EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-02
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

 (b)  
Select <SHOP FAULTS from the other functions menu.

 (c)  
Select <21 CABIN PRESSURE from the shop faults menu.

 (d)  
Select <CPCS-A or <CPCS-B for the left or the right cabin pressure controller.

 (e)  
Make a record of the shop faults that are shown.

 D. Controller Removal
 S 864-002
 (1)  
For controller A, open the circuit breaker 6J28 CABIN PRESS AUTO A on the P6 Main Power Distribution Panel.

 S 864-003

 (2)  
For controller B, open the circuit breaker 6J29 CABIN PRESS AUTO B on the P6 Main Power Distribution Panel.

 S 024-004

 (3)  
Remove the controller from the electronics shelf (AMM 20-11-22/401).

 TASK 21-31-02-404-005
 3. Cabin Pressure Controller Installation
______________________________________
 A. References
 (1)  
AMM 20-11-22/401, Rack-Mounted Electrical/Electronic Module

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

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

 (4)  
AIPC 21-31-02, Fig. 10

 (5)  
WDM 21-31-11, WDM 21-31-12

 (6)  
SSM 21-31-01, SSM 21-31-03

 B. Access
 (1)  Location Zone
 117 Electrical/Electronics Compartment, LH
 118 Electrical/Electronics Compartment, RH

 C. Procedure
 S 424-006
 (1)  
Install the controller in the electronics shelf (AMM 20-11-22/401).

 S 434-007

 (2)  
If installed, remove the protective cover from the pressure sense port on the controller.

 (3)  
Apply electrical power (AMM 24-22-00/201).

 (4)
Make sure the air/ground relay system is in the ground mode.

 S 864-008
 S 864-009
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-02
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
 S 744-010
 CAUTION:_______ MAKE SURE THERE IS NO BLOCKAGE IN THE VALVE FLAPPER DOORS.
 THE AUTOMATIC MOVEMENT OF THE VALVES DURING THE GROUND TEST
 CAN CAUSE DAMAGE IF THE VALVE FLAPPER DOORS ARE NOT FREE TO

 MOVE.
 (5)  Do a ground test of the cabin pressure control system (CPCS) on a CMC CDU (AMM 21-31-00/501):
 (a)  
Make sure the AUTO SELECT switch on the P5 overhead panel is set to NORM.

 (b)  
Make sure the MAN L/MAN R switches on the P5 overhead panel are set to off.

 (c)  
Select <GROUND TEST from the CMC main menu.

 (d)  
Select <21 CABIN PRESSURE from the air conditioning menu.

 (e)  
For a test of the A controller, select <CPCS-A.

 (f)  
For a test of the B controller, select <CPCS-B.

 (g)  
Make sure that IN PROGRESS shows on the CMC CDU.

 (h)  
Make sure that PASS shows on the CMC CDU.

 S 864-011
 (6)  Remove electrical power (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-31-02
 ALL  ú ú 01 Page 404 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 CABIN ALTITUDE CONTROL MODULE - REMOVAL/INSTALLATION
____________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. The first task is the removal of the cabin altitude control module (M181). The second task is the installation of the cabin altitude control module.
　
中國航空網(wǎng) 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 空調(diào) AIR CONDITIONING 1(118)