(b)  
Connect connector DM0709B on the forward door (or DM0711B on aft door) to receptacle J2.

 (c)  
Connect connector P3 to receptacle J3.

 (d)  
Connect connector P4 to receptacle J4.

 S 864-010
 (3)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers for the applicable cargo door:

 (a)  
P59 Aft Equipment Panel
 1) AFT CARGO DOOR POWER UNITS

 (b)  
P414 Power Distribution Center-Left
 1) 414A21 LOWER CARGO DOOR FWD
 2) 414F15 CARGO DOOR CONTROL FWD
 3) 414F16 CARGO DOOR CONTROL AFT

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-05
 ALL  ú ú 01 Page 403 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 414-011
 (4) Close the cargo door.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-05
 ALL  ú ú 01 Page 404 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 LATCH ACTUATOR - REMOVAL/INSTALLATION
_____________________________________
 1.  General_______
 A. This procedure contains two tasks:
 (1)  
The first task is the removal of the latch actuator from the lower lobe cargo door.

 (2)  
The second task is the installation of the latch actuator on the lower lobe cargo door.

 TASK 52-34-06-004-001
 2.  Latch Actuator - Removal________________________
 A. References
 (1)  
52-34-00/001, Forward/Aft Cargo Door

 (2)  
AIPC 52-34-06 Fig. 1, AIPC 52-34-06 Fig. 2

 (3)  
SSM 52-34-01, 52-35-01

 (4)  
WDM 52-34-11, 52-35-11

 B.
Access

 (1)  
Location Zone 122 Forward Cargo Container Compartment, Forward Half 142 Aft Cargo Container Compartment

 (2)  
Access Panel
 821R Door - Forward Cargo Compartment
 822R Door - Aft Cargo Compartment

 C.
Procedure

 S 014-035
 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.
 (1)  Open the cargo door sufficiently to get access to the cargo compartment.
 NOTE: Open the cargo door manually if electrical power is off.
____ Bypass the jammed latch actuator if it is necessary (Ref 52-34-00/001).
 S 864-003
 (2)  
Open these circuit breakers for the applicable cargo door and attach DO-NOT-CLOSE tags:

 (a)  
P59 Aft Equipment Panel
 1) AFT CARGO DOOR POWER UNITS

 (b)  
P414 Power Distribution Panel Center - Left 1) 414A21 LOWER CARGO DOOR FWD 2) 414F15 CARGO DOOR CONTROL FWD

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-34-06
 ALL  ú ú 01 Page 401 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

3. LATCH MECHANISM SEE A
2. WIRE TO THE LATCH ACTUATOR
1. LOWER DOOR
LINING

7. BELLCRANK
6. CLAMP
4. BELLCRANK 8. CLAMP
SEE C
20. PUSHROD 5. ADAPTER  9. CLAMP
RIGGING PIN HOLE
11. PUSHROD
A
10. BELLCRANK
RIGGING PIN HOLE
19. PUSHRODS  12. PUSHRODS
18. PUSHROD
16. LATCH
13. TORQUE TUBE
LOWER LATCH A ACTUATOR
FWD 17. SUPPORT

(EXAMPLE) 14. PUSHROD SEE B BRACKET 15. BEARING
LATCH MECHANISM
A

Latch Actuator
Figure 401 (Sheet 1)
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 艙門 DOORS 3(70)