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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 29-31-12-004-001
 2.  System Pressure Transmitter Removal (Fig. 401)___________________________________
 A.  References
 (1)  
29-09-00/201, Hydraulic Reservoir Pressurization System

 (2)  
29-15-00/201, Hydraulic Systems A, B and Standby


 B.  Access
 (1)  Location Zone
 216 Main Wheel Well, LH
 217 Main Wheel Well, RH

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

 S 864-003

 (2)  
Remove power from the applicable hydraulic system
 (Ref 29-15-00/201).


 S 864-004

 (3)  
Open the applicable circuit breakers and attach DO-NOT-CLOSE tags:


 (a)  P6-2 Circuit Breaker Panel
 1) PRESS IND SYS A

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 29-31-12
 ALL  ú ú 01 Page 401 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500MAINTENANCE MANUAL
SYSTEM A
RESERVOIR

PRESSURE TRANSMITTER FOR SYSTEM A
SEE A FWD
FORWARD BULKHEAD (REF) 
SYSTEM A  OF THE LEFT WHEEL WELL 
PRESSURE MODULE 
(REF)  SYSTEM A 
RETURN FILTER 
(REF)  SYSTEM A IS SHOWN 

(SYSTEM B IS IN THE RIGHT WHEEL WELL)
PRESSURE CLAMP
TRANSMITTER ELECTRICALRESTRICTOR CONNECTORO-RING
HYDRAULIC LINE
CLAMP CUSHION
SCREW (2 PLACES)
PRESSURE TRANSMITTER A
Hydraulic Systems A and B Pressure Transmitter Installation
Figure 401

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 29-31-12
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
 2) PRESS IND SYS B
 S 034-005
 (4)
Remove the connector plug from the pressure transmitter.

 S 034-006

 (5)
Disconnect the hydraulic line at the pressure transmitter.

 S 034-008

 (6)
Remove the mounting bolts, washers, and clamp.

 S 024-007

 (7)
Remove the pressure transmitter.


 TASK 29-31-12-404-009
 3.  System Pressure Transmitter Installation (Fig. 401)________________________________________
 A. Consumable Materials
 (1)
D00567 Skydrol Assembly Lube - MCS 352

 (2)
D00568 Fluid - Hydraulic, BMS 3-11


 B. References
 (1)
24-22-00/201, Manual Control

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

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


 C. Access
 (1)  Location Zone
 216 Main Wheel Well, LH
 217 Main Wheel Well, RH

 D. Procedure
 S 644-011
 (1)
Apply assembly lube or hydraulic fluid to the O-ring and restrictor.

 (2)
Install the O-ring and restrictor in the transmitter port.


 S 434-024
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 29-31-12
 ALL  ú ú 01 Page 403 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (3)  S 434-012Put the clamp on the pressure transmitter.
 (4)  S 424-013Put the pressure transmitter on the mounting holes.
 (5)  S 434-014Install the mounting bolts and washers.
 NOTE:____ Do not tighten the mounting bolts.
 (6)  S 434-015Connect the hydraulic line from the modular unit to the pressure transmitter.
 (7)  S 434-016Tighten the mounting bolts.
 (8)  S 434-017Connect the electrical connector to the pressure transmitter.
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 液压 HYDRAULIC POWER(151)