• 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

R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-32-21-010-059
 C. Get Access
 (1)
 Remove the access panel 826AR from the cargo door to get access to the locking shaft.

 (2)
 Remove the lining and insulation of the cargo door to get access to the affected drift pin mechanism (Ref. TASK 52-32-13-000-001).


 **ON A/C 051-052,
 Subtask 52-32-21-010-059-A
 C. Get Access
 (1)
 Remove the access panel 826AR from the cargo door to get access to the safety shaft of the locking mechanism.

 (2)
 Remove the lining and insulation of the cargo door to get access to the affected drift pin mechanism (Ref. TASK 52-32-13-000-001).


 **ON A/C ALL
 4. Procedure
_________
 **ON A/C 001-049, 053-099, 101-105, 201-220,

 (Ref. Fig. 410/TASK 52-32-21-991-010)
R 1EFF : ALL 1 52-32-21Page A425 1 1 Aug 01/05 1 1 1CES 1


 Drift Pin Mechanism
 Figure 410/TASK 52-32-21-991-010

R 1EFF : 001-049, 053-099, 101-105, 201-220, 1 52-32-21Page A426 1 1 Aug 01/05 1 1 1CES 1


 **ON A/C 051-052,
 (Ref. Fig. 410A/TASK 52-32-21-991-010-C) **ON A/C 106-149, 221-299, 301-399,
 (Ref. Fig. 410B/TASK 52-32-21-991-010-B) **ON A/C 151-199,
R  (Ref. Fig. 410C/TASK 52-32-21-991-010-A) **ON A/C 401-499, 
R R  (Ref. Fig. 410D/TASK 52-32-21-991-010-D) **ON A/C 001-049, 053-099, 101-105, 201-220,
 (Ref. Fig. 411/TASK 52-32-21-991-011) **ON A/C 051-052,
 (Ref. Fig. 411A/TASK 52-32-21-991-011-B) **ON A/C 151-199,
 (Ref. Fig. 411B/TASK 52-32-21-991-011-A) **ON A/C 001-049, 053-099, 101-105, 151-199, 201-220,
 Subtask 52-32-21-020-061 A. Removal of the Drift Pin Assembly (1) Remove and discard the cotter pin (285) from the nut (286). (2) Remove the nut (286), the washers (287) and (289) and the bolt (282) to disconnect the drift pin (283) from the linkage (281). 

R 1EFF : ALL 1 52-32-21Page A427 1 1 Aug 01/05 1 1 1CES 1


 Drift Pin Installation
 Figure 410A/TASK 52-32-21-991-010-C 
R 1EFF :  051-052,  1  52-32-21 Page A428 
1  1  Aug 01/05
 1  1
 1CES  1

 

 INTENTIONALLY BLANK

R 1 1 52-32-21Page A429 1 1 Aug 01/05 1 1 1CES 1


 Drift Pin Mechanism
 Figure 410B/TASK 52-32-21-991-010-B12 (SHEET 1)

R 1EFF : 106-149, 221-299, 301-399, 1 52-32-21Page A430 1 1 Aug 01/05 1 1 1CES 1


 Drift Pin Mechanism
 Figure 410B/TASK 52-32-21-991-010-B22 (SHEET 2)

R 1EFF : 106-149, 221-299, 301-399, 1 52-32-21Page A431 1 1 Aug 01/05 1 1 1CES 1


 Drift Pin Mechanism
 Figure 410C/TASK 52-32-21-991-010-A
 1EFF :  151-199,  1  52-32-21 Page A432 
1  1  Aug 01/05
 1R 1 
1CES  1

 

 INTENTIONALLY BLANK

R 1 1 52-32-21Page A433 1 1 Aug 01/05 1 1 1CES 1


R Drift Pin Mechanism
R Figure 410D/TASK 52-32-21-991-010-D12 (SHEET 1)

R 1EFF : 401-499, 1 52-32-21Page A434 1 1 Aug 01/05 1 1 1CES 1


R Drift Pin Mechanism
R Figure 410D/TASK 52-32-21-991-010-D22 (SHEET 2)

R 1EFF : 401-499, 1 52-32-21Page A435 1 1 Aug 01/05 1 1 1CES 1


 Linkage Mechanism
 Figure 411/TASK 52-32-21-991-011- 13 (SHEET 1)

R 1EFF : 001-049, 053-099, 101-105, 201-220, 1 52-32-21Page A436 1 1 Aug 01/05 1 1 1CES 1


 Linkage Mechanism
 Figure 411/TASK 52-32-21-991-011- 23 (SHEET 2)

 1EFF : 001-049, 053-099, 101-105, 201-220, 1 52-32-21Page A437
1 1 Aug 01/05R 1 1
1CES 1


 Linkage Mechanism
 Figure 411/TASK 52-32-21-991-011- 33 (SHEET 3)

 1EFF : 001-049, 053-099, 101-105, 201-220, 1 52-32-21Page A438
1 1 Aug 01/05R 1 1
1CES 1


 Teleflex Control Cable
 Figure 411A/TASK 52-32-21-991-011-B 
R 1EFF :  051-052,  1  52-32-21 Page A439 
1  1  Aug 01/05
 1  1
 1CES  1

 

 Linkage Mechanism
 Figure 411B/TASK 52-32-21-991-011-A13 (SHEET 1)

R 1EFF : 151-199, 1 52-32-21Page A440 1 1 Aug 01/05 1 1 1CES 1


 Linkage Mechanism
 Figure 411B/TASK 52-32-21-991-011-A23 (SHEET 2)

R 1EFF : 151-199, 1 52-32-21Page A441 1 1 Aug 01/05 1 1 1CES 1


 Linkage Mechanism
 Figure 411B/TASK 52-32-21-991-011-A33 (SHEET 3)

R 1EFF : 151-199, 1 52-32-21Page A442 1 1 Aug 01/05 1 1 1CES 1


 (3)
 
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(107)