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时间:2011-04-12 10:27来源:蓝天飞行翻译 作者:航空
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 S 226-007
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 32-32-08
 ALL  ú ú 01 Page 601 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
SEE B
UPLOCK ACTUATOR
SEQUENCE VALVE ACTUATOR ROD
SEE C
SEE A
UPLOCK ROLLER 
2.53 2.52 
1  (0.010 MAX THICK) THE HARD CHROME PLATE FOR REPAIR, YOU CAN FULL WIDTH ALL AROUND WHERE THE HOOK TOUCHES THE ROLLER  HOOK A 1 
Wing Gear Uplock Wear Limits Figure 601 (Sheet 1) 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-08
 ALL  ú ú 01 Page 602 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 

NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  WORN PART REPLACE  PART WORN REPAIR  INSTR. REPAIR 
DIAMETER  DIM. ALLOWED WEAR 2  MAX ANCE CLEAR-DIAM 
MIN  MAX 
1  BUSHING  ID  0.4995  0.5000  0.5040  0.0050  X 
PIN  OD  0.4980  0.4990  0.4950  X 
2  BUSHING  ID  0.4370  0.4375  0.4410  0.0040  X 
BOLT  OD  0.4360  0.4370  0.4335  X 
3  HOOK  ID  2.520  2.530  2.570  0.080  X 
ROLLER  OD  2.490  2.510  2.470  X 


THE PART DIMENSION CAN BE MORE THAN THE LIMITS SHOWN BUT NOT MORE THAN THE MAXIMUM CLEARANCE.
Wing Gear Uplock Wear Limits
Figure 601 (Sheet 2)

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 32-32-08
 ALL  ú ú 01 Page 603 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 226-008
 (4)  
Compare these dimensions to the limit dimensions.

 S 966-006

 (5)  
If the part is not in tolerance, repair or replace the part.

 S 226-005

 (6)  
Examine these parts for rust and corrosion:

 (a)  
The uplock hook and the roller

 (b)  
The rod end bolt and bushing of the actuator

 (c)  
The head end bolt and bushing of the actuator.


 S 426-003
 (7)  Install the uplock actuator on the uplock mechanism (Ref 32-32-08/401).
 TASK 32-32-08-206-009
 3.  Inspection of the Uplock Mechanism for the Wing Landing Gear____________________________________________________________
 NOTE: This is a scheduled maintenance task.
____
 A. Procedure
 S 216-010
 (1)  
Examine these parts for rust and corrosion:

 (a)  
The uplock hook and the roller

 (b)  
The rod end bolt and bushing of the actuator

 (c)  
The head end bolt and bushing of the actuator.


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 32-32-08
 ALL  ú ú 01 Page 604 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WING LANDING GEAR UPLOCK HOOK - REMOVAL/INSTALLATION
____________________________________________________
 1. General
_______
 A. This procedure has these two tasks:
 (1)  
Uplock Hook Removal

 (2)  
Uplock Hook Installation.


 TASK 32-32-09-004-042
 2. Wing Landing Gear Uplock Hook Removal (Fig. 401)
_____________________________________
 
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本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 4(87)