• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-12 10:07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

 32-11-07
 ALL  ú ú 01 Page 201 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

STRUT SIDE LOWER  STRIKER 10.  WASHER 1.  ROLLER CROSSBOLT 3. 
4.  SIDE PLATE 
SEE  C  SEE  A  9.  SPINDLE BOLT  2.  NUT  5.  LINK 
SEE  B  8.  O-RINGS  SPINDLE  6.  PUSHROD END 
7.  LUBRICATION INSERT  A 
PUSHROD ASSEMBLY11. 
BOLT22.  A  SPINDLE 
14.  BRACKET 
21.  SHIM  13.  WASHER 
A  12.  SPRING HOUSING 
20.  FRAME  NUT BRACKET 15. 14. 
14. 22. BOLT BRACKET  PLANE "E"  SPRING LOCKING WASHER 19.  (2 LOCATIONS) PIN ROD END LOCKNUT 16. 17. 
21. SHIM  LEVER18. 
20. FRAME  A-A  PLANE "D" 0.005  B  FWD 

Installation of the Lower Spindle
Figure 201 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-07
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

SIDE STRUT
4. SIDE PLATE
4.
SIDE PLATE

5.
LINK


FWD
6. ROD END
SHOCK STRUT
12. SPRING HOUSING
ROLLER  DIMENSION "C" = 0.03 |0.01 INCH (RECESSED)
11.  PUSHROD ASSEMBLY 
18.  LEVER  15.  NUT  17.  ROD END 
SEE  D 
HOOK 
UPPER  C 
TORSION 
LINK 

ROLLER"B" = 0.12 |0.01 SUPPORT
INCH
90`
HOOK
ROLLER
TORSION LINK
D
Installation of the Lower Spindle Figure 201 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-07
 ALL  ú ú 01 Page 203 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 492-051
 WARNING:_______ YOU MUST CAREFULLY DO THE STEPS IN THE TASK 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)  
Do this task: "Installation of the Door Locks on the Wing Landing Gear" (AMM 32-00-30/201).

 S 492-052

 (3)  
Do this task: "Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).

 S 842-004

 (4)  
Release the pressure from the hydraulic system No. 4 (AMM 29-11-00/201).

 S 862-005

 (5)  
Remove the load from the wing landing gear until the wheels are clear of the ground (AMM 07-11-01/201).

 S 032-006

 (6)  
Remove three bolts to disassemble the side plates (4) and the related components.

 S 032-007

 (7)  
Remove the cross bolt (1), the nut (2), the spindle bolt (9), and the remaining truck lock components.

 S 032-008

 (8)  
Remove the rod end (6), the locknut and the washer.

 S 032-009

 (9)  
Disconnect the rod end (17) from the lever (18).

 S 032-010

 (10)
 Remove the bolt (22) from the frame (20) and the bracket (14).

 S 032-011

 (11)
 Move the frame (20) and the lever (18) down.

 (a)  
This will permit you to remove the pushrod assembly (11) and the spring (19) from the lower end of the spindle.

 (12)
 Remove the pins (16) and the spring housing (12).

 (13)
 Remove the nut (15), the bracket (14), and the washer (13).


 S 032-012
 S 032-013
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
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 起落架 LANDING GEAR 1(144)