(5)
Install the nut (9).
(6)
TORQUE the nut to 0.3 m.daN (26.54 lbf.in) (9) and safety it with the new cotter pin (8).
(7)
Install the nut (20) , TORQUE it to 0.3 m.daN (26.54 lbf.in) and safety it with the new cotter pin (19).
(8)
Install the bolt (14), the bonding braid (15), install the nut (21) and tighten it.
(9)
Install the bolt (5) , the bonding braid (6) , install the nut (7) and tighten it.
R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 32-22-13Page 409 1201-209, 1May 01/05 1 1 1CES 1
R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
Subtask 32-22-13-420-053-A
A. Installation of the Aft Door
(1) Install the bush (12) and the two shouldered bushes (22) on the door assembly (29).
NOTE : Make sure that the bush (12) and the two shouldered bushes
____ (22) are in the correct position.
(2)
Install the bush (11) on the fittings and keep the door (29) in position.
(3)
Lubricate the bolts (15) and (19) with COMMON GREASE (Material No. 04-022).
(4)
Install the bolts (15) and (19) and the washers (13) and (21).
(5)
Install the nut (10), TORQUE itto between 1.2 and 1.35 m.daN (106.19 and 119.46 lbf.in)and safety with a new cotter pin (9)
(6)
Install the nut (24), TORQUE it to between 1.2 and 1.35 m.daN (106.19 and 119.46 lbf.in) and safety it with a new cotter pin (23).
(7)
Install the bolt (7), the bonding braid (8), then the nut (6) and tighten it.
(8)
Put the jumpers (14) and (20) in position.
(9)
Install the bolts (16), then the nuts (5) and TORQUE them to between
0.37 and 0.48 m.daN (32.74 and 42.47 lbf.in).
(10) Install the bolt (17), the bonding braid (18), then the nut (25) and tighten it.
**ON A/C ALL
Subtask 32-22-13-867-050
B. Retract the NLG
(1) Retract the nose landing gear as slowly as possible (Ref. TASK 32-30-00-867-001).
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Subtask 32-22-13-420-054
C. Connection of the Rotating Rod to the Aft Door
(1) Lubricate the bolt (27) with COMMON GREASE (Material No. 04-004) and COMMON GREASE (Material No. 04-022).
NOTE : Do not mix Material No. 04-004 with Material No. 04-022. You
____ can use Material No. 04-022 as an alternative to Material No. 04-004. Clean and degrease the parts before you use Material No. 04-022.
(2)
Manually close the aft door (25).
(3)
Put the rotating rod (4) in position.
(4)
Install the bolt (27) , the washer (24) and the nut (23). NOTE : If you install a new bolt (27), drill a hole of 2 mm (0.0787
____
in.)
(5)
TORQUE the nut (23) to 0.3 m.daN (26.54 lbf.in) and safety it with the new cotter pin (22).
Subtask 32-22-13-820-050
D. Adjust the length of the rotating rod (4) as follows:
(1)
Disengage the tab of the lockwasher (2) from the nut (3).
(2)
Loosen the nut (3).
(3)
Turn the nut (1) to make the door (25) touch the stop (26).
(4)
Turn the nut (1) 180 deg. to tighten the rotating rod (4).
(5)
TORQUE the nut (3) to between 2.5 and 3 m.daN (18.43 and 22.12 lbf.ft) with the ADAPTOR - WRENCH (98AMS172321000).
(6)
Safety the nut (3) with the new lockwasher (2).
(7)
Safety the nut (1) with the MISCELLANEOUS (Material No. 19-010).
R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 32-22-13Page 411 1201-209, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
Subtask 32-22-13-420-054-A
C. Connection of the Rotating Rod to the Aft Door
(1) Lubricate the bolt (31) with COMMON GREASE (Material No. 04-004) or COMMON GREASE (Material No. 04-022).
NOTE : Do not mix Material No. 04-004 with Material No. 04-022. You
____ can use Material No. 04-022 as an alternative to Material No. 04-004. Clean and degrease the parts before you use Material No. 04-022.
(2)
Manually close the aft door (29).
(3)
Put the rotating rod (4) in position.
(4)
Install the bolt (31), the washer (28) and the nut (27). NOTE : If you install a new bolt (27), drill a hole of 2 mm (0.0787
____
in.)
(5)
TORQUE the nut (27) to 0.3 m.daN (26.54 lbf.in) and safety it with a new cotter pin (26).
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本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架4(12)
