 1 ENGINE - FRONT AND REAR BLEED VALVE ACTUATOR(BVA) BRACKETS - REPLACEMENT OF SERVICE BULLETIN

SB 66018 OPEN

ENGINE 11757

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - FUEL OIL/HEATER EXCHANGER (FOHE)- REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66022 OPEN

ENGINE 21832

NO. 1 ENGINE - FUEL OIL/HEATER EXCHANGER (FOHE)- REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66022 OPEN

ENGINE 11758

NO. 1 ENGINE - FUEL-SHUT-OFF LEVER SUPPORTASSEMBLY - REPLACEMENT OF SERVICE BULLETIN

SB 66023 OPEN

ENGINE 11759

NO. 2 ENGINE - FUEL-SHUT-OFF LEVER SUPPORTASSEMBLY - REPLACEMENT OF SERVICE BULLETIN

SB 66023 OPEN

ENGINE 21833

NO. 2 ENGINE - REPLACEMENT OF THEFUEL-SHUT-OFF-LEVER COTTER PIN BY A SAFETY WIRESERVICE BULLETIN

SB 66024 OPEN

ENGINE 21834

NO. 1 ENGINE - REPLACEMENT OF THEFUEL-SHUT-OFF-LEVER COTTER PIN BY A SAFETY WIRESERVICE BULLETIN

SB 66024 OPEN

ENGINE 11760

NO. 1 ENGINE - TURBINE EXHAUST CASE ASSEMBLY ANDNO. 5 BEARING OIL TUBE BRACKET ASSEMBLIES -REPLACEMENT OF SERVICE BULLETIN

SB 66025 OPEN

ENGINE 11761

NO. 2 ENGINE - TURBINE EXHAUST CASE ASSEMBLY ANDNO. 5 BEARING OIL TUBE BRACKET ASSEMBLIES -REPLACEMENT OF SERVICE BULLETIN

SB 66025 OPEN

ENGINE 21835

NO. 2 ENGINE - TURBINE EXHAUST CASE ASSEMBLY ANDNO. 5 BEARING OIL TUBE BRACKET ASSEMBLIES -REPLACEMENT OF SERVICE BULLETIN.

SB 66025 R1 OPEN

ENGINE 21836

NO. 1 ENGINE - TURBINE EXHAUST CASE ASSEMBLY ANDNO. 5 BEARING OIL TUBE BRACKET ASSEMBLIES -REPLACEMENT OF SERVICE BULLETIN.

SB 66025 R1 OPEN

ENGINE 11762

NO. 1 ENGINE - OIL FILLER AND INDICATOR ASSEMBLY -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66026 OPEN

ENGINE 11763

NO. 2 ENGINE - OIL FILLER AND INDICATOR ASSEMBLY -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66026 OPEN

ENGINE 21837

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 180: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - TIE ROD HIGH PRESSURE TURBINE -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66027 OPEN

ENGINE 21838

NO. 1 ENGINE - TIE ROD HIGH PRESSURE TURBINE -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66027 OPEN

ENGINE 11764

NO. 1 ENGINE - OIL FILLER AND INDICATOR ASSEMBLY -MODIFICATION/REPLACEMENT OF SERVICE BULLETIN

SB 66028 OPEN

ENGINE 11765

NO. 2 ENGINE - OIL FILLER AND INDICATOR ASSEMBLY -MODIFICATION/REPLACEMENT OF SERVICE BULLETIN

SB 66028 OPEN

ENGINE 21839

NO. 1 ENGINE - MODIFICATION/REPLACEMENT OF HPTDISC BALANCING ASSEMBLY AND TRIM BALANCINGINTRODUCTION OF SERVICE BULLETIN

SB 66029 OPEN

ENGINE 11766

NO. 2 ENGINE - MODIFICATION/REPLACEMENT OF HPTDISC BALANCING ASSEMBLY AND TRIM BALANCINGINTRODUCTION OF SERVICE BULLETIN

SB 66029 OPEN

ENGINE 21840

NO. 1 ENGINE - REPLACEMENT OF THE NO. 4 BEARINGOIL PRESSURE TUBE ASSEMBLY AND NEW CLAMPINGINTRODUCTION TO SUIT SERVICE BULLETIN

SB 66030 OPEN

ENGINE 11767

NO. 2 ENGINE - REPLACEMENT OF THE NO. 4 BEARINGOIL PRESSURE TUBE ASSEMBLY AND NEW CLAMPINGINTRODUCTION TO SUIT SERVICE BULLETIN

SB 66030 OPEN

ENGINE 21841

NO. 2 ENGINE - FIELD REPAIR FOR THE NO. 5BEARING-OIL-TUBE DAMPER BRACKET ASSEMBLIES WITHREINFORCING TUBE HALF SLEEVES AND NEW CLAMPINGARRANGEMENT SERVICE BULLETIN

SB 66031 OPEN

ENGINE 21842

NO. 1 ENGINE - FIELD REPAIR FOR THE NO. 5BEARING-OIL-TUBE DAMPER BRACKET ASSEMBLIES WITHREINFORCING TUBE HALF SLEEVES AND NEW CLAMPINGARRANGEMENT SERVICE BULLETIN

SB 66031 OPEN

ENGINE 11768

NO. 1 ENGINE - ELECTRICAL WIRING HARNESS (TT0SENSOR) - REPLACEMENT OF SERVICE BULLETIN

SB 66032 OPEN

ENGINE 11769

NO. 2 ENGINE - ELECTRICAL WIRING HARNESS (TT0SENSOR) - REPLACEMENT OF SERVICE BULLETIN

SB 66032 OPEN

ENGINE 21843

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

Page 181: Operator Make & Model Serial No Date Hours Landings · Item No ATA/AD/SB Description Part No / Serial No / Reference No Disposition Last C/W Group/Tracked Intervals Tolerance Time

Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - BYPASS-DUCT FUEL FAIRING -INSPECTION OF SERVICE BULLETIN

SB 66033 OPEN

ENGINE 21844

NO. 1 ENGINE - BYPASS-DUCT FUEL FAIRING -INSPECTION OF SERVICE BULLETIN

SB 66033 OPEN

ENGINE 11770

NO. 2 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN..

SB 66034 OPEN

ENGINE 21845

NO. 1 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN..

SB 66034 OPEN

ENGINE 11771

NO. 1 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN...

SB 66034 R1 COMPLIED WITH

ENGINE 11772

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 2 ENGINE - ENGINE ELECTRONIC CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN...

SB 66034 R1 COMPLIED WITH

ENGINE 21846

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 1 ENGINE - NO. 4-BEARING FRONT AND REAR CARBONSEAL - REPLACEMENT OF SERVICE BULLETIN

SB 66035 OPEN

ENGINE 11773

NO. 2 ENGINE - NO. 4-BEARING FRONT AND REAR CARBONSEAL - REPLACEMENT OF SERVICE BULLETIN

SB 66035 OPEN

ENGINE 21847

NO. 1 ENGINE - HPT CUP WASHER - REPLACEMENT OFSERVICE BULLETIN

SB 66036 OPEN

ENGINE 11774

NO. 2 ENGINE - HPT CUP WASHER - REPLACEMENT OFSERVICE BULLETIN

SB 66036 OPEN

ENGINE 21848

NO. 1 ENGINE - HPT CUP WASHER - REPLACEMENT OFSERVICE BULLETIN.

SB 66036 R1 OPEN

ENGINE 11775

NO. 2 ENGINE - HPT CUP WASHER - REPLACEMENT OFSERVICE BULLETIN.

SB 66036 R1 OPEN

ENGINE 21849

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - HPT CUP WASHER - REPLACEMENT OFSERVICE BULLETIN..

SB 66036 R2 OPEN

ENGINE 11776

NO. 2 ENGINE - HPT CUP WASHER - REPLACEMENT OFSERVICE BULLETIN..

SB 66036 R2 OPEN

ENGINE 21850

NO. 2 ENGINE - REPLACEMENT/MODIFICATION OFCOMPRESSOR CASE ASSEMBLY SERVICE BULLETIN

SB 66037 OPEN

ENGINE 21851

NO. 1 ENGINE - REPLACEMENT/MODIFICATION OFCOMPRESSOR CASE ASSEMBLY SERVICE BULLETIN

SB 66037 OPEN

ENGINE 11777

NO. 2 ENGINE - REPLACEMENT OF FUEL-FILTERIMPENDING BYPASS SWITCH AND INTRODUCTION OFADAPTER ASSEMBLY SERVICE BULLETIN

SB 66038 OPEN

ENGINE 21852

NO. 1 ENGINE - REPLACEMENT OF FUEL-FILTERIMPENDING BYPASS SWITCH AND INTRODUCTION OFADAPTER ASSEMBLY SERVICE BULLETIN

SB 66038 OPEN

ENGINE 11778

NO. 2 ENGINE - REPLACEMENT OF FUEL-FILTERIMPENDING BYPASS SWITCH AND INTRODUCTION OFADAPTER ASSEMBLY SERVICE BULLETIN.

SB 66038 R1 COMPLIED WITH

ENGINE 21853

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 1 ENGINE - REPLACEMENT OF FUEL-FILTERIMPENDING BYPASS SWITCH AND INTRODUCTION OFADAPTER ASSEMBLY SERVICE BULLETIN.

SB 66038 R1 COMPLIED WITH

ENGINE 11779

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 2 ENGINE - REPLACEMENT OF NUMBER 2 BEARINGSERVICE BULLETIN

SB 66039 OPEN

ENGINE 21854

NO. 1 ENGINE - REPLACEMENT OF NUMBER 2 BEARINGSERVICE BULLETIN

SB 66039 OPEN

ENGINE 11780

NO. 1 ENGINE - REPLACEMENT OF P3 AIR AND OILFAIRING ASSEMBLY SERVICE BULLETIN

SB 66040 OPEN

ENGINE 11781

NO. 2 ENGINE - REPLACEMENT OF P3 AIR AND OILFAIRING ASSEMBLY SERVICE BULLETIN

SB 66040 OPEN

ENGINE 21855

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - REPLACEMENT OF P3 AIR AND OILFAIRING ASSEMBLY SERVICE BULLETIN.

SB 66040 R1 OPEN

ENGINE 21856

NO. 1 ENGINE - REPLACEMENT OF P3 AIR AND OILFAIRING ASSEMBLY SERVICE BULLETIN.

SB 66040 R1 OPEN

ENGINE 11782

NO. 2 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT OF SERVICE BULLETIN

SB 66041 OPEN

ENGINE 21857

NO. 1 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT OF SERVICE BULLETIN

SB 66041 OPEN

ENGINE 11783

NO. 2 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66041 R1 COMPLIED WITH

ENGINE 21858

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 1 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT/MODIFICATION OF SERVICE BULLETIN

SB 66041 R1 COMPLIED WITH

ENGINE 11784

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 2 ENGINE - REPLACEMENT OF OIL NOZZLE ASSEMBLYSERVICE BULLETIN

SB 66042 OPEN

ENGINE 21859

NO. 1 ENGINE - REPLACEMENT OF OIL NOZZLE ASSEMBLYSERVICE BULLETIN

SB 66042 OPEN

ENGINE 11785

NO. 1 ENGINE - REPLACEMENT/MODIFICATION OF FUELMETERING UNIT (FMU) SERVICE BULLETIN

SB 66043 OPEN

ENGINE 11786

NO. 2 ENGINE - REPLACEMENT/MODIFICATION OF FUELMETERING UNIT (FMU) SERVICE BULLETIN

SB 66043 OPEN

ENGINE 21860

NO. 2 ENGINE - REPLACEMENT/MODIFICATION OF FUELMETERING UNIT (FMU) SERVICE BULLETIN.

SB 66043 R1 COMPLIED WITH

ENGINE 21861

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 1 ENGINE - REPLACEMENT/MODIFICATION OF FUELMETERING UNIT (FMU) SERVICE BULLETIN.

SB 66043 R1 COMPLIED WITH

ENGINE 11787

13-SEP-2011H: 504.20C: 504.00

Notes: COMPLIED WITH

NO. 1 ENGINE - INSPECTION OF PRIMARY AND SECONDARYFUEL FAIRING REDUCERS SERVICE BULLETIN

SB 66044 OPEN

ENGINE 11788

NO. 2 ENGINE - INSPECTION OF PRIMARY AND SECONDARYFUEL FAIRING REDUCERS SERVICE BULLETIN

SB 66044 OPEN

ENGINE 21862

NO. 2 ENGINE - REPLACEMENT/MODIFICATION OF P3 AIRPASSAGE SPACER SERVICE BULLETIN

SB 66045 OPEN

ENGINE 21863

NO. 1 ENGINE - REPLACEMENT/MODIFICATION OF P3 AIRPASSAGE SPACER SERVICE BULLETIN

SB 66045 OPEN

ENGINE 11789

NO. 2 ENGINE - REPLACEMENT OF ELECTRICAL WIRINGHARNESS SERVICE BULLETIN

SB 66046 OPEN

ENGINE 21864

NO. 1 ENGINE - REPLACEMENT OF ELECTRICAL WIRINGHARNESS SERVICE BULLETIN

SB 66046 OPEN

ENGINE 11790

NO. 1 ENGINE - ELECTRICAL WIRING HARNESS -REPLACEMENT OF (REV. 1)

SB 66046 R1 OPEN

ENGINE 11909

NO. 2 ENGINE - ELECTRICAL WIRING HARNESS -REPLACEMENT OF (REV. 1)

SB 66046 R1 OPEN

ENGINE 21910

NO. 1 ENGINE - REPLACEMENT OF HP DIFFUSER CASEASSEMBLY SERVICE BULLETIN

SB 66047 OPEN

ENGINE 11791

NO. 2 ENGINE - REPLACEMENT OF HP DIFFUSER CASEASSEMBLY SERVICE BULLETIN

SB 66047 OPEN

ENGINE 21865

NO. 1 ENGINE - REPLACEMENT OF OIL PUMP AND FILTERHOUSING SERVICE BULLETIN

SB 66048 OPEN

ENGINE 11792

NO. 2 ENGINE - REPLACEMENT OF OIL PUMP AND FILTERHOUSING SERVICE BULLETIN

SB 66048 OPEN

ENGINE 21866

NO. 1 ENGINE - REPLACEMENT/MODIFICATION OF FUELOIL HEAT EXCHANGER SERVICE BULLETIN

SB 66049 OPEN

ENGINE 11793

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COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - REPLACEMENT/MODIFICATION OF FUELOIL HEAT EXCHANGER SERVICE BULLETIN

SB 66049 OPEN

ENGINE 21867

NO. 1 ENGINE - TURBOFAN ENGINE - COMPRESSOR CASEASSEMBLY - REPLACEMENT OF SERVICE BULLETIN

SB 66050 OPEN

ENGINE 11794

NO. 2 ENGINE - TURBOFAN ENGINE - COMPRESSOR CASEASSEMBLY - REPLACEMENT OF SERVICE BULLETIN

SB 66050 OPEN

ENGINE 21868

NO. 2 ENGINE - REPLACEMENT OF DATA COLLECTION UNIT(DCU) SERVICE BULLETIN

SB 66051 OPEN

ENGINE 21869

NO. 1 ENGINE - REPLACEMENT OF DATA COLLECTION UNIT(DCU) SERVICE BULLETIN

SB 66051 OPEN

ENGINE 11795

NO. 2 ENGINE - REPLACEMENT OF HIGH PRESSURETURBINE TIE ROD SERVICE BULLETIN

SB 66053 OPEN

ENGINE 21870

NO. 1 ENGINE - REPLACEMENT OF HIGH PRESSURETURBINE TIE ROD SERVICE BULLETIN

SB 66053 OPEN

ENGINE 11796

NO. 2 ENGINE - HIGH PRESSURE TURBINE TIE ROD -REPLACEMENT OF (REV. 1)

SB 66053 R1 OPEN

ENGINE 21908

NO. 1 ENGINE - HIGH PRESSURE TURBINE TIE ROD -REPLACEMENT OF (REV. 1)

SB 66053 R1 OPEN

ENGINE 11907

NO. 1 ENGINE - INSPECTION OF - HP DIFFUSER CASEASSY SERVICE BULLETIN

SB 66054 OPEN

ENGINE 11797

NO. 2 ENGINE - INSPECTION OF - HP DIFFUSER CASEASSY SERVICE BULLETIN

SB 66054 OPEN

ENGINE 21871

NO. 1 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT OF

SB 66055 OPEN

ENGINE 11933

14-SEP-2014H: 1038.80C: 883.00

NO. 2 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT OF

SB 66055 OPEN

ENGINE 21934

14-SEP-2014H: 1038.80C: 833.00

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

NO. 2 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT/MODIFICATION OF (REV. 1)

SB 66055 R1 OPEN

ENGINE 21941

14-SEP-2014H: 1038.80C: 833.00

NO. 1 ENGINE - ELECTRONIC ENGINE CONTROL -REPLACEMENT/MODIFICATION OF (REV. 1)

SB 66055 R1 OPEN

ENGINE 11940

14-SEP-2014H: 1038.80C: 883.00

NO. 2 ENGINE - NO. 4 BEARING FRONT AND REAR CARBONSEALS - REPLACEMENT OF

SB 66056 OPEN

ENGINE 21938

NO. 1 ENGINE - NO. 4 BEARING FRONT AND REAR CARBONSEALS - REPLACEMENT OF

SB 66056 OPEN

ENGINE 11937

NO. 1 ENGINE - NO. 4 BEARING FRONT AND REAR CARBONSEALS - REPLACEMENT OF (REV. 1)

SB 66056 R1 OPEN

ENGINE 11945

NO. 2 ENGINE - NO. 4 BEARING FRONT AND REAR CARBONSEALS - REPLACEMENT OF (REV. 1)

SB 66056 R1 OPEN

ENGINE 21946

TO REMOVE FROM SERVICE FIRE EXTINGUISHERS THATHAVE THIS INCOMPLETE CRIMPING OF THE SIPHON TUBEFEDERAL AVIATION ADMINISTRATION

AD 2003-26-14 N/A

AIRFRAME1361

Notes: NOT APPLICABLE

FIRE PROTECTION - PORTABLE FIRE EXTINGUISHERS ?IDENTIFICATION / REPLACEMENT EASA (E)

AD 2009-0251 N/A

AIRFRAME1351

19-MAY-2011

Notes: NOT APPLICABLE - NOT APPLICABLE TYPE NOT FITTED

FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS ?IDENTIFICATION / REPLACEMENT EASA

AD 2009-0262 N/A

AIRFRAME1352Notes: NOT APPLICABLE - SUPERSEDED BY REV 1

FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS ?IDENTIFICATION / REPLACEMENT EASA.

AD 2009-0262 R1 N/A

AIRFRAME1353

19-MAY-2011

Notes: NOT APPLICABLE - NOT APPLICABLE TYPE NOT FITTED

FIRE PROTECTION - PORTABLE HALON 1211 FIREEXTINGUISHERS ? IDENTIFICATION / REPLACEMENT EASA

AD 2009-0278 N/A

AIRFRAME1354

10-JUL-2010

Notes: NOT APPLICABLE - N/A EQUIPMENT NOT FITTED

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

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Items

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INCORPORATE INTO THE AIRPLANE FLIGHT MANUAL(AFM) THE PROCEDURES AND LIMITATIONS SECTIONREVISIONS FEDERAL AVIATION ADMINISTRATION

AD 2009-05-06 N/A BY SN

AIRFRAME1362

13-OCT-2009

REPLACEMENT OF THE NUTS OF THE RIGHT AND LEFTELEVATORS MASS BALANCE FASTENERS BRAZILIANAIRWORTHINESS DIRECTIVE

AD 2009-09-01 COMPLIED WITH

AIRFRAME1322

13-OCT-2009

Notes: COMPLIED WITH

MODIFICATION OF THE APPROVED AIRPLANE FLIGHTMANUAL (AFM) BRAZILIAN AIRWORTHINESS DIRECTIVE

AD 2009-10-01 COMPLIED WITH

AIRFRAME1323

13-OCT-2009

Notes: COMPLIED WITH

MODIFICATION OF THE APPROVED AIRPLANE FLIGHTMANUAL (AFM) BRAZILIAN AIRWORTHINESS DIRECTIVE.

AD 2009-10-01 R1 N/A

AIRFRAME1877

19-JUL-2010

Notes: NOT APPLICABLE - N/A ANAC AIRCRAFT ONLY

MODIFICATION MODIFICATION OF THE APPROVEDAIRPLANE FLIGHT MANUAL (AFM) BRAZILIAN OF THEAPPROVED AIRPLANE FLIGHT MANUAL (AFM) (PART 1)

AD 2009-10-01 R2 N/A

AIRFRAME1325

MODIFICATION MODIFICATION OF THE APPROVEDAIRPLANE FLIGHT MANUAL (AFM) BRAZILIAN OF THEAPPROVED AIRPLANE FLIGHT MANUAL (AFM) (PART 2)

AD 2009-10-01 R2 N/A

AIRFRAME1326

MODIFICATION OF THE APPROVED AIRPLANE FLIGHTMANUAL (AFM) BRAZILIAN AIRWORTHINESS DIRECTIVE

AD 2009-10-01 R2 COMPLIED WITH

AIRFRAME1324

12-JUL-2010H: 203.30L: 241

Notes: COMPLIED WITH - AMENDMENT INCORPORATED IN AFN

MODIFICATION OF THE APPROVED AIRPLANE FLIGHTMANUAL (AFM) BRAZILIAN AIRWORTHINESS DIRECTIVE

AD 2009-10-01 R3 N/A

AIRFRAME1327

12-JUL-2010H: 203.30L: 241

Notes: NOT APPLICABLE - REVISE TERMINATION DETAILS ON#

MODIFICATION MODIFICATION OF THE APPROVEDAIRPLANE FLIGHT MANUAL (AFM) BRAZILIAN OF THEAPPROVED AIRPLANE FLIGHT MANUAL (AFM) (PART 2)

AD 2009-10-01 R3 N/A

AIRFRAME1329

12-JUL-2010H: 203.30L: 241

Notes: NOT APPLICABLE - REVISE TERMINATION DETAILS ON#

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

MODIFICATION MODIFICATION OF THE APPROVEDAIRPLANE FLIGHT MANUAL (AFM) BRAZILIAN OF THEAPPROVED AIRPLANE FLIGHT MANUAL (AFM) (PART 1)

AD 2009-10-01 R3 N/A

AIRFRAME1328

12-JUL-2010H: 203.30L: 241

Notes: NOT APPLICABLE - REVISE TERMINATION DETAILS ON#

INSERTION OF INFORMATION INTO THE ABNORMALPROCEDURES SECTION OF THE FAA-APPROVED AIRPLANEFLIGHT MANUAL (AFM) FEDERAL AVIATIONADMINISTRATION

AD 2009-23-11 N/A BY SN

AIRFRAME1363

10-DEC-2009

REPLACEMENT OF THE NUTS OF THE RIGHT AND LEFTELEVATORS MASS BALANCE FASTENERS FEDERAL AVIATIONADMINISTRATION

AD 2009-24-14 N/A BY SN

AIRFRAME1364

10-DEC-2009

REPLACE PORTABLE HALON 1211 (BCF) FIREEXTINGUISHERS MANUFACTURED BY FIRE FIGHTINGENTERPRISES LIMITED WITH SERVICEABLE FIREEXTINGUISHERS FEDERAL AVIATION ADMINISTRATION

AD 2010-01-03 N/A

AIRFRAME1365

REPLACE ALL TYPE H1-10 AIR HALON 1211 (BCF)PORTABLE FIRE EXTINGUISHERS MANUFACTURED BY SICLI,HAVING P/N 1708337B4 FEDERAL AVIATIONADMINISTRATION

AD 2010-04-16 N/A

AIRFRAME1366

REWORK THE ELEVATORS, ELEVATORS TRIM TABS ANDAILERONS SURFACES BY DRILLING ADDITIONAL DRAINHOLES IN THEM BRAZILIAN AIRWORTHINESS DIRECTIVE

AD 2010-07-01 COMPLIED WITH

AIRFRAME1330

22-SEP-2010H: 260.50L: 312

Notes: COMPLIED WITH

TO ENSURE THAT THE FLIGHTCREW HAS ACCURATELOCALIZER AND GLIDESLOPE DEVIATION INDICATIONSFEDERAL AVIATION ADMINISTRATION

AD 2010-07-02 N/A

AIRFRAME1367

REPLACE THE FCSOV OF PN 1300230-13 AND PN1300230-23 WITH NEW IMPROVED ONES PN 1300230-15AND PN 1300230-25, RESPECTIVELY BRAZILIANAIRWORTHINESS DIRECTIVE

AD 2010-08-01 COMPLIED WITH

AIRFRAME1331

10-FEB-2010

Notes: COMPLIED WITH - SB 500-21-0001 IMPLEMENTED 2/10/2010

WIRING HARNESS W101 REWORK BRAZILIAN AIRWORTHINESSDIRECTIVE

AD 2010-09-02 COMPLIED WITH

AIRFRAME1332

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH - SB 500-24-0002 ELECTRICAL POWER - PROTECTION TO PREVENT INTERFERENCES WITH HARNESS W101.

TO PROVIDE THE FLIGHTCREW WITH PROCEDURES TORECOVER FROM OR WORK AROUND THESE SOFTWAREANOMALIES DURING FLIGHT FEDERAL AVIATIONADMINISTRATION

AD 2010-09-04 N/A

AIRFRAME1368

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Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

REPLACEMENT OF BOTH AOA SENSORS AND ITS COVERPLATE BRAZILIAN AIRWORTHINESS DIRECTIVE

AD 2010-11-01 N/A BY SN

AIRFRAME1333

TO PREVENT AN OXYGEN CYLINDER FROM RUPTURINGFEDERAL AVIATION ADMINISTRATION

AD 2010-11-05 N/A

AIRFRAME1369

INSERTION OF INFORMATION INTO THE ABNORMALPROCEDURES SECTION OF THE FAA-APPROVED AIRPLANEFLIGHT MANUAL (AFM) FEDERAL AVIATIONADMINISTRATION.

AD 2010-15-09 N/A BY SN

AIRFRAME1370

15-JUN-2010

NO. 1 ENGINE - REPLACEMENT OF THE FOHE FUEL FILTERBYPASS POPPET VALVE

AD 2010-17-01 COMPLIED WITH

ENGINE 11724

18-DEC-2009H: 44.10

Notes: COMPLIED WITH - SB P&W A66021 SB COMPLIED WITH

NO. 2 ENGINE - REPLACEMENT OF THE FOHE FUEL FILTERBYPASS POPPET VALVE

AD 2010-17-01 N/A

ENGINE 21798

27-FEB-2012H: 581.20C: 579.00

Notes: NOT APPLICABLE

REWORK OF THE ELEVATORS, ELEVATORS TRIM TABS, ANDAILERONS SURFACES BY DRILLING ADDITIONAL DRAINHOLES IN THEM FEDERAL AVIATION ADMINISTRATION

AD 2010-21-15 COMPLIED WITH

AIRFRAME1371

22-OCT-2010H: 260.00L: 312

Notes: COMPLIED WITH

REPLACEMENT OF BOTH FLOW CONTROL SHUTOFF VALVES,PART NUMBER (P/N) 1300230-13 AND P/N 1300230-23,WITH P/N 1300230-15 AND P/N 1300230-25 FEDERALAVIATION ADMINISTRATION

AD 2010-23-16 PCW

AIRFRAME1372

10-FEB-2010H: 500.00L: 500

OXYGEN - OXYGEN MASK REGULATOR INFLATABLE HARNESS- IDENTIFICATION / REPLACEMENT EASA

AD 2011-0090 R1 N/A

AIRFRAME1355

23-MAY-2013H: 738.50L: 690

M: 24 23-MAY-2015 M: 3 D: 20

INSTALL CLAMPS AND PROTECTION SLEEVES TO HARNESSW101 WITHIN THE COCKPIT AREA AND REWORK STRUCTURESTO ELIMINATE THE FRETTING SPOTS OF THE HARNESSWITH THE MAIN DOOR LOCKING MECHANISM AND WITH THEOXYGEN TUBE FEDERAL AVIATION ADMINISTRATION

AD 2011-01-04 PCW

AIRFRAME1373

13-SEP-2011

TO PREVENT PBE UNITS FROM IGNITING FEDERALAVIATION ADMINISTRATION

AD 2011-01-09 N/A

AIRFRAME1374

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Item NoATA/AD/SB Description

Part No / Serial No / Reference NoDisposition Last C/WGroup/Tracked

Intervals Tolerance Time At Inst Next DueInstalled

RemainingAdjustment

Items

Copyright © Flightdocs, Inc. All Rights Reserved.

TO PREVENT HAZARD OF CHEMICAL OXYGEN GENERATORS INTHE LAVATORIES.(SUPERSEDED BY AD 2012-11-09)FEDERAL AVIATION ADMINISTRATION

AD 2011-04-09 N/A

AIRFRAME1375

REPLACEMENT OF BOTH AOA SENSORS, REWORK ANDREIDENTIFICATION OF THE RESPECTIVE COVER PLATESAND SEALANT APPLICATION ON THE INTERFACE BETWEENTHE AOA SENSORS AND COVER PLATES, IF NECESSARY(PARA A) (DESC. CONT.)

AD 2011-05-03 COMPLIED WITH

AIRFRAME1335

13-SEP-2011H: 504.20L: 504

Notes: (DESC. CONT. BRAZILIAN AIRWORTHINESS DIRECTIVE RESTATEMENTS OF REQUIREMENTS OF AD 2010-11-01, WITH REVISED INSTRUCTIONS) COMPLIED WITH

PERFORM REPLACEMENT OF BOTH AOA SENSORS, REWORKAND REIDENTIFICATION OF THE RESPECTIVE COVERPLATES AND SEALANT APPLICATION ON THE INTERFACEBETWEEN THE AOA SENSORS AND COVER PLATES, IFNECESSARY (GVI) (PARA B) (DESC. CONT.)

AD 2011-05-03 COMPLIED WITH

AIRFRAME1336

13-SEP-2011H: 504.20L: 504

Notes: (DESC. CONT. BRAZILIAN AIRWORTHINESS DIRECTIVE A GENERAL VISUAL INSPECTION (GVI) TO DETERMINE IF THE SEALANT IS CORRECTLY APPLIED ON THEINTERFACE BETWEEN AOA COVER PLATES AND AOA SENSORS) COMPLIED WITH

REPLACEMENT OF BOTH AOA SENSORS, REWORK ANDREIDENTIFICATION OF THE RESPECTIVE COVER PLATESAND SEALANT APPLICATION ON THE INTERFACE BETWEENTHE AOA SENSORS AND COVER PLATES, IF NECESSARY.BRAZILIAN AIRWORTHINESS DIRECTIVE

AD 2011-05-03 COMPLIED WITH

AIRFRAME1334

13-SEP-2011H: 504.20L: 504

Notes: COMPLIED WITH - AD COMPLIED WITH BY SB500-27-006 R2

TO PREVENT FAILURE OF THE BACKREST LINKS FEDERALAVIATION ADMINISTRATION

AD 2011-07-05 N/A

AIRFRAME1376

22-MAR-2012H: 587.40L: 584

Notes: NOT APPLICABLE

REPLACE ALL SEAT AND SEATING SYSTEMS MANUFACTUREDBY KOITO INDUSTRIES BRAZILIAN AIRWORTHINESSDIRECTIVE

AD 2011-09-01 N/A

AIRFRAME1337

22-MAR-2012H: 587.40L: 584

Notes: NOT APPLICABLE

TO PREVENT THE IN-LINE FLOW INDICATORS OF THEOXYGEN MASK ASSEMBLY FROM FRACTURING ANDSEPARATING FEDERAL AVIATION ADMINISTRATION

AD 2011-14-08 N/A

AIRFRAME1377

REPLACEMENT OF BOTH ANGLE OF ATTACK (AOA)SENSORS AND COVER PLATES, INSPECTION OF THE SENSORAREA, AND, IF NEEDED, APPLICATION OF SEALANTBETWEEN THE AOA COVERS AND THE AOA SENSORS.FEDERAL AVIATION ADMINISTRATION

AD 2011-17-15 N/A

AIRFRAME1378

13-SEP-2011H: 504.20L: 504

Notes: NOT APPLICABLE - EASA AIRCRAFT. SB 500-27-0006 R2 CHANGE OF ANGLE OF ATTACK (AOA) SENSOR FROM PN C-100117-2 TO PN C-100117-3 SERVICEBULLETIN.

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PREVENT TCAS UNITS FROM DROPPING TRACKS FEDERALAVIATION ADMINISTRATION

AD 2012-02-08 RECURRING

AIRFRAME1379

M: 36 13-MAR-2015 M: 1 D: 10

AMEND OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR-IDENTIFICATION / OPERATIONAL PROCEDURE /REPLACEMENT EASA AIRCRAFT FLIGHT MANUAL (AFM)(2.2)

AD 2012-0254 N/A

AIRFRAME1344

Notes: NOT APPLICABLE - N/A BY MANF/PART NUMBER FITTED

REPLACE OXYGEN - FLIGHT CREW OXYGEN MASKREGULATOR -IDENTIFICATION / OPERATIONAL PROCEDURE/ REPLACEMENT EASA AFFECTED OXYGEN MASK REGULATOR(2.1)

AD 2012-0254 N/A

AIRFRAME1343

Notes: NOT APPLICABLE - N/A BY MANF/PART NUMBER FITTED

INSPECT/CHECK OXYGEN - FLIGHT CREW OXYGEN MASKREGULATOR -IDENTIFICATION / OPERATIONAL PROCEDURE/ REPLACEMENT EASA OXYGEN MASK REGULATOR TOINDENTIFY THE P/N AND S/N (1)

AD 2012-0254 N/A

AIRFRAME1342

26-APR-2013H: 713.10L: 673

OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR-IDENTIFICATION / OPERATIONAL PROCEDURE /REPLACEMENT EASA AIRWORTHINESS DIRECTIVE

AD 2012-0254 N/A

AIRFRAME1341

Notes: NOT APPLICABLE - N/A BY MANF/PART NUMBER FITTED

REPLACE OXYGEN - FLIGHT CREW OXYGEN MASKREGULATOR -IDENTIFICATION / OPERATIONAL PROCEDURE/ REPLACEMENT EASA EACH AFFECTED FLIGHT CREWOXYGEN MASK REGULATOR WITH A SERVICEABLE (PART3)

AD 2012-0254 N/A

AIRFRAME1345

24-NOV-2014 M: 12 24-NOV-2015 M: 9 D: 21

REESTABLISHMENT OF NON-HAZARDOUS SUPPLEMENTALOXYGEN SUPPLY IN LAVATORIES BRAZILIAN ASUPPLEMENTAL OXYGEN SYSTEM (F)

AD 2012-08-04 N/A

AIRFRAME1340

18-MAY-2011

REESTABLISHMENT OF NON-HAZARDOUS SUPPLEMENTALOXYGEN SUPPLY IN LAVATORIES BRAZILIAN ALL CHEMICALOXYGEN GENERATORS IN THE LAVATORIES UNTIL OXYGENSUPPLY IS EXPENDED (C )

AD 2012-08-04 N/A

AIRFRAME1339

REESTABLISHMENT OF NON-HAZARDOUS SUPPLEMENTALOXYGEN SUPPLY IN LAVATORIES BRAZILIANAIRWORTHINESS DIRECTIVE

AD 2012-08-04 N/A

AIRFRAME1338

DISCHARGE ELIMINATE ALL CHEMICAL OXYGENGENERATORS AND INSTALL NEW SUPPLEMENTAL OXYGENSYSTEM IN AFFECTED LAVATORIES FEDERAL AVIATIONADMINISTRATION ALL CHEMICAL OXYGEN GENERATORS(PARA G)

AD 2012-11-09 N/A

AIRFRAME1381

20-SEP-2012H: 662.00L: 637

Notes: NOT APPLICABLE - NO OXYGEN GENERATORS INSTALLED

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INSTALL ELIMINATE ALL CHEMICAL OXYGEN GENERATORSAND INSTALL NEW SUPPLEMENTAL OXYGEN SYSTEM INAFFECTED LAVATORIES FEDERAL AVIATIONADMINISTRATION A SUPPLEMENTAL OXYGEN SYSTEM THATMEETS ALL APPLICABLE (PARA L) (DESC. CONT.)

AD 2012-11-09 N/A

AIRFRAME1382

20-SEP-2012H: 662.00L: 637

Notes: (DESC. CONT. SECTIONS OF PARTS 25 AND 121 OF THE FEDERAL AVIATION REGULATIONS (14 CFR PART 25 AND 14 CFR PART 121) IN EACH LAVATORY) NOTAPPLICABLE - NO OXYGEN GENERATORS INSTALLED

ELIMINATE ALL CHEMICAL OXYGEN GENERATORS ANDINSTALL NEW SUPPLEMENTAL OXYGEN SYSTEM IN AFFECTEDLAVATORIES FEDERAL AVIATION ADMINISTRATION

AD 2012-11-09 N/A

AIRFRAME1380

20-SEP-2012H: 662.00L: 637

Notes: NOT APPLICABLE - NO OXYGEN GENERATORS INSTALLED

VERIFY EQUIPMENT & FURNISHINGS - SAFETY BELTS /TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENTEASA IF THE ORGANISATION IS LISTED AMONG THEAUTHORIZED MAINTENANCE OR REPAIR ORGANISATIONREFERENCE DOCUMENTS (2) (DESC. CONT.)

AD 2013-0020 N/A BY SN

AIRFRAME1358

18-JUN-2011

REMOVE EQUIPMENT & FURNISHINGS - SAFETY BELTS /TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENTEASA AND REPLACE BELTS NOT MEETING THECERTIFICATION REQUIREMENTS OR MAKE RELEVANT SEATINOPERATIVE (3)

AD 2013-0020 N/A

AIRFRAME1359

24-NOV-2014 M: 18 24-MAY-2016 M: 15 D: 21

INSPECT EQUIPMENT & FURNISHINGS - SAFETY BELTS /TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENTEASA THE MARKINGS OF SAFETY BELTS AND/OR TORSORESTRAINT SYSTEMS, TO DETERMINE IF THEY HAVE BEENMAINTAINED OR REPAIRED BY (1) (DESC. CONT.)

AD 2013-0020 N/A

AIRFRAME1357

18-JUN-2011

EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSORESTRAINT SYSTEMS - INSPECTION / REPLACEMENT EASA

AD 2013-0020 N/A

AIRFRAME1356

EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSORESTRAINT SYSTEMS - INSPECTION / REPLACEMENT EASAAIRWORTHINESS DIRECTIVE

AD 2013-0020 R1 N/A

AIRFRAME1346

EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSORESTRAINT SYSTEMS - INSPECTION / REPLACEMENT EASA AFTER 14 FEBRUARY 2013 [THE EFFECTIVE DATE OF THEORIGINAL ISSUE OF THIS AD], DO NOT INSTALL SAFETYBELTS OR TORSO RESTRAINT SYSTEMS (4) (DESCCONT.)

AD 2013-0020 R1 N/A

AIRFRAME1350

04-JUN-2013

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EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSORESTRAINT SYSTEMS - INSPECTION / REPLACEMENT EASA INSPECT THE MARKINGS OF SAFETY BELTS AND/OR TORSORESTRAINT SYSTEMS, TO DETERMINE IF THEY HAVE BEENMAINTAINED OR REPAIRED BY (1) (DESC. CONT.)

AD 2013-0020 R1 N/A

AIRFRAME1347

16-MAY-2014

EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSORESTRAINT SYSTEMS - INSPECTION / REPLACEMENT EASA REMOVE AND REPLACE BELTS NOT MEETING THECERTIFICATION REQUIREMENTS OR MAKE RELEVANT SEATINOPERATIVE (3)

AD 2013-0020 R1 N/A

AIRFRAME1349

EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSORESTRAINT SYSTEMS - INSPECTION / REPLACEMENT EASA VERIFY IF THE ORGANISATION IS LISTED AMONG THEAUTHORIZED MAINTENANCE OR REPAIR ORGANIZATIONREFERENCE DOCUMENTS QUOTED IN THE REF.PUBLICATIONS SECTION (2)

AD 2013-0020 R1 N/A

AIRFRAME1348

TO DETECT AND CORRECT CRACKING OF THE BARREL NUTSAT THE HORIZONTAL STABILIZER-TO-VERTICALSTABILIZER ATTACHMENT JOINT (EFFECTIVE UPONRECEIPT)

AD 2014-15-51E N/A

AIRFRAME1999

30-JUL-2014

Notes: NOT APPLICABLE BY AIRCRAFT SERIAL NUMBER.

NO. 1 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL FILTER BYPASS VALVE WEAR CANADIANAIRWORTHINESS DIRECTIVE

AD CF-2010-02 COMPLIED WITH

ENGINE 11725

18-DEC-2009H: 45.10C: 50.00

Notes: COMPLIED WITH

NO. 2 ENGINE - FUEL OIL HEAT EXCHANGER (FOHE)FUEL FILTER BYPASS VALVE WEAR CANADIANAIRWORTHINESS DIRECTIVE

AD CF-2010-02 COMPLIED WITH

ENGINE 21799

18-DEC-2009H: 45.10C: 50.00

Notes: COMPLIED WITH

INCLUSION OF A TEMPORARY LIMITATION TO THEANAC-APPROVED AIRPLANE FLIGHT MANUAL (AFM)BRAZILIAN EMERGENCY AIRWORTHINESS DIRECTIVE

AD E2009-02-04 COMPLIED WITH

AIRFRAME1321

19-MAY-2011

Notes: COMPLIED WITH - IMPLEMENTED AT BUILD

LAVATORY PAPER OR LINEN WASTE RECEPTACLE FIREPREVENTION FEDERAL AVIATION ADMINISTRATION

AD 74-08-09 R3 OPEN

AIRFRAME1360

06-JUN-2014H: 996.80L: 852

H: 1000.00 H: 1996.80 H: 850.10

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