• 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

 B.  The cabin altitude control module is installed in the P5 overhead panel.
 TASK 21-31-03-004-001
 2.  Cabin Altitude Control Module Removal (Fig. 401)_____________________________________
 A.  References
 (1)  
AIPC 21-31-00 Fig. 05

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
SSM 21-31-01, SSM 21-31-04

 (4)  
WDM 21-31-11, WDM 21-31-21, WDM 21-31-22, WDM 21-31-23


 B.  Access
 (1)  Location Zone
 222 Control Cabin

 C.  Procedure
 S 864-002
 (1)
Open these circuit breakers and attach the DO-NOT-CLOSE tags:

 (a)  
P6 Main Power Distribution Panel
 1) 6L6, CABIN PRESSURE MAN - R
 2) 6L7, CABIN PRESSURE MAN - L


 (b)  
P83 circuit breaker panel in the aft equipment center 1) OUTFLOW VALVE - L 2) OUTFLOW VALVE - R

 

 (2)
Make sure all electrical power is off (AMM 24-22-00/201).

 S 024-021

 (3)  
Loosen the four screws which hold the cabin altitude control module in the P5 panel.

 S 024-022

 (4)  
Disconnect the electrical connector (DM181) from the cabin altitude control module and install caps on the electrical connector.

 (5)  
Remove the cabin altitude control module.


 S 864-015
 S 024-023
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-03
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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


CABIN ALTITUDE CONTROL MODULE, M181


Cabin Altitude Control Module Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-03
 ALL  ú ú 05 Page 402 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F31790
A
747-400 MAINTENANCE MANUAL
 TASK 21-31-03-404-004
 3.  Cabin Altitude Control Module Installation (Fig. 401)__________________________________________
 A. References
 (1)  
AIPC 21-31-00 Fig. 05

 (2)  
AMM 21-31-00/501, Cabin Pressure Control System

 (3)  
AMM 24-22-00/201, Manual Control

 (4)  
SSM 21-31-01, SSM 21-31-04

 (5)  
WDM 21-31-11, WDM 21-31-21, WDM 21-31-22, WDM 21-31-23


 B. Access
 (1)  Location Zone
 222 Control Cabin

 C. Procedure
 S 024-024
 (1)  
Remove the protective caps on the electrical connectors.

 S 424-025

 (2)  
Connect the electrical connector (DM181) to the cabin altitude control module.

 S 414-027

 (3)
Install the cabin altitude control module in the P5 panel.

 S 424-026

 (4)  
Tighten the four screws which hold the cabin altitude control module in the P5 panel.

 S 864-020

 (5)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6 Main Power Distribution Panel
 1) 6L6, CABIN PRESSURE MAN - R
 2) 6L7, CABIN PRESSURE MAN - L


 (b)  
P83 circuit breaker panel in the aft equipment center 1) OUTFLOW VALVE - L 2) OUTFLOW VALVE - R

 


 D. Cabin Altitude Module Operational Test
 S 864-017
 (1)  Supply electrical power (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-03
 ALL  ú ú 02 Page 403 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 714-018
 (2)  Do the CPCS Manual Mode Test:
 (a)  
Make sure the left and right outflow valve operate in manual mode: 1) Push the MAN L or R switch on the cabin altitude control
 
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(119)