747-400 AMM 飞机维护手册 起落架 LANDING GEAR 2(110)

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 B.  To do this procedure, you must remove the inboard door of the shock strut on the wing landing gear.
 TASK 32-12-06-206-001
 2.  Wing Landing Gear Shock Strut Inboard Door Examination (Fig. 601)
______________________________________________________
 A.  References
 (1)  
20-11-01/401, Bushings and Bearings

 (2)  
32-12-06/401, Wing Gear Shock Strut Inboard Door

 (3)  
IPC 32-12-05 Fig. 1, 32-12-06

 B.  
Access

 (1)  
Location Zone
 733 Wing Landing Gear Door, LH
 743 Wing Landing Gear Door, RH

 C.  
Procedure

 S 026-002
 (1)  
Do this task "Wing Landing Gear Shock Strut Inboard Door Removal" (Ref 32-12-06/401).

 S 226-005

 (2)  
Examine the components of the inboard door of the shock strut on the wing landing gear for worn areas.

 (a)  
Measure the parts at the locations shown in figure 601.

 (b)  
Compare the measured dimensions to the wear limits in figure

 601.

 (c)  
If a part is not in tolerance, replace the part if you cannot repair it.

 S 426-004
 (3)  Do this task "Wing Landing Gear Shock Strut Inboard Door Installation" (Ref 32-12-06/401).
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MAINTENANCE MANUAL

WING GEAR SHOCK STRUT OUTBOARD DOOR
SEE E
WING GEAR SHOCK STRUT INBOARD DOOR
WING GEAR SHOCK STRUT DOOR FAIRING
FWD SEE D
SEE A
WING GEAR DRAG STRUT
INBOARD DOOR LINKAGE ROD
SEE B
WING GEAR SHOCK STRUT INBOARD DOOR
A
SEE C
FWD
INBD
Wing Gear Shock Strut Inboard Door Wear Limits
Figure 601 (Sheet 1)

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MAINTENANCE MANUAL

INBOARD DOOR

GEAR FITTING

Wing Gear Shock Strut Inboard Door Wear LimitsFigure 601 (Sheet 2)
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MAINTENANCE MANUAL

8. BUSHING/BUSHING (2 PLACES)
7.
CLEVIS LUG
11.
10.

WING LANDING GEAR INBOARD DOOR ASSEMBLY
WING LANDING GEAR OUTBOARD DOOR ASSEMBLY
INBOARD DOOR ASSEMBLY
OUTBOARD DOOR ASSEMBLY
FORWARD AND MID HINGE

E

Wing Gear Shock Strut Inboard Door Wear Limits
Figure 601 (Sheet 3)

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MAINTENANCE MANUAL

INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  WEAR ALLOWED DIM. *[7]  DIAM CLEAR-ANCE MAX 
MIN  MAX 
1  BUSHING  ID  0.5000  0.5005  0.5040  0.005  *[1] 
BOLT  OD  0.4990  0.4995  0.4955  X 
2  BEARING  ID  0.4995  0.5000  0.5040  0.005  X 
BOLT  OD  0.4990  0.4995  0.4950  X 
　
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