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时间:2011-04-02 05:45来源:蓝天飞行翻译 作者:航空
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 (1)  
Location Zone
 101 Control Cabin, LH
 216 Main Wheel Well, LH
 102 Control Cabin, RH
 217 Main Wheel Well, RH


 C.
Reset the Hydraulic Fuse (Standby System)


 S 864-016
 (1)
Make sure the flap control lever is in the FLAP UP detent.

 S 864-017

 (2)  
Do this task to depressurize the standby hydraulic system: "Leading Edge Flaps and Slats Hydraulic Systems A, B and Standby Depressurization" (Ref 27-81-00/201).


 NOTE: The fuse will reset (gets open) automatically when
____ hydraulic pressure on both sides of the fuse is equalized within 5 psi for ten seconds.
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 27-81-61
 ALL  ú ú 02 Page 405 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LEADING EDGE FLAP FLOW LIMITING VALVE - REMOVAL/INSTALLATION
____________________________________________________________
 1.  General
_______
 A.  There are three tasks in this procedure. There is a task for the removal and a task for the installation of the leading edge flap flow-limiting valve (referred to as the flow-limiting valve). The third task is a test of the flow-limiting valve.
 TASK 27-81-71-004-001
 2.  Leading Edge Flap Flow Limiting Valve Removal
_____________________________________________
 A.  References
 (1)  
27-81-00/201, Leading Edge Flap and Slat Control System

 B.  
Access

 (1)  
Location Zone
 216 Main Wheel Well, LH


 C.  
Procedure


 S 864-002
 (1)  
Release the pressure from the hydraulic systems (Ref 27-81-00/201).

 S 034-004

 (2)  
Disconnect the inlet and outlet hydraulic lines from the flow-limiting valve.

 S 024-003

 (3)  
Remove the flow-limiting valve (Fig. 401).##


 NOTE: If both the flow-limiting valve and the hydraulic fuse are
____ being removed, make a note of their locations before removing them.
 TASK 27-81-71-404-005
 3.  Leading Edge Flap Flow-Limiting Valve Installation
__________________________________________________
 A.  Consumable Materials
 (1)  
D00196 Fluid - Hydraulic, BMS 3-11

 (2)  
D00567 Lubricant - Skydrol Assembly Lube


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 27-81-71
 ALL  ú ú 02 Page 401 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

SEE A
(REF) HYDRAULIC RESERVOIR 
LEADING EDGE FLAP VALVE FLOW-LIMITING 
LEADING EDGE FLAP AND SLAT HYDRAULIC FUSE (REF) 
FWD  HYDRAULIC PUMP (REF) 
A STANDBY SYSTEM 

Leading Edge Flap Flow Limiting Valve
Figure 401

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 27-81-71
 ALL  ú ú 02 Page 402 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F40698
A
737-300/400/500MAINTENANCE MANUAL
 B. References
 (1)  
12-12-00/301, Hydraulic Reservoir

 C.
Access

 (1)  
Location Zone
 216 Main Wheel Well, LH


 D.
Procedure


 S 034-024
 (1)
Remove the reducer from each end of the flow-limiting valve.

 S 644-026

 (2)
Lubricate the O-rings with hydraulic fluid or the assembly lube.

 S 434-027

 (3)  
Install the O-rings.

 S 864-022

 (4)  
Put the flow-limiting valve in its position.

 (a)  
 
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