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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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EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú ú 01 Page 402 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

16. LATCH ACTUATOR
21.
 MOUNTING BOLT

22.
 WASHER

23.
 NUT (4 LOCATIONS)


DOOR RIB
SHIM
17. SUPPORT BRACKET
OUTBD
LATCH ACTUATOR SUPPORT
A-A

15. BEARING 27. WASHER 9. CLAMP
26. NUT
6. CLAMP
24. NUT
24.
 NUT


25.
 WASHER

25. WASHER  28. WASHER 30. BOLT
29. BOLT
13. TORQUE TUBE 31. WASHER
31. WASHER
5. ADAPTER
30. BOLT
8. CLAMP TORQUE TUBE CLAMP
B C
Latch Actuator
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú ú 01 Page 403 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 3) 414F16 CARGO DOOR CONTROL AFT
 S 014-004
 (3)  
Remove the lower door lining (1).

 S 034-005

 (4)  
Disconnect the electrical cable (2) at connector P2 from the latch actuator (16).

 S 034-006

 (5)  
Disconnect and remove the adjacent latch mechanism parts to permit the removal of the latch actuator (16) as follows (Fig. 401):

 (a)  
Disconnect the pushrod (14) from the bellcrank (7).

 (b)  
Remove clamps (8)(9) that hold the bellcrank (7), torque tube (13), and double-throw bellcrank (10).

 (c)  
Pull clamps (8)(9) from the torque tube (13).

 (d)  
Remove the torque tube.

 CAUTION:_______BE CAREFUL WHEN YOU REMOVE THE BELLCRANK (7). THE SPLINED TEETH OF THE BELLCRANK CAN CAUSE DAMAGE TO THE FACE OF THE BEARING (15), IF YOU ARE NOT CAREFUL.

 (e)  
Remove the clamp (6) that holds the bellcrank (7) and adapter (5).

 (f)  
Pull the bellcrank in the aft direction to permit clearance for the adapter.

 (g)  
Remove the adapter (5) from the latch actuator (16).


 S 024-007
 (6)  
Remove the four bolts (21)(View A-A, Fig. 401) that hold the latch actuator (16) to the support bracket (17).

 S 824-030

 (7)  
Pull the latch actuator in the aft direction until it is clear of the bellcrank (4).


 NOTE: Make sure you do not move the shims.
____
 TASK 52-34-06-404-008
 3.  Latch Actuator - Installation_____________________________
 A. Standard Tools and Equipment
 (1)  
Bonding Meter (Ref 20-22-01/601)

 B.
Consumable Materials

 (1)  
D00013 Grease - MIL-G-23827


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú ú 02 Page 404 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 C. Parts
 (1)  FORWARD CARGO DOOR;
 Refer to table that follows:

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 5 |Adapter | 52-34-06 | 01 | 495 | | | 6 |Clamp | | | 195 | | | 7 |Bellcrank | | | 465 | | | 8 |Clamp | | | 195 | | | 9 |Clamp | | | 170 | | | 13 |Torque Tube | | | 440 | | | 16 |Actuator (Latch Actuator) | | | 390 | | | 21 |Bolt (Mounting Bolt) | | | 350 | | | 22 |Washer | | | 355 | | | 23 |Nut | | | 360 | | | 24 |Nut | | | 215 | | | 25 |Washer | | | 210 | | | 26 |Nut | | | 190 | | | 27 |Washer | | | 185 | | | 28 |Washer | | | 180 | | | 29 |Bolt | | | 175 | | | 30 |Bolt | | | 200 | | | 31 |Washer | | | 205 | 2......…........…...................................…..........…......…........1
 
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