A320飞机维护手册 AMM 动力装置 POWER PLANT 2(30)

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R  (19) Make sure that the harness (5) is correctly installed on the engine. 
R R  (20) Close the line blocks (35) and if installed, line block (40), and tighten the captive screws. 
R  (21) Tighten the captive bolts on the flip-lock clamps (10). 
R R R R R  (22) TORQUE the bolts (17), (22), (27), (31), (57) and (59) to between 25 and 30 lbf.in (0.28 and 0.33 m.daN). END SPIB NO. CFM02255MW1 
R  (23) Connect the ground wires to the ground studs with the nuts (60), the lockwashers (65) and the washers (70). (Ref. Fig. 404/TASK 71-51-43-991-303)
 -------------------------------------------------------------------------------
WIRE  GROUND
 -------------------------------------------------------------------------------
GD9965DC/1 GD9965DC/2 GD9966DC/1 GD9966DC/2 GD9967DC/1 GD9968DC/1 GD9969DC/1 GD9970DC/1 GD9970DC/2  GD9965DCGD9965DCGD9966DCGD9966DCGD9967DCGD9968DCGD9969DCGD9970DCGD9970DC 
R  (24) Connect the electrical connectors 4000XU-A, 4000XU-B and 4000XU-C to the integrated drive generator (IDG).
 NOTE : The wire harness for connectors 4000XU-A and 4000XU-B may____ touch as shown on
 (Ref. Fig. 405/TASK 71-51-43-991-304) 
R  (25) Connect the electrical connector 4000DN-A to the anti-ice valve.

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R (26) Connect the electrical connector 4001VC-A to the interphone jack disconnect on the aft bulkhead of the inlet cowl. R (27) Make sure that the harness (5) is correctly installed on the engine. R (28) Examine the harness installation and make sure that all flip-lock clamps and line blocks are installed correctly. Subtask 71-51-43-865-067
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 5DA1, 5DA2, 5DA3, 1DB1, 1DB2, 4DG1, 4DG2, 1JH, 3801GX, 3802GX, 3803GX, 7TU, 2RK, 4RK FOR 1000EM1 2KS1, 4KS1, 2JH1, 3JH1, 1WE1, 2WE1, 7WD1, 8WD1, 2XU1 FOR 1000EM2 2KS2, 4KS2, 2JH2, 3JH2, 1WE2, 2WE2, 7WD2, 8WD2, 2XU2
 Subtask 71-51-43-861-052
 C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002) Subtask 71-51-43-860-060
 D. Aircraft Maintenance Configuration
 (1) Do the EIS start procedure (for the lower display of the ECAM system only). (Ref. TASK 31-60-00-860-001).

 (2) Pressurize the aircraft pneumatic system with a ground power cast or through the APU.

 Subtask 71-51-43-710-051
 E. Do this test
 (1) Start the engine. Let it become stable at the idle speed. (Ref. TASK 71-00-00-710-003).

 (2) On the ECAM control panel, get the ELEC page. On the lower display unit of the ECAM system:

 (a) make sure that the voltage and frequency are correct.

 (3) Stop the engine. (Ref. TASK 71-00-00-710-028).

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________ Subtask 71-51-43-860-061
 A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-002) Subtask 71-51-43-862-052
 B. De-energize the aircraft circuits (Ref. TASK 24-41-00-862-002) Subtask 71-51-43-869-052
 C. Depressurize the pneumatic system. Subtask 71-51-43-410-055
 D. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 (3) Remove the access platform(s).

 (4) Remove the warning notice(s).

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 TASK 71-51-43-000-046
 Removal of the ECU (Channel A) Harness (4211KS)

 1. Reason for the Job

__________________
 Self Explanatory

 2. Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific protective covers
 No specific warning notice
 No specific access platform 1 m (3 ft. 3 in.)
　
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