____
(11)
Install the bolt (23), the washer (21) and the nut (20).
(12)
TORQUE the nut (20) to 0.3 m.daN (26.54 lbf.in) and safety it with the new cotter pin (19).
R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
Subtask 32-22-13-420-056-A
A. Installation of the Aft Door Assy
(1) Install the bush (9) and the two shouldered bushes (19) on the door assembly (26).
NOTE : Make sure that the bush (9) and the two shouldered bushes (19)
____
are in the correct position.
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(2) Install the bush (8) on the fittings and keep the door (26) in position.
R (3) Lubricate the bolts (12) and (16) with COMMON GREASE (Material No. R 04-022).
(4)
Install the bolts (12) and (16) and the washers (10) and (18).
(5)
Install the nut (7), TORQUE it to 0.3 m.daN (26.54 lbf.in) and safety it with a new cotter pin (6).
(6)
Install the nut (21), TORQUE it to 0.3 m.daN (26.54 lbf.in) and safety it with a new cotter pin (20).
(7)
Install the bolt (4), the bonding braid (5), then the nut (3) and tighten it.
(8)
Put the jumpers (11) and (17) in position.
(9)
Install the bolts (13), then the nuts (2) and TORQUE them to between
0.37 and 0.48 m.daN (32.74 and 42.47 lbf.in).
(10)
Install the bolt (14), the bonding braid (15), then the nut (22) and tighten it.
(11)
Put the rotating rod (1) in position. NOTE : Do not change the adjustment of the rotating rod (1).
____
(12)
Install the bolt (27), the washer (25) and the nut (24).
(13)
TORQUE the nut (24) to 0.3 m.daN (26.54 lbf.in) and safety it with a new cotter pin (23).
**ON A/C ALL
Subtask 32-22-13-640-053
B. Lubricate the doors of the nose landing gear (Ref. TASK 12-22-32-640-002).
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5. Close-up
________ Subtask 32-22-13-860-055
A. Put the aircraft back to its initial configuration.
(1)
Remove the access platform(s).
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
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DOOR ASSY - LEG - REMOVAL/INSTALLATION
______________________________________ TASK 32-22-15-000-001 Removal of the Leg Door Assy WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______
OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
R This procedure is only applicable if the leg door assy is removed for R replacement. For the applicable procedure to remove the leg door assy for R access only, Ref. TASK 32-22-15-010-001.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice(s)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-22-15-991-001 Fig. 401
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3. Job Set-up
__________ Subtask 32-22-15-941-050
A. Safety Precautions
(1)
In the cockpit, on the panel 400VU, put the warning notice(s) in position to tell persons not to operate the landing gear control level.
(2)
In the cockpit, on the steering handwheels (CAPT and F/O) and on the brake pedals, put warning notice(s) in position to tell persons not to operate them.
(3)
Put the safety barriers in position.
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本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM LANDING GEAR 起落架4(18)
