A320飞机维护手册 AMM DOORS 舱门6(151)

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 (5) Install the new cotter pins (9).
 (6) Connect the bonding leads (7).
 (7) Put the washer (6), then the actuator (5) in position.
 (8) Apply COMMON GREASE (Material No. 04-004) to the rod pin of the door.
 (9) Install the washer (4) and the nut (3) and tighten it.
 (10) Install the cotter pin (2).
 Subtask 52-41-14-220-050 
R R  B. Check and Adjustment of the Out-of-flush Dimension Between the Door (21) and the Fuselage (Ref. Fig. 402/TASK 52-41-14-991-003) 
R R R  (1) Keep the door against the stop and measure the out-of-flush dimension J1 between the door (21) and the fuselage. The out-of-flush dimension J1 must be 0 -0.8 +0.8 mm (0.0000 -0.0314 +0.0314 in.). 
R  (2) If the out-of-flush dimension J1 is not in the tolerances:
 (a) Open the door (21).
 (b) Remove the two self-locking nuts (22), the two screws (23) and the washers (24).
 (c) Put a new set of washers (24), and install the two screws (23) and the two self-locking nuts (22).

 

 (d)
 Close the door and make sure that the clearance J2 is 0.2 mm (0.0078 in.).

 (e)
 TORQUE the two self-locking nuts (22) to between 0.35 and 0.45 daN (0.78 and 1.01 lbf).

 (f) Close the door (21).
 Subtask 52-41-14-220-053

 C. Check and Adjustment of the Clearance between the Door and the Feeders (Ref. Fig. 403/TASK 52-41-14-991-005)
 (1)
 Open the door (17).

 (2)
 Make sure that the clearance J3 between the door (17) and the feeders

 (18) is 20 mm (0.7874 in.) minimum.

 (3)
 If the clearance J3 is not in the tolerance:

 (a) Loosen the nut (15).
 (b) Lower the eccentric nut (16) and make sure that the clearance J3 R is 20 mm (0.7874 in.) minimum.
 (c) Torque the nut (15) to between 0.62 and 0.75 daN (1.39 and 1.68 lbf).
 (4) Close the door (17).
 Subtask 52-41-14-220-051

 D. Check of the Load on the Locking Handle
 (1)
 Close the door

 (2)
 Measure the load on the door handle with a dynamometer and make sure that the load is between 8 daN (17.9847 lbf) and 15 daN (33.7213 lbf).

 Subtask 52-41-14-710-050
 E. Test
 (1) Do an operational test of the door warning system (Ref. TASK 52-71-00-710-001).
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 Avionics-Compartment Aft Door - Check of Clearance
 Figure 402/TASK 52-41-14-991-003- 12 (SHEET 1)
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 1  1
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 Avionics-Compartment Aft Door - Check of Clearance
 Figure 402/TASK 52-41-14-991-003- 22 (SHEET 2)
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R Clearance between Avionics-Compartment Aft Door and Feeders R Figure 403/TASK 52-41-14-991-005
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 5. Close-up
________ Subtask 52-41-14-865-052
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 46WV
 Subtask 52-41-14-410-050
 B. Close Access
 (1)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (2)
 Close the access door 824 (Ref. TASK 52-41-00-410-002).

 (3)
 Remove the access platform(s).

 1EFF : ALL 1 52-41-14Page 411 1 1 Aug 01/04 1 1 1CES 1 1EFF : ALL 1 52-41-14Page 601 1 1 May 01/03 1 1 1CES 1 C. Referenced Information

 DOOR - AVIONICS COMPARTMENT, AFT - INSPECTION/CHECK___________________________________________________
 TASK 52-41-14-200-001 
R R Detailed Inspection of Aft Avionics Compartment Access Door, Internal Structure 
1. Reason for the Job__________________
 Refer to the MPD TASK: 524121-01
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R  No specific No specific  circuit breaker(s) safety clip(s) access platform 1.80 m (5 ft. 11 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
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