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时间:2011-04-12 10:23来源:蓝天飞行翻译 作者:航空
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 S 434-008
 (3)
If it is necessary, install the nose wheel (AMM 32-45-02/401).

 S 584-009

 (4)  
Remove the jack from the nose gear.


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 32-21-08
 ALL  ú ú 01 Page 403 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 TOW FITTING - INSPECTION/CHECK
______________________________
 1.  General_______
 A.  This procedure contains a task to examine the tow fitting pin and the bushing for worn parts.
 B.  To do this procedure, you must remove the tow fitting.
 TASK 32-21-08-206-001
 2.  The Tow Fitting Pin and the Bushings Inspection (Fig. 601)_______________________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometers, inside and outside measuring.

 B.  
References

 (1)  
32-21-08/401, Tow Fitting

 (2)  
IPC 32-21-08 Fig. 1

 C.  
Access

 (1)  
Location Zone
 715 Nose Landing Gear


 D.  
Procedure


 S 016-002
 (1)
Do this task: "Removal of the Tow Fitting" (Ref 32-21-08/401).

 S 226-003

 (2)
Examine the tow fitting pin and the bushings for worn parts.

 (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 the part is not in tolerance, replace the part if you cannot repair it.

 (3)  
Do this task: "Installation of the Tow Fitting" (Ref 32-21-08/401).


 S 416-006
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 32-21-08
 ALL  ú ú 01 Page 601 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

SEE A
FWD
2. PIN
1. BUSHING (TYPICAL 4 PLACES)
3. BUSHING
A
Tow Fitting Wear Limits
Figure 601 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-21-08
 ALL  ú ú 01 Page 602 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  INSTR REPAIR 
DIAMETER  MITTED WEAR DIM. PER- MAX CLEAR-ANCE DIA 
MIN  MAX 
1  BUSHING  ID  1.3750  1.3800  1.4380  X 

2  PIN  OD  1.7480  1.7490  1.7490  0.0110  X  1 

3  BUSHING  ID  1.755  1.757  1.7590  0.0110  X 

 

PART IS REPAIRABLE. SEE OVERHAUL MANUAL FOR REPAIR INSTRUCTIONS.
Tow Fitting Wear Limits
Figure 601 (Sheet 2)

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 32-21-08
 ALL  ú ú 01 Page 603 ú Oct 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 NOSE LANDING GEAR AXLE SLEEVE - REMOVAL/INSTALLATION
____________________________________________________
 1.  General
_______
 A.  This procedure has two tasks:
 (1)  
The removal of the axle sleeve from the axle for the nose landing gear.

 (2)  
The installation of the axle sleeve on the axle for the nose landing gear.
 
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本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 3(157)