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时间:2011-03-22 06:52来源:蓝天飞行翻译 作者:admin
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 (8)
 TORQUE the screws (3) to between 0.35 and 0.45 m.daN (30.97 and 39.82 lbf.in).

 (9)
 Install the security plate (9) with the screws (8).


 (10)
 TORQUE the screws (8) to between 0.05 and 0.068 m.daN (4.42 and 6.01 lbf.in).

 (11)
 Safety the screws (8) with the lockwire MISCELLANEOUS (Material No. 19-010).

 (12)
 Put the new O-ring (6) with a thin layer of FUELS (Material No. 01-001) on the drain plug (7).

 (13)
 Install the drain plug (7) in the APU fuel pump (1).

 (14)
 TORQUE the drain plug (7) to between 0.97 and 1.2 m.daN (85.84 and

 106.19 lbf.in).

 (15)
 Remove the blanking caps from the electrical connectors.

 (16)
 Make sure that the electrical connectors are clean and in the correct condition.


 (17) Connect the electrical connector (2) to the APU fuel pump (1).
 Subtask 28-22-51-420-053

 B. Installation of the APU Fuel Pump (4QC) NOTE : This installation procedure is applicable for the APU fuel pump
____ with R P/N C12CB0011/C12CB0012/C12CB0013.
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Do an inspection of the component interface and/or the adjacent area.


 1EFF : ALL 1 28-22-51Page 412 1 1 Feb 01/05 1 1 1CES 1


 (3)
 Install the new packing (7) and the new packing (8) with a thin layer of FUELS (Material No. 01-001) to the APU fuel pump (1).

 (4)
 Put the APU fuel pump (1) in position.

 (5)
 Carefully push the APU fuel pump (1) into the canister (6) with the release slot in line with the security blockscrew (5).

 (6)
 Turn the APU fuel pump (1) clockwise until the pump is in the correct position.

 (7)
 Attach the APU fuel pump (1) with the screws (10) to the canister (6).

 (8)
 TORQUE the screws (10) to between 0.35 and 0.45 m.daN (30.97 and

 39.82 lbf.in).

 (9)
 Put the new packing (4) with a thin layer of FUELS (Material No. 01-001) on the drain plug (3).


 (10)
 Install the drain plug (3) in the APU fuel pump (1).

 (11)
 TORQUE the drain plug (3) to between 0.49 and 0.6 m.daN (43.36 and

 53.09 lbf.in).

 (12)
 Remove the blanking caps from the electrical connectors.

 (13)
 Make sure that the electrical connectors are clean and in the correct condition.


 (14) Connect the electrical connector (2) to the APU fuel pump (1).
 Subtask 28-22-51-865-055

 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD, 1QC, 2QC, 3QC.
 Subtask 28-22-51-710-051
 D. Test R (1) Do the leak test of the APU fuel line (Ref. TASK 28-22-00-790-002). R (2) Examine the APU fuel pump connections for leaks during the test.
 NOTE : Leaks are not permitted.
____
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 5. Close-up
________ Subtask 28-22-51-410-052
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the LH MLG door (Ref. TASK 32-12-00-410-001).

 (3)
 Remove the access platform(s).

 (4)
 Remove the warning notice(s).


 1EFF : ALL 1 28-22-51Page 414 1 1 Feb 01/03R 1 1 1CES 1


 CANISTER - APU FUEL PUMP (9QM) - REMOVAL/INSTALLATION
_____________________________________________________
 TASK 28-22-52-000-001
 Removal of the APU Fuel-Pump Canister (9QM)
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking plugs
 No specific container
 No specific access platform 1.65 m (5 ft. 5 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 
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