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avr. 24, 2015 C-GFKA

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C-GFKA Detailed View

Registration C-GFKA Date avr. 24, 2015

Make Pilatus TTAF 17365.3

Model PC-12/45 Serial No. 182

Actions

Acc - Accomplishment Cal - Calibration

Cap - Capacity test Che - Check

Cle - Clean & flow check Cle - Clean/ reinstall

Cle - Cleaning Cor - Correlation check

Fun - Functional check Hyd - Hydrostatic test

Ins - Inspection Ins - Inspection/ cleaning

Lea - Leak check Lub - Lubrication

On - On condition Ope - Operational Check

Ove - Overhaul Rec - Recertify

reo - reoil Rep - Replacement

Ret - Retirement Rew - Reweight

Sea - Seal inspection

Cycles values

Cycle Name Value Cycle Name Value Cycle Name Value Cycle Name Value

Landings 13 570.0

Components

Component/Action Make/Model Part No. Serial No. Tracking

No. Limit Perf.

Time at

Inst. Due TTSC TTSN Rem.

AIR CONDITIONER ITEMS: / /

-- Cold air unit / reo / 500.0H

17197.2H

17697.2H

168.1H

331.9H

-- Duct overtemperature sensor / Fun

/ 60.0M

août 17, 12

août 17, 17

32.2M

27.8M

-- Heat exchanger matrix / Ins / 500.0H

17197.2H

17697.2H

168.1H

331.9H

-- Overtemperature sensor / Fun

/ 60.0M

août 17, 12

août 17, 17

32.2M

27.8M

-- Water separator condensor / Cle

/ 500.0H

17197.2H

17697.2H

168.1H

331.9H

ALTIMETRY/ AVIONICS ITEMS /

/

-- AHRS system swing check #1 & #2 / Acc

/ 17229.4H 135.9H


of 22

Components


No. Limit Perf.

Time at


24.0M août 19, 14 août 19, 16 8.2M 15.8M

-- Altimeter, second / Cal / 5934PAD-3 408981 24.0M

avr. 24, 14

avr. 24, 16

12.0M

12.0M

-- Autopilot computer / On King/ KCP 220

065-00064-0015 2061

4248.6H mai 15, 02

13116.7H 155.3M

-- Autopilot mode controller / On

King/ KCP 220

065-00086-0017 2336

9541.9H mars 3, 08

7823.4H 85.7M

-- Encoding altimeter / Cal / 066-03064-0005 3245 24.0M

avr. 24, 14

avr. 24, 16

12.0M

12.0M

-- Standby compass swing ref: 12-A-34-21-00-00A-903A-A / Che

/ 12.0M

mars 24, 15

mars 24, 16

1.0M

11.0M

-- Static system / Lea / 24.0M

mars 24, 15

mars 24, 17

1.0M

23.0M

-- Transponder system / Cor / 24.0M

avr. 24, 14

avr. 24, 16

12.0M

12.0M

CHAPTER 4- AIRWORTHINESS LIMITATIONS ITEMS /

/

-- Cabin fire extinguisher / Ret / BA51015GR-3 X-982077 120.0M

mai 30, 14

mai 30, 24

10.8M

109.2M

-- Cargo door lower lug fittings (Qty 3) / Rep Cycle Name : Landings

/ 13000.0H 17000.0C

12956.8H 9552.0C

25956.8H 26552.0C

4408.5H 4018.0C

8591.5H 12982.0C

-- Cargo door piano hinge- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Cargo door skin- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Co-pilot crew seat backrest tubes with recline system installed / Rep

/ 5000.0H

12756.0H nov. 3, 10

17756.0H

4609.3H 53.7M

390.7H

-- Engine mount frame / 571.20.12.036 085 20000.0H 0.0H 20000.0H 17365.3H 2634.7H


of 22

Components


No. Limit Perf.

Time at


assembly- PRE SB 04-009- Structural limitations 20000hrs/ 27000 cycles whichever occurs first / Acc Cycle Name : Landings

27000.0C

0.0C

27000.0C

13570.0C

13430.0C

-- Engine mounting frame- Replace all bolts, washers and nuts / Acc

/ 11000.0H

11000.1H juil. 5, 09

22000.1H

6365.2H 69.6M

4634.8H

-- Flap LH- Life limit / Ret Cycle Name : Landings

/ 557.50.12.003 085 25000.0H 30000.0C

17197.2H 13360.0C

17278.8H 13477.0C

24918.4H 29883.0C

17446.9H 13687.0C

7553.1H 16313.0C

-- Flap RH- Life limit / Ret Cycle Name : Landings

/ 557.50.12.004 086 25000.0H 30000.0C

0.0H 0.0C

25000.0H 30000.0C

17365.3H 13570.0C

7634.7H 16430.0C

-- Flight controls- Bonding leads to all flight control surfaces / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Frame 40- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Fuselage and associated structure - PRE SB 04-009- Structural limitations / Acc Cycle Name : Landings

/ 20000.0H 27000.0C

0.0H 0.0C

20000.0H 27000.0C

17365.3H 13570.0C

2634.7H 13430.0C

-- Horizontal stab trim runaway, aural warning system ref: 12-A-27-40-00-00A-903A-A / Fun

/ 3000.0H 12.0M

17365.3H mars 24, 15

20365.3H mars 24, 16

0.0H 1.0M

3000.0H 11.0M

-- Horizontal stabilizer- Life limit / Ret Cycle Name : Landings

/ 25000.0H 30000.0C

0.0H 0.0C

25000.0H 30000.0C

17365.3H 13570.0C

7634.7H 16430.0C

-- IB flap drive arms- in-situ inspection / Acc

/ 150.0H 12.0M

17339.8H janv. 30, 15

17489.8H janv. 30, 16

25.5H 2.8M

124.5H 9.2M

-- MLG Actuator / Ret Cycle Name : Landings

/ 25000.0H 30000.0C

0.0H 0.0C

25000.0H 30000.0C

17365.3H 13570.0C

7634.7H 16430.0C

-- Nitrogen accumulator / Ret Cycle Name : Landings

/ 25000.0H 30000.0C

0.0H 0.0C

25000.0H 30000.0C

17365.3H 13570.0C

7634.7H 16430.0C

-- NLG Drag link / Ret / 25000.0H 0.0H 25000.0H 17365.3H 7634.7H


of 22

Components


No. Limit Perf.

Time at


Cycle Name : Landings

30000.0C

0.0C

30000.0C

13570.0C

16430.0C

-- Passenger/ crew door piano hinge- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Passenger/ crew door skin- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- Pilot crew seat backrest tubes with recline system installed / Rep

/ 5000.0H

12756.0H nov. 3, 10

17756.0H

4609.3H 53.7M

390.7H

-- Pitch trim actuator / Ove / 978.73.14.203 449 5000.0H 60.0M

17197.2H avr. 24, 14

22197.2H avr. 24, 19

168.1H 12.0M

4831.9H 48.0M

-- Pitch trim actuator / Ret Cycle Name : Landings

/ 978.73.14.203 449 20000.0H 27000.0C

17197.2H 13360.0C

1494.6H 1176.0C

35702.6H 39184.0C

1662.7H 1386.0C

18337.3H 25614.0C

-- Pitch trim actuator attachment parts, fail safe plates and their attachment parts (IPC 12-20-00-07) / Ins

/ 10000.0H

9901.8H juin 20, 08

19901.8H

7463.5H 82.1M

2536.5H

-- SABA Flap actuator LH IB / Ove Cycle Name : Landings

/ 978.73.20.309 1792 5000.0H 7000.0C

14515.3H 10939.0C

19515.3H 17939.0C

2850.0H 2631.0C

2150.0H 4369.0C

-- SABA Flap actuator LH IB / Ret Cycle Name : Landings

/ 978.73.20.309 1792 20000.0H 27000.0C

14515.3H 10939.0C

4989.4H 3598.0C

29525.9H 34341.0C

7839.4H 6229.0C

12160.6H 20771.0C

-- SABA Flap actuator LH OB / Ove Cycle Name : Landings

/ 978.73.20.309 1731 5000.0H 7000.0C

14515.3H 10939.0C

19515.3H 17939.0C

2850.0H 2631.0C

2150.0H 4369.0C

-- SABA Flap actuator LH OB / Ret Cycle Name : Landings

/ 978.73.20.309 1731 20000.0H 27000.0C

14515.3H 10939.0C

4843.1H 4187.0C

29672.2H 33752.0C

7693.1H 6818.0C

12306.9H 20182.0C

-- SABA Flap actuator LH OB / Ove Cycle Name : Landings

/ 978.73.20.309 1731 5000.0H 7000.0C

14515.3H 10939.0C

19515.3H 17939.0C

2850.0H 2631.0C

2150.0H 4369.0C

-- SABA Flap actuator LH OB / Ret Cycle Name : Landings

/ 978.73.20.309 1731 20000.0H 27000.0C

14515.3H 10939.0C

4843.1H 4187.0C

29672.2H 33752.0C

7693.1H 6818.0C

12306.9H 20182.0C

-- SABA Flap actuator RH IB / / 978.73.20.309 1158 5000.0H 14515.3H 19515.3H 2850.0H 2150.0H


of 22

Components


No. Limit Perf.

Time at


Ove Cycle Name : Landings

7000.0C

10939.0C

17939.0C

2631.0C

4369.0C

-- SABA Flap actuator RH IB / Ret Cycle Name : Landings

/ 978.73.20.309 1158 20000.0H 27000.0C

14515.3H 10939.0C

4995.2H 4877.0C

29520.1H 33062.0C

7845.2H 7508.0C

12154.8H 19492.0C

-- SABA Flap actuator RH IB / Ove Cycle Name : Landings

/ 978.73.20.309 1158 5000.0H 7000.0C

14515.3H 10939.0C

19515.3H 17939.0C

2850.0H 2631.0C

2150.0H 4369.0C

-- SABA Flap actuator RH IB / Ret Cycle Name : Landings

/ 978.73.20.309 1158 20000.0H 27000.0C

14515.3H 10939.0C

4995.2H 4877.0C

29520.1H 33062.0C

7845.2H 7508.0C

12154.8H 19492.0C

-- SABA Flap actuator RH OB / Ove Cycle Name : Landings

/ 978.73.20.309 0759 5000.0H 7000.0C

14515.3H 10939.0C

19515.3H 17939.0C

2850.0H 2631.0C

2150.0H 4369.0C

-- SABA Flap actuator RH OB / Ret Cycle Name : Landings

/ 978.73.20.309 0759 20000.0H 27000.0C

14515.3H 10939.0C

9485.2H 13301.0C

25030.1H 24638.0C

12335.2H 15932.0C

7664.8H 11068.0C

-- SABA Flap backlash ref: 12-A-27-50-03-00A-313B-A / Ins Cycle Name : Landings

/ 1000.0H 12.0M 1300.0C

17365.3H mars 24, 15 13570.0C

18365.3H mars 24, 16 14870.0C

0.0H 1.0M 0.0C

1000.0H 11.0M 1300.0C

-- Small oxygen cylinder / Ret / 957.12.12.211 C12110238 180.0M

janv. 15, 13

janv. 15, 28

27.3M

152.7M

-- SSID Aileron / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID aileron bellcranks- Eddy current and magnetic particle / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID aileron cable segment- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID aileron control rods- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID aileron control rods- Magnetic particle / Ins

/ 12500.0H*

0.0H*

*

32500.0H*

17365.3H*

*

15134.7H*


of 22

Components


No. Limit Perf.

Time at



15000.0C* 0.0C* * 42000.0C* 13570.0C* * 28430.0C*

-- SSID aileron control system / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Aileron hinge points- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Aileron trim tab / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Antenna structure / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Antenna- Bottom fuselage skin- Eddy current / Ins Cycle Name : Landings

/ 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

28300.0H* 37000.0C*

17365.3H* 13570.0C*

* *

10934.7H* 23430.0C*

-- SSID Antenna- Upper fuselage skin- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Cargo door- Examine all structural elements / Acc Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Elevator / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Elevator control lever- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Elevator control rods- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Elevator control rods- Magnetic particle / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Elevator hinges- Eddy current / Ins

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*


of 22

Components


No. Limit Perf.

Time at



-- SSID Elevator- control system / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Emergency door / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Engine mount- Magnetic particle / Ins Cycle Name : Landings

/ 6600.0H* 8000.0C*

0.0H* 0.0C*

* *

26600.0H* 35000.0C*

17365.3H* 13570.0C*

* *

9234.7H* 21430.0C*

-- SSID Flap aft links- eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Flap bellcranks- Eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Flap cove rib fittings- Eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Flap drive arm (not removed) Eddy current / Ins Cycle Name : Landings

/ 2500.0H* 3000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Flap drive arm (removed) Eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Flap mechanism / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Flap support arm- Eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Frames 21 and 24 side frame attachments- Eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Frames 21 and 24 wing attachments- Eddy current / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*


of 22

Components


No. Limit Perf.

Time at


-- SSID Frames 41 and 43 stabilizer attachment- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Fuselage frames 10 to 16- Examine all structural elements / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Fuselage frames 16 to 36- Examine all structural elements / Acc Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Fuselage frames 36 to 43- Examine all structural elements / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Main landing gear trailing link- Eddy current inspection CMM 02099 / Acc Cycle Name : Landings

/ 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Main landing gear yoke fitting lugs- Eddy current Inspection. CMM 02099 / Acc Cycle Name : Landings

/ 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Main landing gear- Overhaul CMM 02099 Inspection kit PN 500.60.12.027 / Ove Cycle Name : Landings

/ 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Passenger/ crew door / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Rudder / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Rudder bellcranks- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Rudder cable quadrant shear spigot / Ins

/ 12500.0H*

0.0H*

*

32500.0H*

17365.3H*

*

15134.7H*


of 22

Components


No. Limit Perf.

Time at



15000.0C* 0.0C* * 42000.0C* 13570.0C* * 28430.0C*

-- SSID Rudder control system / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Rudder hinges- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Rudder trim tab / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Upper flange carry through frame 21 and 24 / Ins Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- SSID Upper longerons frame 10- Eddy current inspection AMM ref. 12-A-53-10-06-1A-353A-A / Acc Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Vertical stabilizer / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Vertical stabilizer main and rear spar attachment to fuselage- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Vertical stabilizer main attachment to horizontal stabilizer- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Vertical stabilizer pitch trim actuator fitting and attachment- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Windshield LH and RH and cockpit side windows / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- SSID Wing main and rear spar to fuselage attachment-

/ 10000.0H*

0.0H*

*

30000.0H*

17365.3H*

*

12634.7H*


of 22

Components


No. Limit Perf.

Time at


Eddy current / Ins Cycle Name : Landings

12000.0C* 0.0C* * 39000.0C* 13570.0C* * 25430.0C*

-- SSID Wing main spar fastener holes rib 1 thru rib 6- Eddy current / Ins Cycle Name : Landings

/ 3300.0H* 4000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Wing main spar fastener holes rib 2 thru rib 3- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Wing main spar fastener holes strap rib 6- Eddy current / Ins Cycle Name : Landings

/ 3300.0H* 4000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Wing rear spar at rib 8 flap arm attachment- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- SSID Wing- Examine all structural elements rib 1 to rib 20 / Acc Cycle Name : Landings

/ 10000.0H* 12000.0C*

0.0H* 0.0C*

* *

30000.0H* 39000.0C*

17365.3H* 13570.0C*

* *

12634.7H* 25430.0C*

-- Tail horizontal stabilizer- PRE SB 04-009 - Structural limitations / Acc Cycle Name : Landings

/ 20000.0H 27000.0C

0.0H 0.0C

20000.0H 27000.0C

17365.3H 13570.0C

2634.7H 13430.0C

-- Tail vertical stabilizer- PRE SB 04-009- Structural limitations / Acc Cycle Name : Landings

/ 20000.0H 27000.0C

0.0H 0.0C

20000.0H 27000.0C

17365.3H 13570.0C

2634.7H 13430.0C

-- Vertical stabilizer forward attachment to frame 40- Eddy current / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Wing assy LH- PRE SB 04-009- Structural limitations 20000hrs/ 27000 cycles, whichever occurs first / Acc Cycle Name : Landings

/ 20000.0H 27000.0C

0.0H 0.0C

20000.0H 27000.0C

17365.3H 13570.0C

2634.7H 13430.0C


of 22

Components


No. Limit Perf.

Time at


-- Wing assy RH- PRE SB 04-009- Structural limitations 20000hrs/ 27000 cycles, whichever occurs first / Cycle Name : Landings

/ 20000.0H 27000.0C

0.0H 0.0C

20000.0H 27000.0C

17365.3H 13570.0C

2634.7H 13430.0C

-- Wing main spar fastener holes strap rib 6- Eddy current inspection, NO cracks permitted / Acc Cycle Name : Landings

/ 16000.0H 22500.0C

15989.6H févr. 17, 13 12273.0C

31989.6H 34773.0C

1375.7H 26.2M 1297.0C

14624.3H 21203.0C

-- Wing skin around drain holes- Eddy current / Ins Cycle Name : Landings

/ 2500.0H* 3000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- Wing tips / Ins Cycle Name : Landings

/ 12500.0H* 15000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Wing to fuselage attachments- Requires 10yr/ 11000 hr inspection required on attachment fittings / Acc

/ 11000.0H 120.0M

8838.2H juin 13, 07

19838.2H juin 13, 17

8527.1H 94.4M

2472.9H 25.6M

Engine / Ove Cycle Name : Landings

Pratt & Whitne y Canada/PT6A-67B

PT6A-67B PCE-PR0036 3500.0H*

15618.3H* nov. 10, 12 11967.0C

*

19597.6H*

1747.0H* 29.5M 1603.0C

*

2232.3H*

-- AGB internal scavenge pump inlet screen / Ins

/ 1000.0H

16587.6H juil. 5, 13

17587.6H

777.7H 21.6M

222.3H

-- Borescope / Ins / 400.0H

17197.2H

17597.2H

168.1H

231.9H

-- Compressor 1st stage / Ins / 1750.0H*

15618.3H* nov. 9, 12

*

17568.0H*

1747.0H* 29.5M

*

202.7H*

-- Compressor bleed valve / Ove

/ 3123532-1 24A698 3500.0H*

15618.3H* nov. 10, 12

*

19699.3H*

1747.0H* 29.5M

*

2334.0H*

-- Compressor rotor shaft / Ret Cycle Name : Landings

/ 3043063 37B038 24000.0C

11967.0C

11324.0C

24643.0C

12927.0C

11073.0C

-- CT disc / Ret Cycle Name : Landings

/ 3053740-01 A000C6LT 8000.0C

15618.3H nov. 10, 12 11967.0C

4819.0C

15148.0C

1747.0H 29.5M 6422.0C

1578.0C

-- Engine driven fuel pump (High pressure) / Ove

/ 825601-5 3541 3500.0H* 15618.3H* * 19699.3H* 1747.0H* * 2334.0H*


of 22

Components


No. Limit Perf.

Time at


nov. 10, 12 29.5M

-- Engine driven low pressure fuel pump ref: 12-A-28-20-03-00A-920A-A / Ove

/ 968.84.51.108 B4107 3500.0H

17365.3H mars 24, 15

20865.3H

0.0H 1.0M

3500.0H

-- Engine oil filter / Rep / 1000.0H

16587.6H juil. 5, 13

17587.6H

777.7H 21.6M

222.3H

-- Engine shock mount assembly- Lower LH / Ove

/ 93880-23 1413 3500.0H

15618.3H nov. 10, 12

19118.3H

1747.0H 29.5M

1753.0H

-- Engine shock mount assembly- Lower RH / Ove

/ 93880-23 R0778 3500.0H

15618.3H nov. 10, 12

19118.3H

1747.0H 29.5M

1753.0H

-- Engine shock mount assembly- Upper center / Ove

/ 93880-23 R0779 3500.0H

15618.3H nov. 10, 12

19118.3H

1747.0H 29.5M

1753.0H

-- Engine shock mount assembly- Upper LH / Ove

/ 93880-23 R0777 3500.0H

15618.3H nov. 10, 12

19118.3H

1747.0H 29.5M

1753.0H

-- Engine shock mount assembly- Upper RH / Ove

/ 93880-23 R0780 3500.0H

15618.3H nov. 10, 12

19118.3H

1747.0H 29.5M

1753.0H

-- Flow divider / Ove / 26130-2 1505 3500.0H

15770.5H déc. 9, 12

19270.5H

1594.8H 28.5M

1905.2H

-- Fuel control unit (FCU) / Ove

/ 8063-044 2336840 3500.0H*

15779.4H* déc. 12, 12

*

19459.0H*

1585.9H* 28.4M

*

2093.7H*

-- Fuel nozzles / Cle / 400.0H

17197.2H

17597.2H

168.1H

231.9H

-- Fuel pump inlet screen / Cle / 600.0H

17354.2H févr. 22, 15

17954.2H

11.1H 2.1M

588.9H

-- Generator/ battery 1 and 2 ground points- examine the corrosion protective layer / Acc

/ 24.0M

avr. 24, 14

avr. 24, 16

12.0M

12.0M

-- Hot section inspection / Acc / 1750.0H

17365.3H mars 24, 15

19115.3H

0.0H 1.0M

1750.0H

-- Ignition exciter box / Ove / 10-381550-4E NN98167388 3500.0H*

15845.6H* janv. 5, 13

*

19843.9H*

1519.7H* 27.6M

*

2478.6H*


of 22

Components


No. Limit Perf.

Time at


-- Impeller, centrifugal / Ret Cycle Name : Landings

/ 3036898 8F006 24000.0C

11967.0C

11324.0C

24643.0C

12927.0C

11073.0C

-- Oil cooler assembly / Ove / 968.32.14.102 T0157 3500.0H*

14573.4H* févr. 18, 12

*

18866.2H*

2791.9H* 38.2M

*

1500.9H*

-- Oil to fuel heater / Ove / 10585J WA8630 3500.0H*

15618.3H* nov. 10, 12

*

19699.3H*

1747.0H* 29.5M

*

2334.0H*

-- P3 engine air filter / Rep / 1000.0H

16587.6H juil. 5, 13

17587.6H

777.7H 21.6M

222.3H

-- P3 engine air filter / Cle / 150.0H*

17354.2H* févr. 22, 15

*

17497.2H*

11.1H* 2.1M

*

131.9H*

-- Propeller governor / Ove / 8210-137H 11968212 3500.0H*

15618.3H* nov. 10, 12

*

19699.3H*

1747.0H* 29.5M

*

2334.0H*

-- Propeller overspeed governor / Ove

/ 210949 14261060 6500.0H

15618.3H nov. 10, 12

22118.3H

1747.0H 29.5M

4753.0H

-- PT disc 1st stage / Ret Cycle Name : Landings

/ 3037312 25B474 15000.0C

11967.0C

11228.0C

15739.0C

12831.0C

2169.0C

-- PT disc 2nd stage / Ret Cycle Name : Landings

/ 3037313 39B614 15000.0C

11967.0C

11228.0C

15739.0C

12831.0C

2169.0C

-- Reduction gearbox chip detector and accessory gearbox chip detector if post SB 79-005 ref: 12-A-79-30-01-00A-903A-A / Ins

/ 600.0H 12.0M

17365.3H mars 24, 15

17965.3H mars 24, 16

0.0H 1.0M

600.0H 11.0M

-- Rotor, compressor 1st stage / Ret Cycle Name : Landings

/ 3039001 TXA1A5955 24000.0C

11967.0C

6387.0C

29580.0C

7990.0C

16010.0C

-- Rotor, compressor 2nd stage / Ret Cycle Name : Landings

/ 3040952 37B388 24000.0C

11967.0C

11324.0C

24643.0C

12927.0C

11073.0C

-- Rotor, compressor 3rd stage / Ret Cycle Name : Landings

/ 3040933 39B225 24000.0C

11967.0C

11324.0C

24643.0C

12927.0C

11073.0C

-- Rotor, compressor 4th stage / Ret

/ 3040944 35B845


of 22

Components


No. Limit Perf.

Time at



24000.0C 11967.0C 11324.0C 24643.0C 12927.0C 11073.0C

-- Second generator brushes / Ins

/ 200.0H

17354.2H févr. 22, 15

17554.2H

11.1H 2.1M

188.9H

-- Second generator drive assembly aft bearing / Rep

/ 3000.0H

15866.3H janv. 13, 13

18866.3H

1499.0H 27.4M

1501.0H

-- Second generator drive assembly housing / Ins

/ 1000.0H

17197.2H avr. 25, 14

18197.2H

168.1H 12.0M

831.9H

-- Second generator- Post SB 24-010 / On

/ 524.32.12.158 100184

13232.6H mars 28, 11

4132.7H 48.9M

-- Spark igniters / Ins / 150.0H* 12.0M

17354.2H* févr. 22, 15

*

17497.2H* févr. 22, 16

11.1H* 2.1M

*

131.9H* 9.9M

-- Starter generator / Ove / 23085-024 98106 1000.0H

16829.6H sept. 7, 13

17829.6H

535.7H 19.6M

464.3H

-- Starter generator brushes / Ins

/ 200.0H

17354.2H févr. 22, 15

17554.2H

11.1H 2.1M

188.9H

-- Torque limiter / Ove / 3244882-2 C50076 3500.0H*

15618.3H* nov. 10, 12

*

19699.3H*

1747.0H* 29.5M

*

2334.0H*

LANDING GEARS ITEMS / /

-- Hydraulic power pack / Ret Cycle Name : Landings

/ 960.30.01.154 G0130591 20000.0H 27000.0C

17197.2H avr. 24, 14 13360.0C

9824.2H 11987.0C

27373.0H 28373.0C

9992.3H 12.0M 12197.0C

10007.7H 14803.0C

-- L/H main wheel bearings ref: Use MOBIL SHC100 grease. (not mobilith SHC100 grease- ref. Pilatus service letter 110) 1 year or every tire change 12-A-12-20-06-00A-902A-A / Lub

/ 12.0M

mars 24, 15

mars 24, 16

1.0M

11.0M

-- Landing gear compartments- / Ins Cycle Name : Landings

/ 6000.0H 72.0M

16393.6H mai 24, 13

22393.6H mai 24, 19

971.7H 23.0M

5028.3H 49.0M

-- LH Cleveland brake assembly / On

/ 030-24400 1554 14704.2H 2661.1H


of 22

Components


No. Limit Perf.

Time at


mars 20, 12 37.1M

-- LH Cleveland wheel assembly / On

/ 040-42400 2043/2020

16930.8H oct. 3, 13

434.5H 18.7M

-- LH IB Cleveland wheel half / On

/ 151-19901 2020

16930.8H oct. 3, 13

434.5H 18.7M

-- LH MLG Assy / Ove Cycle Name : Landings

/ 532.10.12.043 IL-094 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- LH OB Cleveland wheel half / On

/ 152-19901 2043

16930.8H oct. 3, 13

434.5H 18.7M

-- Main landing gear axles and bushings wear inspection ref: 12-A-32-10-00-00A-313A-A / Acc

/ 2000.0H 12.0M

17365.3H mars 24, 15

19365.3H mars 24, 16

0.0H 1.0M

2000.0H 11.0M

-- NLG Steering mechanism / Ins Cycle Name : Landings

/ 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

32500.0H* 42000.0C*

17365.3H* 13570.0C*

* *

15134.7H* 28430.0C*

-- Nose landing gear / Ove Cycle Name : Landings

/ 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- Nose wheel assembly / On Cycle Name : Landings

/ 959.56.02.301 1072

16930.8H oct. 3, 13 13136.0C

434.5H 18.7M 434.0C

-- Nose wheel bearings ref: Use MOBIL SHC100 grease. (not mobilith SHC100 grease- ref. Pilatus service letter 110) 1 year or every tire change 12-A-12-20-06-00A-902A-A / Lub

/ 12.0M

mars 24, 15

mars 24, 16

1.0M

11.0M

-- R/H main wheel bearings ref: Use MOBIL SHC100 grease. (not mobilith SHC100 grease- ref. Pilatus service letter 110) 1 year or every tire change 12-A-12-20-06-00A-902A-A / Lub

/ 12.0M

mars 24, 15

mars 24, 16

1.0M

11.0M

-- RH Cleveland brake assembly / On

/ 030-24400 1327

17161.3H déc. 3, 13

204.0H 16.7M

-- RH Cleveland wheel assembly / On

/ 040-42400 1550/1553 16553.4H 811.9H


of 22

Components


No. Limit Perf.

Time at


juin 28, 13 21.9M

-- RH IB Cleveland wheel half / On

/ 151-19901 1553

16553.4H juin 28, 13

811.9H 21.9M

-- RH MLG assy / Ove Cycle Name : Landings

/ 532.10.12.044 IL-094 8300.0H* 10000.0C*

0.0H* 0.0C*

* *

25000.0H* 30000.0C*

17365.3H* 13570.0C*

* *

7634.7H* 16430.0C*

-- RH OB Cleveland wheel half / On

/ 152-19901 1550

16553.4H juin 28, 13

811.9H 21.9M

MISC INSPECTION ITEMS: / /

-- Apply a light layer of the PTFE teflon spray OKS 571 to the cargo door switch roller and surface ref: 12-A-52-70-00-00A-903A-A / Acc

/ 12.0M

17365.3H mars 24, 15

mars 24, 16

0.0H 1.0M

11.0M

-- Cabin altitude switch ref: 12-A-21-30-08-00A-903A-A / Fun

/ 60.0M

mars 24, 15

mars 24, 20

1.0M

59.0M

-- Cabin differential pressure switch ref: 12-A-21-30-08-00A-903A-A / Fun

/ 60.0M

mars 24, 15

mars 24, 20

1.0M

59.0M

-- Cargo door / Ins / 6000.0H 72.0M

12000.1H avr. 16, 10

18000.1H avr. 16, 16

5365.2H 60.3M

634.8H 11.7M

-- Cockpit side windows- 11,000 hrs or 10 year inspection/ check of attachment lugs / Acc

/ 11000.0H 120.0M

10425.1H déc. 19, 08

21425.1H déc. 19, 18

6940.2H 76.2M

4059.8H 43.8M

-- De-icers (airfoil) agemaster application ref: 12-A-30-10-00-00A-313A-A / Acc

/ 6.0M

mars 24, 15

sept. 24, 15

1.0M

5.0M

-- De-icers (airfoil) require ICE-X application / Acc

/ 150.0H

17365.3H mars 24, 15

17515.3H

0.0H 1.0M

150.0H

-- Door frames and emergency exits frame / Ins

/ 6000.0H 72.0M

11691.6H janv. 8, 10

17691.6H janv. 8, 16

5673.7H 63.5M

326.3H 8.5M

-- Elevator cable tension- Check on new aircraft or after replacement of any elevator control system cable / Acc

/

17197.2H avr. 28, 14

168.1H 11.9M

-- Engine and stick pusher / 500.0H 17365.3H 17865.3H 0.0H 500.0H


of 22

Components


No. Limit Perf.

Time at


torque transducers- remove cannon plug, clean connections and reinstall ref: 12-A-71-00-03-00A-250A-A / Acc

12.0M mars 24, 15 mars 24, 16 1.0M 11.0M

-- Engine torque limiter test ref: 12-A-71-00-00-00A-903A-A / Acc

/ 500.0H 12.0M

17365.3H mars 24, 15

17865.3H mars 24, 16

0.0H 1.0M

500.0H 11.0M

-- External corrosion preventative 12 month inspection and application ref: 12-A-20-40-00-00A-901A-A / Acc

/ 12.0M

mars 24, 15

mars 24, 16

1.0M

11.0M

-- Flap flex shaft LH IB remove, clean, lubricate and reinstall (vickers flex shafts only) / Acc

/ 2000.0H

17365.3H mars 24, 15

19365.3H

0.0H 1.0M

2000.0H

-- Flap flex shaft LH OB remove, clean, lubricate and reinstall (vickers flex shafts only) / Acc

/ 2000.0H

17365.3H mars 24, 15

19365.3H

0.0H 1.0M

2000.0H

-- Flap flex shaft RH IB remove, clean, lubricate and reinstall (vickers flex shafts only) / Acc

/ 2000.0H

17365.3H mars 24, 15

19365.3H

0.0H 1.0M

2000.0H

-- Flap flex shaft RH OB remove, clean, lubricate and reinstall (vickers flex shafts only) / Acc

/ 2000.0H

17365.3H mars 24, 15

19365.3H

0.0H 1.0M

2000.0H

-- Flap PDU / Ove Cycle Name : Landings

/ 978.73.20.003 1271 10000.0H 13500.0C

17197.2H 13360.0C

27197.2H 26860.0C

168.1H 210.0C

9831.9H 13290.0C

-- Flap screw actuators, lubricated "BLACK" SABA actuators, Max 5 pumps grease / Acc

/ 150.0H* 12.0M

17354.2H* févr. 22, 15

*

17497.2H* févr. 22, 16

11.1H* 2.1M

*

131.9H* 9.9M

-- Flight control cables- including auto pilot & stick pusher cables / Ins

/ 2000.0H 60.0M

15866.3H janv. 11, 13

17866.3H janv. 11, 18

1499.0H 27.4M

501.0H 32.6M

-- Front pressure bulkhead / Ins

/ 6000.0H 72.0M

12000.1H avr. 16, 10

18000.1H avr. 16, 16

5365.2H 60.3M

634.8H 11.7M

-- Fuel cross vent and outward check valve ref: 12-A-28-10-01-00A-903A-A / Ope

/ 1000.0H

17365.3H mars 24, 15

18365.3H

0.0H 1.0M

1000.0H

-- Fuel low level warning system / Fun

/ 1000.0H 17197.2H 18197.2H 168.1H 831.9H


of 22

Components


No. Limit Perf.

Time at


48.0M avr. 24, 14 avr. 24, 18 12.0M 36.0M

-- Fuselage internal bottom surface / Ins

/ 6000.0H 72.0M

11691.6H janv. 8, 10

17691.6H janv. 8, 16

5673.7H 63.5M

326.3H 8.5M

-- Garming GPS 430/530- Ref. MM supplement no 07311M- Inspect the cooling air fan / Ins

/ 150.0H*

17354.2H* févr. 22, 15

*

17497.2H*

11.1H* 2.1M

*

131.9H*

-- Horizontal stabilizer / Ins Cycle Name : Landings

/ 6000.0H 72.0M

16393.6H mai 25, 13

22393.6H mai 25, 19

971.7H 23.0M

5028.3H 49.0M

-- Internal corrosion preventative 12 month inspection and application ref: 12-A-20-40-00-00A-901A-A / Acc

/ 12.0M

mars 24, 15

mars 24, 16

1.0M

11.0M

-- Nicad (#1) battery deep cycle / Acc

/ 976.17.31.302 9902918 400.0H 6.0M

17306.3H déc. 22, 14

17706.3H juin 22, 15

59.0H 4.1M

341.0H 1.9M

-- Nicad battery / Cap / 6.0M

févr. 22, 15

août 22, 15

2.1M

3.9M

-- Passenger O2 masks / Ins / 36.0M

oct. 3, 13

oct. 3, 16

18.7M

17.3M

-- Passenger/ crew door 6 yr/ 6000hrs inspection with trim removed / Acc

/ 6000.0H 72.0M

12018.9H avr. 23, 10

18018.9H avr. 23, 16

5346.4H 60.0M

653.6H 12.0M

-- Pressurization safety & outflow valve / Cle

/ 3000.0H 24.0M

17197.2H avr. 25, 14

20197.2H avr. 25, 16

168.1H 12.0M

2831.9H 12.0M

-- Pressurization system test / Acc

/ 3000.0H 24.0M

17197.2H avr. 25, 14

20197.2H avr. 25, 16

168.1H 12.0M

2831.9H 12.0M

-- Rear pressure bulkhead inspection with trim removed / Acc

/ 6000.0H 72.0M

16393.6H mai 25, 13

22393.6H mai 25, 19

971.7H 23.0M

5028.3H 49.0M

-- Rudder cable tension- Check on new aircraft or after replacement of any elevator control system cable / Acc

/

17197.2H avr. 28, 14

168.1H 11.9M

-- Servo mount - "PITCH" clutch ref: 12-A-22-10-00-00A-313A-A / Che

/ 1000.0H 12.0M

17365.3H mars 24, 15

18365.3H mars 24, 16

0.0H 1.0M

1000.0H 11.0M


of 22

Components


No. Limit Perf.

Time at


-- Servo mount- "ROLL" clutch ref: 12-A-22-10-00-00A-313A-A / Che

/ 1000.0H 12.0M

17365.3H mars 24, 15

18365.3H mars 24, 16

0.0H 1.0M

1000.0H 11.0M

-- Servo mount- "YAW" clutch ref: 12-A-22-10-00-00A-313A-A / Che

/ 1000.0H 12.0M

17365.3H mars 24, 15

18365.3H mars 24, 16

0.0H 1.0M

1000.0H 11.0M

-- Small oxygen cylinder / Hyd / 60.0M

janv. 17, 13

janv. 17, 18

27.2M

32.8M

-- Structure around windows / Ins

/ 6000.0H 72.0M

11691.6H janv. 8, 10

17691.6H janv. 8, 16

5673.7H 63.5M

326.3H 8.5M

-- Vertical stabilizer internal surfaces / Ins

/ 6000.0H 72.0M

16393.6H mai 24, 13

22393.6H mai 24, 19

971.7H 23.0M

5028.3H 49.0M

-- Wing internal surfaces & flap compartment / Ins

/ 6000.0H 72.0M

16393.6H mai 25, 13

22393.6H mai 25, 19

971.7H 23.0M

5028.3H 49.0M

MISC ITEMS / /

-- Cabin fire extinguisher / Rew

/ 12.0M

oct. 31, 14

oct. 31, 15

5.8M

6.2M

-- ELT / Rec / 453-5068 6043 12.0M*

oct. 21, 14 *

*

oct. 31, 15 *

6.1M*

*

6.2M*

-- ELT battery / Rep / 60.0M

oct. 25, 13

oct. 25, 18

18.0M

42.0M

-- First aid kit / Sea / 6.0M

févr. 22, 15

août 22, 15

2.1M

3.9M

-- First aid kit contents / Ins / 12.0M

nov. 21, 14

nov. 21, 15

5.1M

6.9M

-- Survival equipment / Sea / 6.0M*

oct. 1, 14 *

*

avr. 30, 15 *

6.8M*

*

0.2M*

-- Survival equipment contents / Ins

/ 12.0M

sept. 1, 14

sept. 1, 15

7.8M

4.2M

-- Survival equipment- rations / Rep

/


of 22

Components


No. Limit Perf.

Time at


60.0M* * * juil. 22, 16 * * * 14.9M*

ON CONDITION ITEMS: / /

-- Flap flex shaft LH IB / On / 945.02.02.201 BWEB172

1450.8H sept. 4, 99

15914.5H 187.7M

-- Flap flex shaft LH OB / On / 945.02.02.202 BWEB101

1450.8H sept. 4, 99

15914.5H 187.7M

-- Flap flex shaft RH IB / On / 945.02.02.201 BWEB198

1450.8H sept. 4, 99

15914.5H 187.7M

-- Flap flex shaft RH OB / On / 945.02.02.202 BWEB254

1450.8H sept. 4, 99

15914.5H 187.7M

-- Nose landing gear shimmy dampener / On

/ 532.20.12.215 AM112

17365.3H mars 24, 15

0.0H 1.0M

Propeller / Ove Hartzell/ HC-E4A-3D

HC-E4A-3D HJ-764 4000.0H 120.0M

14172.0H janv. 24, 12

18172.0H janv. 24, 22

3193.3H 39.0M

806.7H 81.0M

-- Propeller feathering microswitches / Fun

/ 3000.0H 12.0M

17365.3H mars 24, 15

20365.3H mars 24, 16

0.0H 1.0M

3000.0H 11.0M

-- Propeller lubrication. Max 1 ounce grease to each blade (6 pumps) equal amounts to each blade / Acc

/ 400.0H 12.0M

17365.3H mars 24, 15

17765.3H mars 24, 16

0.0H 1.0M

400.0H 11.0M

SEATS ITEMS / /

-- Copilot- seat belts / Ove / 5PC41000-504 176 144.0M

mai 26, 09

mai 26, 21

70.9M

73.1M

-- Passenger seat- seat belts / Ove

/ 959.30.01.602 10038 144.0M

mai 30, 14

mai 30, 26

10.8M

133.2M


/ 403008 12520 144.0M

sept. 30, 10

sept. 30, 22

54.8M

89.2M


/ 403008 12524 144.0M

sept. 30, 10

sept. 30, 22

54.8M

89.2M


of 22

Components


No. Limit Perf.

Time at



/ 403008 12522 144.0M

sept. 30, 10

sept. 30, 22

54.8M

89.2M


/ 959.30.01.615 13706 144.0M

mai 30, 14

mai 30, 26

10.8M

133.2M


/ 959.30.01.616 19200 144.0M

mai 30, 14

mai 30, 26

10.8M

133.2M

-- Pilot seat- seat belts / Ove / 5PC41000-503 177 144.0M

mai 26, 09

mai 26, 21

70.9M

73.1M

" * " indicates that a Manual Next Due is set./(p)

Indicates that component is affected by penalty factor.

Recurring AD's

AD No. Description Type Limit Perf. Due TTSC Rem.

" * " indicates that a Manual Next Due is set.

Inspections

Inspection Limit Perf. Due TTSC Rem. 100 hour inspection @ 150 hours interval 150.0H*

17354.2H* févr. 22, 15

17497.2H*

11.1H* 2.1M

131.9H*

Annual inspection 12.0M*

17365.3H mars 24, 15 *

mars 30, 16 *

0.0H 1.0M*

11.2M*

" * " indicates that a Manual Next Due is set.

Meters

Meter Action Limit Perf. Due TTSC TTSN Rem. VCS VCS check 500.0H 839.1H

oct. 1, 10 1339.1H 191.9H

54.8M 308.1H

This report has been prepared by:

actions c-gfka detailed view - aso · c-gfka detailed view registration c-gfka date avr. 24, ......

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