• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 17:53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

_
 in.) and 0.1 mm (0.0039 in.).

 5 Make sure that you can align a hole of the nut (6) with the
_ slot of the shaft (1) and keep the clearance given above. If not:
 -loosen the nut (6),
 -remove the washer (5),
 -adjust the thickness of the washer (5) to get the clearance given above with a hole of the nut (6) aligned with the slot of the shaft (1),
 1EFF : 005-049, 055-099, 101-105, 151-199, 1 32-21-27Page 430 1201-228, 301-302, 1May 01/05 1 1 1CES 1 1EFF : 005-049, 051-051, 055-099, 101-105, 1 32-21-27Page 431 1151-199, 201-228, 301-302, 1May 01/05 1 1 1CES 1 1EFF : 051-051, 1 32-21-27Page 432 1 1 May 01/05 1 1 1CES 1 1EFF : 051-051, 1 32-21-27Page 433 1 1 May 01/05 1 1 1CES 1 1EFF : 051-051, 1 32-21-27Page 434 1 1 May 01/05 1 1 1CES 1 1EFF : 001-004, 051-054, 1 32-21-27Page 435 1 1 May 01/05 1 1 1CES 1


 NOTE : The total thickness of the washer (5) (shoulder____ included) must not be less than 4 mm (0.1574 in.). If the thickness of the washer (5) is less than 4 mm (0.1574 in.), replace it with the new washer (5).
 - do a passivating treatment on the reworked surface (Ref. CMM 320901), - do the torque procedure on the nut (6) again.
 6_ Apply a layer of SPECIAL MATERIALS (Material No. 05-047) to the threads of the screw (10).
 7_ Install the screw (10), the washer (7), the nut (8) and tighten it.
 8_ Install the new cotter pin (9) on the nut (8).
 (5) Do a check for possible damage on connectors, proximity sensors and targets.
 (6) Apply COMMON GREASE (Material No. 04-022) to the hinges of the torque links (Ref. TASK 12-22-32-640-001).
 (7) Install the removed wheel of the nose gear (Ref. TASK 32-41-12-400-001).
 (8) Apply a layer of SEALANTS (Material No. 09-001) to the areas identified E.
 (9) Make sure that the lubrication points are clean and in good condition on the shaft (1). 
R  **ON A/C 051-051, 
R  Subtask 32-21-27-420-050-B 
R  B. Installation of the Torque Link Assy 
R R  (1) Install the lower arm (Ref. Fig. 403/TASK 32-21-27-991-002) 
R R  (a) Align the bores of the lower arm, of the lower bracket and of the new washer (20) and washer (21). 
R  (b) Install the lower shaft (26).

 

R  (c) Engage the screw (22) with the screw head up. 
R  (d) Install the support (23) and the nut (25) and TORQUE the nut to 
R  between 1.7 and 2 m.daN (12.53 and 14.74 lbf.ft). 
R  (e) Safety the nut (25) with the new cotter pin (24). 
R  (2) Install the upper arm 
R  (Ref. Fig. 405A/TASK 32-21-27-991-003-A) 
R  (a) Put the support (63) in position on the upper arm of the torque 
R  links. 
R  (b) Install the screw (68), the washers (67) and (75) and the nut 
R  (76). 
R  (c) TORQUE the nut (76) to between 0.6 and 0.7 m.daN (53.09 and 61.94 
R  lbf.in) and safety it with the new cotter pin (74). 
R  (d) Put the stop (62) in position on the support (63). 
R  (e) Install the screws (60), the washers (61) and (64) and the nuts 
R  (66). 
R  (f) TORQUE the nuts (66) to between 0.6 and 0.7 m.daN (53.09 and 
R  61.94 lbf.in) and safety them with the cotter pin (65). 
R  (g) Put the upper arm of the torque links and the washer (72) and 
R  washer (73) in position. 
R  (h) Install the upper shaft (71), align the rigging holes. 
R  (i) Clean the screw (77) with CLEANING AGENTS (Material No. 11-004A) 
R  and dry it with filtered compressed air. 
R  (j) Apply a light coat of SPECIAL MATERIALS (Material No. 05-047) to 
R  the screw (77). Install the screw and correctly put the threads 
R  in position. 
R  (k) Install the washer (70). 
R  (l) Install the nut (69) but do not tighten.

 

R  (3) Install the target support 
R  (Ref. Fig. 404A/TASK 32-21-27-991-005-A) 
R  (a) If you have the alternative solution 1 
R  1_  Put the casing (137) in position on the screw (146).
R  2_  Install the screw (139) and the new lockwasher (140).
R  3_  Tighten the screw (139) and safety it with the lockwasher
R  (140). 
R  4_  Install the indicator (135) on the screw (146).
R  5_  Install the screw (134), the washers (133) and (132) and the
R  nut (131). 
R  6_  TORQUE the nut (131) to between 0.6 and 0.7 m.daN (53.09 and
R  61.94 lbf.in) and safety it with the new cotter pin (130). 
 
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3(115)