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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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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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)