• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:57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) Move the locking mechanism of the opened cargo door in the locked condition as follows:
 (a)
 Press the roller lever (5) of the interlock mechanism outboard to release the blockage of the locking shaft.

 (b)
 Turn the locking handle up to the locked position and push it into the recess of the handle flap.


 **ON A/C ALL
 4. Procedure
_________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 408/TASK 52-32-21-991-008)
 **ON A/C 051-052,

 (Ref. Fig. 408A/TASK 52-32-21-991-008-A) R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-32-21-020-056
 A. Removal of the Interlock Mechanism NOTE : Remove the interlock mechanism (262) which includes the roller
____ lever (263), the interlock lever (269) and the spring pin (268) carefully because the spring (273) is under load.
 (1) Disconnect the roller lever (263) from the interlock fitting as follows:
 (a) Remove and discard the pin (258) from the nut (259).
 1EFF : ALL 1 52-32-21Page 491 1 1 Aug 01/05 1 1 1CES 1


 Interlock Mechanism
 Figure 408/TASK 52-32-21-991-008

R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page 492 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Interlock Mechanism
 Figure 408A/TASK 52-32-21-991-008-A 
R 1EFF :  051-052,  1  52-32-21 Page 493 
1  1  Aug 01/05
 1  1
 1CES  1

 

 (b)
 Remove the nut (259), the washers (260) and the bolt (265) from the interlock fitting.

 (c)
 Hold the roller lever (263) and remove the sleeve (261) from the interlock fitting.

 (d)
 Move the roller end of the roller lever (263) through the cutout of the cargo door structure inboard.


 (2)
 Disconnect the interlock lever (269) from the interlock fitting as follows:

 (a)
 Remove and discard the cotter pin (252), the washer (251) and the pin (271) from the interlock fitting.

 (b)
 Remove and discard the cotter pin (253) from the nut (254).

 (c)
 Remove the nut (254), the washers (255), the sleeve (270) and the bolt (267) from the interlock fitting.

 

 (3)
 Remove the interlock mechanism (262) from the cargo door as follows:

 (a)
 Pull the interlock mechansim down until the interlock lever (296) is free from the interlock fitting.

 (b)
 Remove the interlock mechanism (262) so that the spring pin (268) disengages from the spring sleeve (272).

 

 (4)
 Remove the spring sleeve (272) from the interlock fitting as follows:

 (a)
 Remove the spring (273) from the spring sleeve (272).

 (b)
 Remove and discard the cotter pin (257) and the washer (256) from the pin (266).

 (c)
 Remove the pin (266) together with the spacers (264) and the spring sleeve (272) from the interlock fitting.

 


R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page 494 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 051-052,


 Subtask 52-32-21-020-056-A
 A. Removal of the Interlock Mechanism NOTE : Remove the interlock mechanism which includes the roller lever
____ (5), the interlock lever (16) and the spring pin (15) carefully because the spring (24) is under load.
 (1)
 Disconnect the roller lever (5) from the structure bracket as follows:

 (a)
 Remove and discard the pin (8) from the nut (7).

 (b)
 Remove the nut (7), the washers (2) and the bolt (1) from the structure bracket.

 (c)
 Move the roller end of the roller lever (5) through the cutout of the cargo door structure inboard.

 

 (2)
 Disconnect the interlock lever (16) from the structure bracket as follows:

 (a)
 Release the retaining ring (22) and remove the pin (19) from the structure bracket.

 (b)
 Remove and discard the cotter pin (10) from the nut (11).

 (c)
 Remove the nut (11), the washers (12) and the bolt (18) from the structure bracket.

 

 (3)
 Remove the interlock mechanism from the cargo door as follows:

 (a)
 Pull the interlock mechansim down until the interlock lever (16) is free from the structure bracket.

 (b)
 Remove the interlock mechanism so that the spring pin (15) disengages from the spring sleeve (23).

 

 (4)
 
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 DOORS 舱门5(97)