• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-06 23:15来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 Verify that both outflow valves remain in the open position.

 S 035-118

 (13)
 Remove the ICU altitude switch breakout box:


 (a)  Open these circuit breakers:
 1)  P6 Main Power Distribution Panel a) 6L6, CABIN PRESS MAN L b) 6L7, CABIN PRESS MAN R c) 6J28, CABIN PRESS AUTO A d) 6J29, CABIN PRESS AUTO B e) 6J30, CABIN PRESS ICU CONT L f) 6J31, CABIN PRESS ICU CONT R
 2)  P414 Left Power Distribution Center a) 414M8, CABIN PRESS ICU L b) 414B8, CABIN PRESS ICU R
 (b)  
Remove the ICU altitude switch breakout box from the ICU's and the connectors DM7950B and DM7951B.

 (c)  
Install connector DM7950B on the left ICU and DM7951B on the right ICU.


 F.  Put the Airplane Back to its Usual Condition
 S 865-119
 (1)  Close these circuit breakers:
 (a)  P6 Main Power Distribution Panel
 1) 6L6, CABIN PRESS MAN L
 2) 6L7, CABIN PRESS MAN R
 3) 6J28, CABIN PRESS AUTO A
 4) 6J29, CABIN PRESS AUTO B
 5) 6J30, CABIN PRESS ICU CONT L
 6) 6J31, CABIN PRESS ICU CONT R

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-00
 ALL  ú ú 04 Page 521 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  P414 Left Power Distribution Center
 1) 414M8, CABIN PRESS ICU L
 2) 414B8, CABIN PRESS ICU R

 S 865-120
 (2)  Remove the electrical power, if it is not necessary (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-00
 ALL  ú ú 05 Page 522 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 PRESSURIZATION OUTFLOW VALVE - REMOVAL/INSTALLATION
___________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the left and the right pressurization outflow valves. The procedure has these parts:
 (1)  
The removal of power to the valves

 (2)  
The removal of the access panel from the aft bulkhead of the bulk cargo compartment

 (3)  
The removal of the valve

 (4)  
The installation of the valve

 (5)  
A test of the valve.


 B.  For the replacement of the outflow valve actuator assembly (ac motor, dc motor and gear housing), refer to AMM 21-31-07/401. For the replacement of the ac motor, refer to AMM 21-31-06/401. For the replacement of the dc motor, refer to AMM 21-31-08/401.
 TASK 21-31-01-004-001
 2.  Pressurization Outflow Valve Removal (Fig. 401)____________________________________
 A.  Standard Tools and Equipment
 (1)  Knife, plastic (nonmetallic)
 B.  References
 (1)  AIPC 21-31-01, Fig. 2
ACCESS DOOR

Pressurization Outflow Valve Installation
Figure 401 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-01
 ALL  ú ú 01 Page 401 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

3. DC MOTOR 
CONNECTOR 
DC MOTOR  4. AC MOTOR 
CONNECTOR 
2. SCREEN  AC MOTOR 
5. POTENTIOMETER 
CONNECTOR 
POSITION 
POTENTIOMETER 
SEE  B 
7. SCREW 
8. WASHER 
9. NUT 
1. OUTFLOW 
VALVE 
ASSEMBLY  6. BONDING JUMPER 
(2 LOCATIONS)  10. BOLT 
A  GEAR CASE  11. WASHER 
LAMINATED SHIM 
(2 LOCATIONS) 
BRACKET 

SEALANT 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 空调 AIR CONDITIONING 1(112)