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时间:2011-04-15 08:31来源:蓝天飞行翻译 作者:航空
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 (2)  
Measure the part

 (3)  
Compare the dimensions with the correct dimensions in the table.

 (4)  
Install, repair or replace the part.


 TASK 52-36-01-206-001
 2.  Examine the Condition of the Bulk Cargo Door (Fig. 601)____________________________________________
 A.  References
 (1)  
AMM 52-36-00/001, Bulk Cargo Door

 (2)  
AMM 52-36-03/401, Bulk Cargo Door Uplatch Hook

 (3)  
AIPC 52-36-01 Fig. 2, AIPC 52-36-03 Fig. 2, AIPC 52-36-04 Fig. 1

 B.  
Access

 (1)  
Location Zone
 146 Bulk Cargo Compartment, RH


 (2)  
Access Panel
 823R Door - Bulk Cargo Compartment


 C.  
Procedure

 (1)  
Open the bulk cargo door sufficiently for access (AMM 52-36-00/001).

 (2)  
Remove the lining from the bulk cargo door.

 S 216-010

 (3)  
Examine the latch mechanism for corrosion, deterioration and general condition.


 S 016-002
 S 036-003
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-36-01
 ALL  ú ú 01 Page 601 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

B B
SEE C
SEE A
SEE B
A
A
A
FWD
B
Bulk Cargo Wear Limits
Figure 601 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-36-01
 ALL  ú ú 01 Page 602 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

2. INSERT/PROBE  1. BUSHING/PROBE 
A-A  5. BUSHING/BOLT 
4. FITTING/BUSHING  SNUBBER FITTING 
B-B 


3. BUSHING/SPACER 
C  Bulk Cargo Door Wear Limits Figure 601 (Sheet 2)  C-C 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-36-01
 ALL  ú ú 01 Page 603 ú Oct 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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  REPAIR INSTR. 
DIAMETER  WEAR DIM. ALLOWED  DIAM CLEAR-ANCE MAX 
MIN  MAX 
1  BUSHING  ID  1.5015  1.5025  1.512  0.022  X 
PROBE  OD  1.498  1.499  1  X 
2  INSERT  ID  0.225  0.235  2  X 
PROBE  OD  0.838  0.843  1  X 
3  BUSHING  ID  0.261  0.263  0.290  0.080  X 
SPACER  OD  0.240  0.260  0.210  X 
4  FITTING  ID  0.3761  0.3766  0.0000  0.0010  X 
BUSHING  OD  0.3756  0.3761  0.0005  X 
5  BUSHING  ID  0.2500  0.2515  0.0000  0.0030  X 
BOLT  OD  0.2485  0.2495  0.0005  X 


DAMAGE THROUGH THE CHROME LAYER IS NOT SATISFACTORY REPLACE THE INSERT IF IT IS LESS THAN 0.210 INCHES THICK
NOTE:REFER TO OVERHAUL MANUAL 52-36-35 TO REPLACE THE BUSHINGS.
Bulk Cargo Door Wear Limits
Figure 601 (Sheet 3)

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 52-36-01
 ALL  ú ú 01 Page 604 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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