• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 00:00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

 52-33-21-991-003-A  Fig. 403A 

R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-21Page 428 1224-224, 228-228, 1May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,


 3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-105,
 Subtask 52-33-21-860-050
 A. Aircraft Maintenance Configuration Make sure that the AFT cargo-compartment door is opened (Ref. TASK 52-30-00-860-001).
 (1)
 Make sure that the access platform is in position below the AFT cargo-compartment door.

 (2)
 Make sure that the lining from the Bulk cargo compartment door (referred to as Bulk door) and the insulation packs are removed from the work area (Ref. TASK 52-33-13-000-001).

 (3)
 If necessary, open the Bulk door sufficiently to get access to the applicable components (Ref. TASK 52-30-00-860-006).

 (4)
 Make sure that the fully opened Bulk door is safetied with an applicable support device.

 (5)
 Make sure that the access platform in position in front of the Bulk door.


R **ON A/C 106-149, 221-221, 224-224, 228-228,
 Subtask 52-33-21-860-050-A
 A. Aircraft Maintenance Configuration Make sure that the AFT cargo-compartment door is opened (Ref. TASK 52-30-00-860-001).
 (1)
 Make sure that the access platform is in position below the AFT cargo-compartment door.

 (2)
 Make sure that the lining from the Bulk cargo compartment door (referred to as Bulk door) and the insulation packs are removed from the work area (Ref. TASK 52-33-13-000-001).


R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-21Page 429 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 (3)
 Make sure that the Bulk door sufficiently openend to get access to the applicable components (Ref. TASK 52-30-00-860-010).

 (4)
 Make sure that the fully opened Bulk door is safetied with an applicable support device.

 (5)
 Make sure that the access platform in position in front of the Bulk door.


R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 4. Procedure
_________ R **ON A/C 001-003, 051-054,
 Subtask 52-33-21-910-050
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Clean the component interface and/or the adjacent area.

 (4)
 Apply a layer of SEALANTS (Material No. 09-018) to the mating surfaces of the joint assemblies (48), the lever (77) and the main lever (66).

 (5)
 Apply a layer of SEALANTS (Material No. 09-016) to the mating surfaces of the flange bearings (36).

 (6)
 Apply a layer of SEALANTS (Material No. 09-005) to the mating surface of the hook arrester (81).

 (7)
 Apply a layer of COMMON GREASE (Material No. 04-011) to the splines of the joint assemblies (48) and the barrel locks (31).


 (8) Apply COMMON GREASE (Material No. 04-004) to the shaft of all bolts. R
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-21Page 430 1224-224, 228-228, 1May 01/05 1 1 1CES 1


R  **ON A/C 004-049, 055-099, 101-149, 221-221, 224-224, 228-228,
 Subtask 52-33-21-910-050-A
 A. Preparation for Installation
 (1) Make sure that the parts retained from the removed component are clean and in the correct condition.
 (2) Do an inspection of the component interface and/or the adjacent area.
 (3) Clean the component interface and/or the adjacent area.
 (4) Apply a layer of SEALANTS (Material No. 09-005) to the mating surfaces of the outer flange bearings (154) and the flange bearings (151), (179) and (196).
 (5) Apply a layer of SEALANTS (Material No. 09-005) to the mating surface of the hook arrester (81) and the attachment sheet (114) .
 (6) Apply a layer of COMMON GREASE (Material No. 04-011) to the splines of the joint assemblies (163) and the tooth shaft (149).
 (7) Apply COMMON GREASE (Material No. 04-004) to the shaft of all bolts. 
R  **ON A/C 001-003, 051-052, 
R  Subtask 52-33-21-420-050 
R R  B. Installation of the Door Handle Mechanism (Ref. Fig. 401/TASK 52-33-21-991-001) 
R  (1) Install the spring unit (9) and/or the push rod (24) as follows: 
R  (a) Connect the push rod (24) to the main lever (66) as follows: 
R R  NOTE : Make sure that the locking shaft is in the locked____ position. 
R R  1_  Put the push rod (24) and the related bushes (61),(62) to themain lever (66). 
 
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6(63)