• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-15 08:39来源:蓝天飞行翻译 作者:航空
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

 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO INSTALL
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2) Install the door locks on the wing landing gear (Ref 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 57-15-00
 ALL  ú ú 01 Page 201 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (3)  S 492-012Install the door locks on the body landing gear (Ref 32-00-30/201).
 (4)  S 022-013Remove the bolt that is unserviceable.
 (5)  S 612-014When you replace a bolt that attaches brackets and fittings, do one of the two steps that follows: (a) Apply the sealant in the hole where you will install the bolt. (b) Apply the sealant on the bolt shank.
 (6)  S 422-007Install the new bolt.
 S 092-006

 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO REMOVE
_______ THE DOOR LOCKS FROM THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT REMOVE THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (7)
Remove the door locks from the wing landing gear (Ref 32-00-30/201).

 S 092-010

 (8)
Remove the door locks from the body landing gear (Ref 32-00-30/201).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 57-15-00
 ALL  ú ú 01 Page 202 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WING LANDING GEAR SUPPORT BEAM GATE FITTING - REMOVAL/INSTALLATION
__________________________________________________________________
 1.  General
_______
 A.  This section contains two tasks. The first is the removal of the gate fitting on the support beam for the wing landing gear. The second is the installation of the gate fitting on the support beam for the wing landing gear.
 TASK 57-15-01-004-001
 2.  Gate Fitting Removal
____________________
 A.  Special Tools and Equipment
 (1) MIT65B01185 Landing Gear Beam Bearing Installation Tool
 B.  Standard Tools and Equipment
 (1)  
Hoist - Chain, with dynamometer, or other suitable tool for application of up or down 10,000-pound (maximum) load on support beam.

 (2)
Protective cloth cover


 C.  References
 (1)
7-11-01/201, Jacking Airplane

 (2)
06-09-08/201, Wing Access Doors and Panels

 (3)
32-00-30/201, Landing Gear Door Locks

 (4)
IPC 57-41-07 Fig. 1


 D.  Access
 (1)  
Location Zone 572 Landing Gear Support Beam and Rear Spar to Trailing Edge, Left

 672  Landing Gear Support Beam and Rear Spar to Trailing Edge, Right

 (2)  
Access Panel
 On the left wing:
 571AT Access Panel - Trailing Edge Up
 571BT Access Panel - Trailing Edge Up
 571CT Access Panel - Trailing Edge Up
 571DT Access Panel - Trailing Edge Up
 571AB Access Panel - Trailing Edge Lower
 572AB Access Panel - Trailing Edge Lower
 572BB Access Panel - Trailing Edge Lower
 572CB Access Panel - Trailing Edge Lower
 572DB Access Panel - Trailing Edge Lower
 572EB Access Panel - Trailing Edge Lower

 

 On the right wing: The same number panels as the left wing, but in the 600 number series
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 57-15-01
 ALL  ú ú 01 Page 401 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

SEE A
LANDING GEAR 
SUPPORT BEAM  FLAP TRACK 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 机翼 WINGS(12)