• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:42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

 Material No. 11-004  USA MIL-T-81533
 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
 (Ref. 20-31-00)

 Material No. 19-003  USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 1EFF : ALL 1 52-13-11Page 410 1 1 May 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
3 self adhesive patches 11-21-52 08 -010 3 self adhesive patches 11-21-52 08A-010 27 cotter pin 52-13-04 02B-010 56 cotter pin 52-13-04 04B-170 56 cotter pin 52-13-04 04D-170
R  56 cotter pin 52-13-04 04E-170 128 cotter pin 53-46-04 80B-060 152 lock plate 52-13-11 21 -040 152 lock plate 52-13-11 21A-040
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 25-23-45-000-003 Removal of the Door Frame Linings at the Left AFT Passenger/Crew Door 25-23-45-000-004 Removal of the Door Frame Linings at the Right AFT Passenger/Crew Door 25-23-45-400-005 Installation of the Door Frame Linings at the Right
 AFT Passenger/Crew Door
 25-23-45-400-008 Installation of the Door Frame Linings at the Left
 AFT Passenger/Crew Door

 25-23-46-400-002  Installation of the Door Linings at the AFT
 Passenger/Crew Doors
 25-62-44-400-001 Installation of the Escape-Slide Pack-Assembly
 51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only)

 1EFF : ALL 1 52-13-11Page 411 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-00-00-081-001  Removal of the Safety Barriers
 52-10-00-080-001  Removal of the Passenger/Crew Door Ballast Weight
 (98D52103501000) for Escape Slide
 52-10-00-080-001  Removal of the Passenger/Crew Door Ballast Weight
 (98D52103501000) for Escape Slide/Raft
 52-10-00-220-007  Check of the Preload of the Cover Plate
 52-10-00-410-001  Closing of the Passenger/Crew Door
 52-10-00-480-001  Installation of the Passenger/Crew Door Ballast
 Weight (98D52103501000) for Escape Slide
 52-10-00-480-001  Installation of the Passenger/Crew Door Ballast
 Weight (98D52103501000) for Escape Slide/Raft
 52-10-00-860-001  Special Precautions before Work on the Passenger/Crew
 Door
 52-10-00-860-002  Special Precautions after Work on the Passenger/Crew
 Door
 52-11-00-820-002  Load Adjustment of the Control Handle of the FWD
 Passenger/Crew Door
 52-13-12-400-002  Installation of the Guide Arms
 52-13-31-000-001  Removal of the Lining Flap
 52-71-00-820-001  Adjustment of the Proximity Switches (11WV1, 11WV2,
 15WV1, 15WV2) of the Locking Hook of the Pax/Crew
 Doors with the CHECKING TOOL-DOOR
 52-13-11-991-002  Fig. 401
 52-13-11-991-004  Fig. 402
 52-13-11-991-005  Fig. 403
 **ON A/C 001-002,
 52-13-11-991-007  Fig. 404 

R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 52-13-11-991-007-A Fig. 404A
 **ON A/C ALL
 52-13-11-991-018 Fig. 405

 1EFF : ALL 1 52-13-11Page 412 1 1 Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------


REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
**ON A/C 001-049, 051-061, 101-104, 201-203,
 52-13-11-991-011 Fig. 406 R **ON A/C 062-099, 105-149, 151-199, 204-299, 301-399, 401-499,
 52-13-11-991-011-A Fig. 406A
 **ON A/C ALL
 52-13-11-991-016 Fig. 407
 
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2(78)