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时间:2011-04-06 23:15来源:蓝天飞行翻译 作者:航空
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 (a)  
P6 Main Power Distribution Panel
 1) 6J28 CABIN PRESS AUTO A
 2) 6J29 CABIN PRESS AUTO B
 3) 6J30 CABIN PRESS CONT L ICU
 4) 6J31 CABIN PRESS CONT R ICU
 5) 6L6 CABIN PRESS MAN L
 6) 6L7 CABIN PRESS MAN R


 (b)  
P414 Main Power Distribution panel
 1) 414M8 CABIN PRESS ICU LEFT
 2) 414B8 CABIN PRESS ICU RIGHT


 (c)  
P83 in aft equipment center
 1) OUTFLOW VALVE-R
 2) OUTFLOW VALVE-L

 

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 21-31-07
 ALL  ú ú 01 Page 401 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
ACCESS DOOR
SEEA
SAFETY
SCREEN

DC MOTOR
GEAR CASE HOUSING
LEVER ARM
CONNECTING
ROD BOLT

CONNECTING ROD
GATE FRAME
A
AC MOTOR
POSITION
POTENTIOMETER
CONNECTOR

BOLT (2 LOCATIONS) WASHER (2 LOCATIONS) LAMINATED SHIM BOLT (3 LOCATIONS) BRACKET
Pressurization Outflow Valve Actuator Assembly Installation
Figure 401

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 21-31-07
 ALL  ú ú 01 Page 402 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 014-003
 (2)  
Remove the access panel from the aft bulkhead of the bulk cargo compartment to get access to the outflow valves.

 S 034-004

 (3)  
Remove the safety screen.

 S 034-005

 (4)  
Remove the electrical connectors from the outflow valve:

 (a)  
The DC motor electrical connectors DV90C-right or DV91C-left

 (b)  
The AC motor electrical connector DV90A-right or DV91A-left

 (c)  
The position potentiometer electrical connector DV90B - right or DV91B - left.

 


 S 034-007
 (5)  
Remove the connecting rod bolt.

 S 034-008

 (6)
Remove the bolt that holds the actuator to the gate frame.

 S 034-009

 (7)
Remove the bolt that holds the gearcase housing to the bracket.

 S 024-010

 (8)  
Remove the outflow valve actuator assembly. Make sure the laminated shims stay in their position on the bracket.


 TASK 21-31-07-404-011
 3.  Pressurization Outflow Valve Actuator Installation__________________________________________________
 A. References
 (1)  
AMM 21-31-00/501, Cabin Pressure Control System

 (2)  
24-22-00/201, Manual Control

 (3)  
IPC 21-31-01 Fig. 1

 (4)  
WDM 21-31-13, 21-31-21, 21-31-22

 (5)  
SSM 21-31-02, 21-31-04


 B. Access
 (1)  Location Zone
 151 Area Aft of Bulk Cargo Compartment, LH
 152 Area Aft of Bulk Cargo COmpartment, RH

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 21-31-07
 ALL  ú ú 01 Page 403 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 C. Procedure
 S 434-024
 (1)
Make sure the laminated shim is in its position on the bracket.

 S 424-012

 (2)  
Put the actuator in its position on the valve frame and install the bolts and washers. Do not tighten the bolts.


 NOTE:____The shim is permanently bonded to the structure. Adjustment of the shim is not necessary.
 S 434-013
 (3)  
Install the bolts that hold the actuator to the frame, and tighten all the bolts.

 S 434-014

 (4)
Install the connecting rod bolt, washers, nut and cotter pin.
 
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