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时间:2011-04-13 08:10来源:蓝天飞行翻译 作者:航空
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 S 412-020

 (10) Close the applicable access door (AMM 06-09-03/201).

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 36-11-07
 ALL  ú ú 01 Page 204 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WING ISOLATION VALVE - REMOVAL/INSTALLATION
___________________________________________
 1.  General
_______
 A.  This gives procedures for these tasks:
 (1)  
The removal of the wing isolation valve

 (2)  
The installation of the wing insolation valve.


 NOTE: This task contains a leak test of the valve after its
____
 installation.

 (3)  
An operational check of the wing isolation valve.

 (4)  
A visual check of the wing isolation valves.

 B.  
The two isolation valves are installed in the pneumatic manifold aft of the air-conditioning bay. It is necessary to open the applicable air-conditioning access door to get access to the valves.

 C.  
It is necessary to remove the pack no. 1 water separator to get access to the left wing isolation valve.


 TASK 36-11-07-004-001
 2.  Wing Isolation Valve Removal (Fig. 401)
____________________________
 A.  References
 (1)  
AMM 06-09-03/201, Body Section 44 Access Doors and Panels

 (2)  
AMM 21-51-05/201, Water Separator

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

 (4)  
AMM 36-00-00/201, Pneumatic System

 B.  
Access

 (1)  
Location Zone 191 Fairing, Wing To Body, Forward Lower Half, LH 192 Fairing, Wing To Body, Forward Lower Half, RH

 (2)  
Access Panel
 191NL Air-Conditioning Access Door
 192NR Air-Conditioning Access Door


 C.  
Procedure

 (1)  
Supply the electrical power (AMM 24-22-00/201).

 (2)
Release the pressure in the pneumatic system (AMM 36-00-00/201).

 S 864-004

 (3)  
Put the opposite wing ISLN switch (P5 Pilots' Overhead Panel) in the closed position.


 S 864-002
 S 864-003
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 ALL  ú ú 01 Page 401 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

PACK NO. 1 
LEFT WING  WATER SEPARATOR 
ISOLATION 
VALVE 
AIR CONDITIONING 
PACKS  SEE  B 
SEE  A 

RIGHT WING ISOLATION VALVE
SEE B FWD
AIR CONDITIONING PACKS
CLAMP
A
(2 LOCATIONS) BONDING JUMPER
FLOW DIRECTION INDICATOR
1
ELECTRICALDUCT CONNECTOR
OUTBD FWD
LEFT WING ISOLATION VALVE IS SHOWN (RIGHT WING ISOLATION VALVE IS SIMILAR)
1 ON RIGHT WING ISOLATION
VALVE, FLOW DIRECTION  B
INDICATOR POINTS INBOARD.
Wing Isolation Valve Installation
Figure 401

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 ALL  ú ú 01 Page 402 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (4)  S 864-035Put the ISLN switch for the valve that you will remove in the open position.
 (5)  S 864-005Put the APU VALVE switch in the closed position.
 S 864-006

 WARNING: YOU MUST RELEASE THE PRESSURE IN THE DUCT BEFORE YOU REMOVE A
_______ PNEUMATIC SYSTEM COMPONENT. HIGH PRESSURE AIR CAN CAUSE INJURY TO PERSONS.
 (6)  
Open the wing anti-ice valves to release the pressure in the pneumatic ducts (AMM 36-00-00/201).

 S 014-007

 (7)  
Open the access door 192NR for the right isolation valve or 191NL for the left isolation valve (AMM 06-09-03/201).
 
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