• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:52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

 (b)
 Install the bolt (46), the washer (47), the tab plate (44), the washer (43) and the nut (42) on the sliding sleeve (58).

 


 NOTE : You can install a lock plate (59) as an alternative to the
____ washer (43) and the tab plate (44).
 (c) Tighten the nut (42) and safety it with the cotter pin (41).
 (3) Connect the telescopic rod assembly (57) to the yoke assembly (52) as follows:
 (a)
 If remove, install the bush (51) in the yoke assembly (52).

 (b)
 Assemble the fork-end (56) to the yoke assembly (52) and the piston of the door damper (55).

 (c)
 Install the bolt (54), the washers (53) and (50) and the nut (49).

 (d)
 Tighten the nut (49) and safety it with the cotter pin (48).


 1EFF : 301-399, 1 52-22-14Page 417 1 1 May 01/04 1 1 1CES 1


 5. Close-up
________ Subtask 52-22-14-410-051
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Do the special precaution for the door damper and emergency operation cylinder (Ref. TASK 52-22-00-860-004).

 (3)
 Close applicable the door (Ref. TASK 52-22-00-410-001).

 (4)
 Remove the access platform(s).


 1EFF : 301-399, 1 52-22-14Page 418 1 1 May 01/04 1 1 1CES 1


 SEAL - DOOR - MAINTENANCE PRACTICES
___________________________________
 TASK 52-22-18-300-001
 Preventive Seepage Procedure
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific lint-free cloth
 No specific access platform 3.20 m (10 ft. 6 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-012 USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 11-016 USA BOEING BAC 5000 BAC 5504 BAC 5750 CLEANING SOLVENT (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and Composite Material 52-22-00-010-001 Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-410-001 Closing of the Emergency Exit Doors from the Passenger Compartment 52-22-00-860-003 Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder
 1EFF : 301-399, 1 52-22-18Page 201 1 1 May 01/04 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------


52-22-00-860-004 Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder 52-22-18-991-002 Fig. 201
 3. Job Set-up
__________ Subtask 52-22-18-010-051
 A. Get Access
 (1)
 Open the applicable emergency exit door (referred to as door) (Ref. TASK 52-22-00-010-001).

 (2)
 Make sure that the access platform in position below the opened door.

 (3)
 Make sure that the special precaution procedure on the door damper and emergency operation cylinder is done (Ref. TASK 52-22-00-860-003).


 4. Procedure
_________ Subtask 52-22-18-390-050
 A. Seepage Prevention at the Sealing Profile
 (Ref. Fig. 201/TASK 52-22-18-991-002)

 (1)
 Clean the lower area of the sealing profile with CLEANING AGENTS (Material No. 11-016) and a lint-free cloth.

 (2)
 If necessary, repair the paint coating of the sealing profile (Ref. TASK 51-75-12-300-001).

 (3)
 Apply a layer of COMMON GREASE (Material No. 04-012) on the contact area of the sealing profile.


 1EFF : 301-399, 1 52-22-18Page 202 1 1 May 01/04 1 1 1CES 1


 Sealing Profile at the Emergency Exit - Seepage Prevention
 Figure 201/TASK 52-22-18-991-002

 1EFF : 301-399, 1 52-22-18Page 203 1 1 May 01/04 1 1 1CES 1


 5. Close-up
________ Subtask 52-22-18-410-051
 A. Close Access
 
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3(105)