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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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 TASK 29-15-51-004-040
 2.  Standby Hydraulic System Reservoir Removal (Fig. 401)__________________________________________
 A.  Special Tools and Equipment
 (1)  B29002-5 - Reservoir Depressurization Valve Lock
 B.  Standard Tools and Equipment
 (1)  
Container to catch hydraulic fluid (approx 5 gal. capacity).

 (2)  
Quick disconnect coupling half P/N 375530-12 with approx. 18 inch of hose


 C.  References
 (1)  29-09-00/201, Hydraulic Reservoir Pressurization System
 D.  Access
 (1)  Location Zone
 101 Control Cabin, LH
 102 Control Cabin, RH
 215 Keel Beam

 E.  Prepare for the Removal
 S 864-002
 (1)  
Release pressure from the system B hydraulic reservoir (Ref 29-09-00/201).

 S 494-037

 (2)  
Install the reservoir depressurization valve lock on the depressurization valve to the open position.

 (3)
Put the FLT CONTROL A and B switches on the P5 panel to OFF.

 (4)  
Attach DO-NOT-OPERATE tags on the FLT CONTROL switches.


 S 864-003
 S 934-004
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 29-15-51
 ALL  ú ú 02 Page 401 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
DEPRESSURIZATION VALVE FOR 
THE SYSTEM B RESERVOIR 
DEPRESSURIZATION VALVE FOR 
FILL LINE  THE SYSTEM A RESERVOIR 
BALANCE LINE 
STANDBY RESERVOIR 
SEE  B 
RETURN LINE 
SUPPLY LINE FOR 
THE STANDBY EMDP 

STANDBY EMDP
A

Standby Hydraulic System Reservoir Removal/Installation
Figure 401 (Sheet 1)

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 29-15-51
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

(EXAMPLE)
STANDBY RESERVOIR

Standby Hydraulic System Reservoir Removal/Installation
Figure 401 (Sheet 2)

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 29-15-51
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 024-044
 CAUTION: MAKE SURE THAT YOU PULL DOWN ON THE KNURLED RING OF THE
_______ SELF-SEAL DISCONNECT BEFORE YOU TURN IT FOR REMOVAL. IF YOU DO NOT DO THIS, TOO MUCH TORQUE WILL BE NECESSARY TO TURN THE RING WHICH WILL DAMAGE THE SELF-SEAL DISCONNECT.
 (5)  
Remove the supply line for the standby hydraulic pump at the quick-disconnect at the bottom of the standby hydraulic reservoir.

 S 434-005

 (6)  
Put the hose, with the quick-disconnect coupling half installed, into a container.

 S 684-007

 (7)  
Drain the fluid into the container.

 S 164-008

 (8)  
If you get hydraulic fluid on the airplane, clean it off immediately (Ref 12-12-00/301).

 S 434-038

 (9)  
Connect the quick-disconnect on the hose to the quick-disconnect on the bottom of the standby reservoir.


 F. Procedure
 S 024-039
 (1)  Remove the standby reservoir:
 (a)  
Disconnect the balance line to the system B reservoir.

 (b)  
Install a protective cap.

 (c)  
Disconnect the return line.

 (d)  
Install a protective cap.

 (e)  
Disconnect the fill line.

 (f)  
Install a protective cap.

 (g)  
Remove the electrical connector and the low quantity switch.

 (h)  
Remove the fasteners that attach the standby reservoir to the mounting bracket.
 
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