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时间:2011-04-14 10:24来源:蓝天飞行翻译 作者:航空
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8.
 NUT

HINGE FAIRING
(FORWARD HINGE FAIRING SHOWN)

B
Aft Cargo Door Figure 402 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

18. CENTER HINGE PINS
17. CENTER HINGE PINS
16.75 INCHES 16. END HINGE PIN  (3 LOCATIONS) 9.06 INCHES  (3 LOCATIONS) 9.06 INCHES  19. END HINGE PINS 16.75 INCHES 
(EXAMPLE) (REF) HINGE FAIRINGS 
FORWARD/AFT CENTER HINGES SEE C 
FWD  A-A 
29. BOLT  30. BOLT  29. BOLT  31. HINGE HALF 
23. BOLT  24. BOLT 23. BOLT  32. SHIM 

HALF 27. SHIM 28. HINGE  FWD  INBD  (9 LOCATIONS) 33. WASHER (9 LOCATIONS) 34. NUT 
25. NUT (8 LOCATIONS)26. WASHER (8 LOCATIONS)  AFT CENTER HINGE 
FORWARD CENTER HINGE 

Aft Cargo Door
Figure 402 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 014-053
 CAUTION:_______ IN CASE THE DOOR DOES NOT OPEN, STOP IMMEDIATELY.  DO NOT
 OPERATE THE DOOR CONTROL SWITCH.  HOLDING THE DOOR CONTROL
 SWITCH MAY DAMAGE THE ACTUATOR.  WAIT AT LEAST 1 MINUTE BEFORE
 SECOND ATTEMPT.  IF THE DOOR STILL DOES NOT OPEN, WAIT AT LEAST

 10 MINUTES BEFORE THIRD ATTEMPT.
 (2)  
Open the cargo door sufficiently to get access to the cargo compartment.

 S 034-004

 (3)  
Remove the cargo door junction box (AMM 52-34-05/401).

 S 034-005

 (4)  
Remove the upper and lower door lining.

 S 034-006

 (5)  
Remove the swivel clamp (8) from the door support fitting (9) (Fig. 403).

 S 034-007

 (6)  
Remove the rain seal from the cargo door (AMM 52-09-03/401).

 S 494-008

 (7)  
Install the cargo door sling and apply sufficient tension to release the door hinges of the door weight (Fig. 404).

 S 034-009

 (8)  
Disconnect the links (View D, Fig. 405) which extend from each rotary actuator arm to the door support fittings.

 S 014-010

 (9)  
Remove the doorway ceiling panel (AMM 25-52-01/401).

 S 034-011

 (10)
 Remove the hinge pins (Fig. 401, Fig. 402).

 (a)  
Remove the fasteners that attach the third and fourth center hinge sections on the forward end of the door.


 NOTE: Identify the shims with a tag for the installation
____ procedure. You must install the shims in the same position.
 On the aft cargo door, remove the fifth and sixth center hinge sections from the forward end of the door.
 (b)  Install the bolt in the end hinge pin (16 and 19) to remove the end hinge pin.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

WIRE BUNDLE 
FLEXIBLE 
CONDUIT 
SEE  A 
2. LINK 
3. ROTARY 
ACTUATOR 
ARM 
1. DOOR 
2. LINK 
4. SWIVEL 
CLAMP 
8. SWIVEL 
CLAMP 
FITTING SUPPORT 9. DOOR  9. FITTING SUPPORT DOOR  5. NUT 6. WASHER 7. SCREW 
8. SWIVEL  4. SWIVEL  3. ROTARY 
CLAMP  CLAMP  ACTUATOR  1. DOOR 
7. SCREW  ARM 
6. WASHER  WIRE BUNDLE 
5. NUT  FLEXIBLE CONDUIT  DOOR CLOSED 
 
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