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时间:2011-04-02 16:53来源:蓝天飞行翻译 作者:航空
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CONTROL VALVE  FLOW BRAKE  AUTOBRAKE SHUTTLE VALVES  INBD  FLOW VALVES BRAKE  VALVE CONTROL 
FUSES  FUSES 
INBD  RIGHT ANTISKID 
OUTBD CONTROL VALVES 

WHEEL WELL ACCUMULATOR AFT BULKHEAD SEE A
STA 727
BL 0
VIEW IN THE AFT DIRECTION
PRESSURE
RELIEF VALVE
CHARGING VALVE
PRESSURE GAGE
HYDRAULIC
LINE
FWD INBD
A
Pressure Relief Valve Installation Figure 401
B12697
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 32-41-71
 ALL  ú ú 03 Page 404 ú Mar 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 BRAKE HYDRAULIC FUSES - REMOVAL/INSTALLATION
____________________________________________
 1.  General_______
 A.  This procedure has one task. It is to replace the volumetric hydraulic fuses for the brakes.. There are two fuses for the left normal brake hydraulic system and two fuses for the right normal hydraulic system. There is one fuse for the left alternate brake hydraulic system and one fuse for the right brake alternate system. The fuses are all located in the airplane wheel well (Ref Fig. 401).
 B.  Bleed the brakes after after fuse replacement per instructions in Hydraulic Brake System - Maintenance Practices.
 TASK 32-41-72-004-001
 2.  Volumetric Hydraulic Fuse Replacement_____________________________________
 A.  General
 (1)  
For this procedure the volumetric hydraulic fuses will be referred to as the fuses.

 B.  
References

 (1)  
AMM 20-50-11/201, Standard Torque Values

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

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

 (4)  
AMM 32-41-00/201, Hydraulic Brake System

 C.  
Access

 (1)  
Location Zones
 216 Left Main Landing Gear Door
 217 Right Main Landing Gear Door


 D.  
Procedure (Fig. 401)


 S 024-002
 (1)  
Do the procedure to remove power from all three hydraulic systems (AMM 29-15-00/201).

 S 024-003

 (2)  
Do the procedure to remove the pressure from all three hydraulic reservoirs (AMM 29-09-00/201).

 (3)  
Loosen the two B nuts on the two sides of each fuse.

 (4)  
Remove the fuse.

 (5)  
Install a new fuse.

 S 434-007

 (6)  
Tighten the two B nuts on the two sides of each fuse (AMM 20-50-11/201).


 S 034-004
 S 024-005
 S 424-006
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 32-41-72
 ALL  ú ú 01 Page 401 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
BRAKE FLOW FUSE BRAKE FLOW FUSE

HYDRAULIC SYSTEM) SEE
A
BL 0
VIEW IN THE AFT DIRECTION
Brake Hydraulic Fuses Replacement
Figure 401 (Sheet 1)

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 32-41-72
 ALL  ú
 ú  01  Page 402
 ú  Nov 15/93 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D00128
A

737-300/400/500MAINTENANCE MANUAL
ANTISKID
VALVE

TO BRAKES
FUSES SHOWN) (PNEUDRAULIC FUSE SEE B  FUSES SHOWN) (PNEUDRAULIC BYPASS VALVE LEVER SEE B 
A BRAKE FLOW FUSES (LEFT BRAKE NORMAL HYDRAULIC SYSTEM) 3 
LEVER IN CLOSED POSITION 1 
FUSE  LOCKWIRE  LEVER IN OPEN POSITION  CLOSED POSITION LEVER IN 2  OPEN POSITION LEVER IN 
FLOW  FLOW 
PNEUDRAULIC FUSE  DECOTO FUSE 
B  B 
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 3(35)