S 024-021
 S 024-023
 S 034-018
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-28-07
 ALL  ú ú 01 Page 401 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

FORWARD BULKHEAD LINING
FWD
FORWARD RIGHT
SIDEWALL AREA

SEE A
AFT CARGO DOOR
AFT CARGO COMPARTMENT 
CEILING 
LINING 
CONDITIONED AIR 
CHECK VALVE 
SEE  B 
FORWARD 
BULKHEAD 
LINING 

FWD
FORWARD RIGHT SIDEWALL AREA (AFT CARGO COMPARTMENT)
A
Aft Cargo Compartment Conditioned Air Check Valve - Installation
Figure 401 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-28-07
 ALL  ú ú 01 Page 402 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F27709
A
747-400
MAINTENANCE MANUAL

CONDITIONED AIR CHECK VALVE

RING

A-A

Aft Cargo Compartment Conditioned Air Check Valve - Installation
Figure 401 (Sheet 2)

F27755
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-28-07
 ALL  ú ú 01 Page 403 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 TASK 21-28-07-404-002
 3. Conditioned Air Check Valve Installation (Fig. 401)
________________________________________
 A. References
 (1)  
AIPC 21-28-00 Fig. 12

 (2)  
AMM 21-00-00/201, Air Conditioning

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

 (4)  
AMM 25-52-01/401, Containerized Cargo Compartment Ceiling and Sidewall Lining

 (5)  
AMM 36-00-00/201, Pneumatic Power.

 B. Access
 (1)  Location Zone
 142 Aft Cargo Compartment, RH

 C. Procedure
 S 024-004
 (1)  Remove the covers from the ducts.
 (a)  Make sure that there is no unwanted materials in the ducts.
 S 284-007
 (2)
Make sure the flappers in the check valve can move easily.

 S 424-024

 (3)  
Put the check valve in the sleeve.

 (a)  
Make sure the air flow arrow points in the aft direction.

 (b)  
Make sure that the hinge pin is in the vertical position.

 S 424-025
 (4)  Install the coupling and the clamp at each end of the check valve.
 (a)  Tighten the coupling nuts to 60-70 pound-inches(8 newton meters).
 D. Installation test for the Check Valve
 S 864-017
 (1)  
Supply electrical power (AMM 24-22-00/201).

 (2)  
Apply pneumatic pressure (AMM 36-00-00/201).

 S 864-011

 (3)  
Remove the DO-NOT-CLOSE tags and turn the pack 3 switch on P5 overhead panel to ON (AMM 21-00-00/201).

 (4)  
Turn the pack flow switch on P461 panel to HI.

 S 864-012
 S 864-013
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-28-07
 ALL  ú ú 01 Page 404 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 794-008
 (5)  Make sure there is no leak around the check valve.
 (a)  If there is air leakage, adjust the check valve to the clamp and coupling connections.
 S 864-027
 (6)  Turn the pack flow switch to OFF.
　
中國航空網 www.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 AIR CONDITIONING 1(87)