• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 17:55来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

_______
 1. Reason for the Job
__________________
 This procedure is only applicable when the aft door assy is removed for access. For the applicable procedure to remove the aft door assy for replacement, Ref. TASK 32-22-13-000-001.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice(s)
 No specific access platform 1.7 m (5 ft. 7 in.)

 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.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM LANDING GEAR 起落架4(16)