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时间:2011-04-12 10:20来源:蓝天飞行翻译 作者:航空
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WING GEAR WHEEL WELL INBOARD DOOR  STRIKE BOARD 
WING GEAR WHEEL WELL OUTBOARD DOOR 
FWD 

Wing Gear Wheel Well Door Figure 2 

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A
747-400
MAINTENANCE MANUAL


Wing Gear Shock Strut Door
Figure 3

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A
747-400 FAULT ISOLATION/MAINT MANUAL
WING GEAR DOORS
COMPONENT  102 FIG. SHT  QTY  ACCESS/AREA  REFERENCE 
BOARD - WHEEL WELL STRIKE DOOR - SHOCK STRUT INBOARD DOOR - SHOCK STRUT OUTBOARD DOOR - WHEEL WELL INBOARD DOOR - WHEEL WELL OUTBOARD FAIRING - SHOCK STRUT DOOR  2 2 2 2 2 2  2 2 2 2 2 2  WING GEAR WHEEL WELL DOORS WING GEAR DOORS WING GEAR DOORS WING GEAR DOORS WING GEAR DOORS WING GEAR SHOCK STRUT DOORS  32-12-03 32-12-06 32-12-07 32-12-02 32-12-01

Wing Gear Doors - Component Index
Figure 101

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747-400
FAULT ISOLATION/MAINT MANUAL


WING GEAR DOORS


Wing Gear Doors - Component Location
Figure 102 (Sheet 1)

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747-400
FAULT ISOLATION/MAINT MANUAL

RADIUS ROD (REF)
WING GEAR STRIKE BOARD WHEEL WELL INBOARD DOOR
WING GEAR WHEEL
FWD
WELL OUTBOARD DOOR
WING GEAR WHEEL WELL DOORS
B
DOOR (REF) LINKAGE RODS
WING GEAR SHOCK STRUT OUTBOARD DOOR
WING GEAR SHOCK STRUT INBOARD DOOR
WING GEAR SHOCK STRUT DOOR FAIRING
FWD
WING GEAR SHOCK STRUT DOORS C
Wing Gear Doors - Component Location Figure 102 (Sheet 2)
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747-400 MAINTENANCE MANUAL
 WING GEAR DOORS - ADJUSTMENT/TEST
_________________________________
 1.  General_______
 A.  This procedure has two tasks:
 (1)  
The adjustment of the doors for the wing landing gear.

 (2)  
The adjustment of the doors for the wing landing gear after the door actuator replacement.

 B.  
When you replace the door, you must adjust the door.

 C.  
When you replace the sequence valve, it is necessary to operate the door to examine the rigging pin installation. If you can not install the rigging pin freely, the door adjustment is necessary.

 D.  
When you remove or replace the door actuator, you must adjust the doors. This will make sure that the door actuator is fully locked when the doors are closed. There is a adjustment task for the door actuator replacement.

 E.  
There is no operational test with these adjustment procedures. Each adjustment procedure is a satisfactory replacement for an operational test.


 TASK 32-12-00-835-001
 2.  Adjustment - Wing Gear Doors____________________________
 
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