• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 17:50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

 For the 2M harness, position the harness on the bracket (3) and TORQUE the upper locknut (4) to between 0.396 and 0.452 m.daN (35.04 and 39.99 lbf.in).


R 1EFF : 001-003, 051-052, 301-399, 1 32-11-43Page 433 1 1 May 01/05 1 1 1CES 1


 (5) Safety the locknuts (4) together with MISCELLANEOUS (Material No. 19-010).
 CAUTION : MAKE SURE THAT ALL ELECTRICAL CONNECTORS ARE IDENTIFIED_______ WITH THEIR FIN NO. TO CORRECTLY CONNECT EACH PLUG TO ITS RELATED RECEPTACLE. INCORRECT CONNECTION OF THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO THE AIRCRAFT ELECTRICAL SYSTEM.
 (6) Remove the blanking caps from the electrical connectors.
 (7) For the 1M harness: (Ref. Fig. 401/TASK 32-11-43-991-001) 
R  **ON A/C 001-002, 051-052,
 (Ref. Fig. 405/TASK 32-11-43-991-004) 
R  **ON A/C 001-003, 051-052, 
R  Post SB  32-1190 For A/C 001-002,051-052,
 (Ref. Fig. 405B/TASK 32-11-43-991-004-D) 
R  **ON A/C 001-003, 051-052,
 (a) Connect the electrical connectors that follow: - 21GA-A (20GA-A) (7) - 3GW-A (2GW-A) (8) - LGAB1 (LGAB2) (9) - 15GA-A (14GA-A) (13) - 13GG-A (12GG-A) (61) - 17GG-A (16GG-A) (62). 
R  **ON A/C 001-002, 051-052,
 (Ref. Fig. 405/TASK 32-11-43-991-004) 
R  **ON A/C 001-003, 051-052, 
R  Post SB  32-1190 For A/C 001-002,051-052,
 (Ref. Fig. 405B/TASK 32-11-43-991-004-D) 

R 1EFF : 001-003, 051-052, 1 32-11-43Page 434 1 1 May 01/05 1 1 1CES 1


R  **ON A/C 001-003, 051-052,
 (b) Put the clamp (51) in position on the cable for the connector (9).
 (c) Install the clamp (51) on the bracket (54) with the bolts (50), the washers (52) and the nuts (53).
 (Ref. Fig. 406/TASK 32-11-43-991-010)
 (d) Connect the electrical connector 4027VC (4028VC) (2) at the MLG disconnection box (Ref. TASK 32-11-46-400-001).
 (8) For the 2M harness: (Ref. Fig. 401/TASK 32-11-43-991-001) 
R  **ON A/C 001-002, 051-052,
 (Ref. Fig. 405/TASK 32-11-43-991-004) 
R  **ON A/C 001-003, 051-052, 
R  Post SB  32-1190 For A/C 001-002,051-052,
 (Ref. Fig. 405B/TASK 32-11-43-991-004-D) 
R  **ON A/C 001-003, 051-052,
 (a) Connect the electrical connectors that follow: - LGAB3 (LGAB4) (10) - 23GA-A (22GA-A) (11) - 17GA-A (16GA-A) (12) - 11GG-A (14GG-A) (60) - 15GG-A (18GG-A) (63).
 (Ref. Fig. 404/TASK 32-11-43-991-003)
 (b) Put the clamp (58) in position on the cable for the connector (10).
 (c) Install the clamp (58) on the bracket (55) with the bolts (59), the washers (57) and the nuts (56).
 (Ref. Fig. 406/TASK 32-11-43-991-010) 

R 1EFF : 001-003, 051-052, 1 32-11-43Page 435 1 1 May 01/05 1 1 1CES 1


 (d)
 Connect the electrical connector 4029VC (4030VC) (1).

 (e)
 Install the plug (91) in the liner (90). Do not tighten the center nut (92).

 (f)
 Align the end of the protective sleeve of the 2M harness with the inboard face of the plug (91).

 (g)
 Tighten the center nut (92) sufficiently to secure the plug (91). (Ref. Fig. 401/TASK 32-11-43-991-001)

 (h)
 Install the grommet (19) approximately 75.0 mm (2.9527 in.) from the electrical connector (11) and attach with a new cable tie (18).


 (Ref. Fig. 402/TASK 32-11-43-991-037)
 (9) Install the P clips (16) on the leg assembly with the bolts (14), the washers (15) and the nuts (17).
 (10)
 TORQUE the nuts (17) to between 0.40 and 0.45 m.daN (35.39 and 39.82 lbf.in).

 (Ref. Fig. 403/TASK 32-11-43-991-002)

 (11)
 Install the clamps (40) on the harnesses with the bolts (41), the washers (39) and the nuts (38).

 (12)
 TORQUE the nuts (38) to between 0.40 and 0.45 m.daN (35.39 and 39.82 lbf.in).

 (13)
 Install the clamps (36) on the harnesses with the bolts (37), the washers (35) and the nuts (34).

 (Ref. Fig. 401/TASK 32-11-43-991-001)

 (14)
 Make sure that the dimension X for the 1M harness is 150.0 mm (5.9055 in.).

 (15)
 Make sure that the dimension Y for the 2M harness is 280.0 mm (11.0236 in.).

 (Ref. Fig. 403/TASK 32-11-43-991-002)

 (16)
 TORQUE the nuts (34) to between 0.40 and 0.45 m.daN (35.39 and 39.82 lbf.in).


R 1EFF : 001-003, 051-052, 1 32-11-43Page 436 1 1 May 01/05 1 1 1CES 1


 (17)
 Put the band-clamps (33) in position on the line-support blocks.

 (18)
 Visually inspect each harness for correct routing and installation.
 
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2(117)