S 494-041
(3)
Do this task: "Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).
F.
Procedure
S 224-050
CAUTION: MAKE SURE THAT YOU DO NOT MOVE OR DAMAGE THE WING GEAR TRUCK
_______ SENSORS OR TARGET BRACKET. IF THE TARGET BRACKET OR SENSORS ARE MOVED, THEN THE AIRPLANE SYSTEMS MAY NOT RECOGNIZE AN IN-AIR CONDITION.
(1) If the sensor or target bracket is moved or damaged, then do the task to measure the wing landing gear truck sensor clearance (AMM 32-61-22/201).
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A
747-400
MAINTENANCE MANUAL
SEE A
SHOCK STRUT
DRAG BRACE
HYDRAULIC LINES
FWD SEE F TRUCK
TILT
ACTUATOR
UPPER
SEE E TORSION
LINK
SEE B
TRUCK WHEEL SEE C SEE D
Figure 401 (Sheet 1) Wing Gear Shock Strut Installation
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
SHOCK STRUT
OUTBOARD DOOR FITTING
DRAG BRACE
SHOCK STRUT
A
HYDRAULIC LINES
TRUCK ACTUATOR TILT
LOWER TORSION LINK
B
Wing Gear Shock Strut Installation Figure 401 (Sheet 2)
JUNCTION BOX
SHOCK STRUT
UPPER TORSION LINK
WHEEL
TRUCK
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A
747-400 MAINTENANCE MANUAL
INNER CYLINDER YOKE
1.
WASHER
2.
NUT
3.
LUBRICATION INSERT
4.
O-RINGS (2 LOCATIONS)
5.
LOCKBOLT
BRAKE ROD
BRAKE ROD
7. BRAKE
ROD BOLT
6. O-RINGS (2 LOCATIONS)
C
INNER CYLINDER YOKE
8.
SPLINE WASHER
9.
PIVOT NUT FWD
10.LUBRICATION INSERT
11.
LOCKBOLT INBD
12.
O-RINGS
13.
TRUCK PIVOT BOLT
1
TRUCK BEAM
BOLT HEAD MUST BE
ON THE INBOARD
SIDE OF THE TRUCK
BEAM
1
D
Wing Landing Gear Shock Strut Installation
Figure 401 (Sheet 3)
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A
747-400
MAINTENANCE MANUAL
SHOCK STRUT
14. BOLT
TRUCK LOCK ASSEMBLY
15. NUT
UPPER
TORSION
LINK
E 17. SHIM
16. LOCKBOLT
SHOCK STRUT
19. WASHER
18. NUT
22. BOLT PIN
20.
21.
END CAP (2 PLACES)
23. WASHER (2 PLACES) 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(98)