operator make & model serial no date hours landings · item no ata/ad/sb description part no /...
TRANSCRIPT
![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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/1.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/2.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/3.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/4.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/5.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/6.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/7.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/8.jpg)
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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/9.jpg)
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
Page 9 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.
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
Page 10 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 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.
Page 11 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.
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
Copyright © Flightdocs, Inc. All Rights Reserved.
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
Page 13 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.
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
Page 14 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.
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
Page 15 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.
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
Page 16 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.
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
Page 17 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.
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
Page 18 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.
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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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.
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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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 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
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.
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
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.
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
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.
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
Page 25 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.
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
Page 26 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.
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
Page 27 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.
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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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 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
Page 29 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 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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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 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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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.
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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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.
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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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 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
Page 34 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.
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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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 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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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/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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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 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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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 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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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 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
Copyright © Flightdocs, Inc. All Rights Reserved.
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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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.
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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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 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
Page 44 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.
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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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.
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
Page 46 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.
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
Page 47 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.
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
Page 48 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.
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
Page 49 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.
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
Page 50 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.
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
Page 51 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.
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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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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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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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.
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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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.
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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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.
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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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.
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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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 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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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 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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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 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
Page 62 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.
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
Page 63 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.
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
Page 64 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.
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
Page 65 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.
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
Page 66 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.
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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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.
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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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.
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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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.
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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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.
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
Page 71 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.
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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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
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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
Page 73 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.
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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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.
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
Page 75 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.
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
Page 76 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.
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
Page 77 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.
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
Page 78 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.
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
Page 79 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.
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
Page 80 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.
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
Page 81 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.
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
Page 82 of 193
PROJECTED TO DATE: N/A HOURS: N/A LANDINGS: - CYCLES: - APU HOURS: N/A
COMPLETE TRACKED ITEMS N80EJ 03-FEB-2015
![Page 83: 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](https://reader033.vdocuments.net/reader033/viewer/2022042016/5e7488d67a94bc2e0823d19c/html5/thumbnails/83.jpg)
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.
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
Page 83 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.
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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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.
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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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.
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
Page 86 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.
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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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.
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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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 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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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.
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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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.
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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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.
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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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.
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
Page 93 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.
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
Page 94 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.
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
Page 95 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.
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
Page 96 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.
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
Page 97 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.
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
Page 98 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.
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
Page 99 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.
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
Page 100 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.
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
Page 101 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.
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
Page 102 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.
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
Page 103 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 - 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
Page 104 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 - 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
Page 105 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 - 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
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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
Page 107 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.
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
Page 108 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 - 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
Page 110 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 - 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
Page 111 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 - 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
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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.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
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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.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
Page 114 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 - 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
Page 115 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 - 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
Page 116 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 - 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
Page 117 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 - 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
Page 119 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 - 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
Page 120 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 - 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
Page 121 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 - 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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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 - 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
Page 123 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 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
Page 125 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.
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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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 - 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
Page 127 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.
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
Page 128 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.
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
Page 129 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 - 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.
Page 130 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.
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
Page 131 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 - 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
Page 132 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.
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
Page 133 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.
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
Page 134 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.
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
Page 135 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.
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
Page 136 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.
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
Page 137 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.
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.
Page 138 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.
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
Page 139 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.
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
Page 140 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.
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
Page 141 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.
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
Page 142 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.
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
Page 143 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.
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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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 - 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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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.
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
Page 147 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.
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
Page 148 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.
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
Page 149 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.
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
Page 150 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.
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
Page 151 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.
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
Page 152 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 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
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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
Page 155 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.
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
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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 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
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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.
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
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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 500-31-0005R6
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
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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 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
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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.
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
Page 162 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 - 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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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 - 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
Page 164 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.
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
Page 165 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.
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
Page 166 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.
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
Page 167 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.
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
Page 168 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.
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
Page 169 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.
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
Page 170 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.
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
Page 171 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.
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
Page 172 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.
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
Page 173 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 - 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
Page 174 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 - 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
Page 175 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 - 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
Page 176 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 - 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
Page 177 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 - 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
Page 178 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.
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
Page 179 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.
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
Page 180 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 - 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
Page 181 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 - 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
Page 182 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.
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
Page 183 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 - 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
Page 184 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.
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
Page 185 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.
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
Page 186 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.
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#
Page 187 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.
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
Page 188 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.
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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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.
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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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.
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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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.
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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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 - 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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