• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 15:00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.  If you get hydraulic fluid on the airplane, clean it off immediately (Ref 12-40-00/201).
 TASK 29-15-94-004-001
 2.  EDP Supply Shutoff Valve Removal (Fig. 401)________________________________
 A.  References
 (1)  
12-40-00/201, Cleaning and Washing

 (2)  
29-09-00/201, Hydraulic Reservoir Pressurization System


 B.  Procedure
 S 864-002
 (1)  Release the pressure from the applicable reservoir
 (Ref 29-09-00/201).

 NOTE:____The system A reservoir is connected to the No. 1 engine. The system B reservoir is connected to the No. 2 engine.
 S 684-003
 (2)  Drain the applicable reservoir.
 (a)  
When the hydraulic fluid has drained, close the drain valve.

 (b)  
Install a lockwire on the drain valve.


 S 864-004
 (3)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  P6-2 circuit breaker panel
 1) HYD SOV ENG NO. 1
 2) HYD SOV ENG NO. 2


 (4)
Disconnect the electrical connector from the shutoff valve.

 S 024-005

 (5)  
Remove the bolts from the adapter flanges that are on the sides of the valve.

 (6)  
Pull the valve out from between the adapter flanges.


 S 034-008
 S 024-006
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-15-94
 ALL  ú ú 01 Page 401 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SUPPLY 
SHUTOFF 
VALVE 
ASEE  BOLT, 
WASHER, 
NUT 
(4 LOCATIONS) 
ADAPTER 
FLANGE, 
O-RING 
FROM THE 
RESERVOIR 
SUPPLY 
SHUTOFF 
VALVE 
ELECTRICAL 
CONNECTOR 
TO THE ENGINE 
DRIVEN PUMP 
FWD 
OUTBD 

SUPPLY SHUTOFF VALVE FOR ENGINE 1
(THE VALVE FOR ENGINE 2 IS ALMOST THE SAME)

A

EDP Supply Shutoff Valve Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-15-94
 ALL  ú ú 01 Page 402 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 TASK 29-15-94-404-007
 3.  EDP Supply Shutoff Valve Installation (Fig. 401)_____________________________________
 A. References
 (1)  
12-12-00/301, Hydraulic Reservoir

 (2)  
12-40-00/201, Cleaning and Washing

 (3)  
24-22-00/201, Manual Control

 (4)  
29-09-00/201, hydraulic Reservoir


 B. Procedure
 S 644-009
 (1)  
Lubricate the O-rings with hydraulic fluid and put them in their position on the valve.

 S 424-010

 (2)  
Carefully put the valve between the adapter flanges.


 (a)  Make sure the O-rings do not get damaged or out of their position when you install the valve.
 S 424-020
 (3)  
Install the bolts to the adapter flanges.

 S 434-011

 (4)  
Connect the electrical connector to the valve.

 S 614-012

 (5)
Fill the applicable hydraulic reservoir (Ref 12-12-00/301).

 S 864-013

 (6)  
Pressurize the applicable reservoir (Ref 29-09-00/201).

 S 864-014

 (7)  
Supply electrical power (Ref 24-22-00/201).

 S 864-015

 (8)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:


 (a)  P6-2 circuit breaker panel
 1) HYD SOV ENG NO. 1
 2) HYD SOV ENG NO. 2

 S 864-016
 CAUTION:_______DO NOT TURN THE FIRE HANDLE. IF YOU TURN THE FIRE HANDLE THE FIRE BOTTLE WILL RELEASE ITS CONTENTS.
 (9)  Push the override button behind the fire handle for the applicable engine and pull the handle (on the P-8 panel).
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 液压 HYDRAULIC POWER(127)