B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-105, 151-156, 201-209,
32-22-13-991-008 Fig. 404 R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
32-22-13-991-008-A Fig. 404A
1EFF : ALL 1 32-22-13Page 425 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
3. Job Set-up
__________
Subtask 32-22-13-860-053
A. Aircraft Maintenance Configuration
(1)
In the cockpit, on the panel 400VU, put warning notice(s) in position to tell persons not to operate the landing gear control lever.
(2)
Put the safety barriers in position.
(3)
Put an access platform in position.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-156, 201-209,
(Ref. Fig. 404/TASK 32-22-13-991-008) R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
(Ref. Fig. 404A/TASK 32-22-13-991-008-A)
**ON A/C 001-049, 051-099, 101-105, 151-156, 201-209,
Subtask 32-22-13-020-054
A. Removal of the Aft Door Assy
NOTE : Do not change the adjustment of the rotating rod (1).
____
(1)
Remove the nuts (18) and (4) and the bolts (11) and (2).
(2)
Remove the bonding braids (12) and (3).
(3)
Remove the cotter pin (19) and discard it, remove the nut (20) and the washer (21).
(4)
Remove the bolt (23) and release the door (22) from its connection to the rotating rod (1).
1EFF : ALL 1 32-22-13Page 426 1 1 Aug 01/05 1 1 1CES 1
NLG Aft Door Assy
Figure 404/TASK 32-22-13-991-008
R 1EFF : 001-049, 051-099, 101-105, 151-156, 1 32-22-13Page 427 1201-209, 1May 01/05 1 1 1CES 1
NLG Aft Door Assy Figure 404A/TASK 32-22-13-991-008-A
R 1EFF : 106-149, 157-199, 210-299, 301-399, 1 32-22-13Page 428 1401-499, 1Aug 01/05 1 1 1CES 1
(5) Remove the cotter pin (16) and discard it, remove the nut (17), the bolt (13) and the washer (14).
NOTE : Keep the door (22) in position to help you remove the second
____
hinge assembly.
(6) Remove the cotter pin (5) and discard it, remove the nut (6), the washer (9) and the bolt (10).
(7) Remove the door (22). R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
Subtask 32-22-13-020-054-A
A. Removal of the Aft Door Assy
NOTE : Do not change the adjustment of the rotating rod (1).
____
(1)
Remove the nuts (22) and (3) and the bolts (14) and (4).
(2)
Remove the bonding braids (15) and (5).
(3)
Remove the nuts (2), the jumpers (11) and (17) and the bolts (13).
(4)
Remove the cotter pin (23) and discard it, remove the nut (24) and the washer (25).
(5)
Remove the bolt (27) and release the door (26) from its connection to the rotating rod (1).
(6)
Remove the cotter pin (20) and discard it, remove the nut (21), the bolt (16), the washer (18) and the two shouldered bushes (19).
NOTE : Keep the door (26) in position to help you to remove the
____
second hinge assembly.
(7)
Remove the cotter pin (6) and discard it, remove the nut (7), the bolt (12), the washer (10) and the bushes (8) and (9).
(8)
Remove the door (26).
1EFF : ALL 1 32-22-13Page 429 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
TASK 32-22-13-410-001
Installation of the Aft Door Assy after Removal for Access
1. Reason for the Job
__________________
This procedure is only applicable when the aft door assy was removed for access. For the applicable procedure to install the aft door assy after replacement, Ref. TASK 32-22-13-400-001.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架4(16)
