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时间:2011-04-02 15:00来源:蓝天飞行翻译 作者:航空
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___________________________________________________________
 1.  General
_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of the hydraulic systems A and B reservoirs.
 TASK 29-15-41-004-001
 2.  Hydraulic Systems A and B Reservoirs Removal (Fig. 401)
____________________________________________
 A.  Standard Tools and Equipment
 (1)  
Container to hold hydaulic fluid

 (2)  
Regulated source of nitrogen - 0 to 200-psi maximum pressure


 B.  References
 (1)  
12-40-00/201, Cleaning and Washing

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

 (3)  
29-15-00/201, Hydraulic Systems A, B and Standby

 (4)  
29-33-12/401, Hydraulic Fluid Quantity Transmitter Indicator


 C.  Access
 (1)  Location Zone
 216/217 Main Wheel Well

 D.  Prepare for Removal (Fig. 401)
 S 864-006
 (1)  
Remove hydraulic power (Ref 29-15-00/201).

 S 934-007

 (2)  
Put the DO-NOT-OPERATE tags on the applicable hydraulic system pump switches.

 S 864-008

 (3)  
Release pressure from the hydraulic reservoir (Ref 29-09-00/201).

 (4)  
Open the drain valve.


 S 034-014
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 29-15-41
 ALL  ú ú 01 Page 401 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

HYDRAULIC 
SYSTEM 
SEE  A 
SYSTEM A 
RESERVOIR 
SEE  B  RESERVOIR 
PRESSURIZATION 
MODULE 
SYSTEM B 
RESERVOIR 
SEE  C 

FWD
HYDRAULIC SYSTEM A
Hydraulic Systems A and B Reservoir Removal/Installation
Figure 401 (Sheet 1)

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 29-15-41
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
CLAMP 
MOUNTING BOLT 
(EXAMPLE)  LINE FROM THE RESERVOIR 
PRESSURIZATION MODULE 

CLAMP BOLT FOR THE RESERVOIR PRESSURE LINE (EXAMPLE)RETURN AND FILL LINE MOUNTING BOLT FOR THE DRAIN VALVE
DRAIN VALVE (4 LOCATIONS)
EMDP SUPPLY LINE
EDP SUPPLY LINE
SYSTEM A RESERVOIR B
PRESSURE RELIEF VALVE
CLAMP BOLT FOR THE RESERVOIR PRESSURE LINE (EXAMPLE)
MOUNTING BOLT
(EXAMPLE)
LINE FROM THE RESERVOIR PRESSURIZATION MODULE
FILL LINE
RETURN LINE MOUNTING BOLT FOR THE DRAIN VALVE (4 LOCATIONS)
DRAIN VALVE EMDP SUPPLY LINE
EDP SUPPLY LINE
PTU SUPPLY LINE
SYSTEM B RESERVOIR C
Hydraulic Systems A and B Reservoir Removal/Installation Figure 401 (Sheet 2)
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 29-15-41
 ALL  ú ú 01 Page 403 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 684-009
 (5)  
Drain the fluid from the reservoir into a container.

 S 164-016

 (6)  
Clean all hydraulic fluid from the installation area if it is necessary (Ref 12-40-00/201).


 E. Procedure
 S 024-003
 (1)  Remove the hydraulic reservoir:
 (a)  
Disconnect the reservoir pressurization line and clamp.

 (b)  
Disconnect the hydraulic lines from the reservoir.

 (c)  
Install protective covers on the fittings and the hoses.

 (d)  
Disconnect the electrical connector from the fluid quantity transmitter.
 
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