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 NOTE: For access to the filter, the trailing edge flaps must be
____ extended a minimum of 10 units. Also, the inboard ground spoiler must be in the full up position.
 S 862-055
 WARNING: MAKE SURE TO ATTACH DO-NOT-OPERATE TAGS ON THE CONTROL LEVERS
_______ AND SWITCHES. THIS IS TO PREVENT ACCIDENTAL OPERATION OF THE CONTROL SURFACES WHICH CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  
Attach DO-NOT-OPERATE tags to the FLAP and SPEED BRAKE levers, and the ALTERNATE FLAPS, SPOILER A and B switches.

 S 862-054

 (3)  
Remove hydraulic power from systems A and B (AMM 29-15-00/201).

 S 862-003

 (4)  
Release pressure from the hydraulic reservoirs (AMM 29-09-00/201).

 S 032-005

 (5)  
Disconnect the hydraulic lines from the case drain filter.

 (6)  
Drain the hydraulic fluid into a container.

 S 162-007

 (7)  
Clean all hydraulic fluid from the installation area if it is necessary (AMM 12-40-00/201).

 (8)  
Install caps on the hydraulic lines.

 (9)  
Remove the mounting bolts.

 S 682-006
 S 432-008
 S 032-009
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 022-010
 (10) Remove the case drain filter.
 TASK 29-15-91-402-011
 5. EDP Case Drain Filter Installation (Fig. 201)
__________________________________
 A. Consumable Materials
 (1)  
D00567 Skydrol Assembly Lube - MCS 352

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

 B. References
 (1)  AMM 71-00-00/201, Power Plant
 C. Access
 (1)  Location Zone 309 Wing Trailing Edge Inboard Flap and Spoilers, LH 409 Wing Trailing Edge Inboard Flap and Spoilers, RH
 D. Procedure
 S 642-013
 (1) Apply assembly lube or hydraulic fluid to the union and O-rings.
 S 422-049
 CAUTION: MAKE SURE YOU INSTALL THE CHECK VALVE IN THE "OUT" PORT , AND
_______ THE ARROW ON THE CHECK VALVE MATCHES THE ARROW ON THE FILTER HEAD. FAILURE TO DO THIS CAN CAUSE DAMAGE TO THE EDP.
 (2)  Install the union, check valve and O-rings in the case drain filter ports.
 S 422-050
 CAUTION: MAKE SURE THE ARROW ON THE FILTER HEAD WILL POINT INBOARD.
_______ FAILURE TO DO THIS CAN CAUSE DAMAGE TO THE EDP.
 (3)  
Put the case drain filter on the mounting bracket.

 (4)  
Install the bolts.

 (5)  
Remove the caps from the hydraulic lines.

 (6)  
Connect the hydraulic lines to the case drain filter.

 (7)
Motor the engine-driven hydraulic pump (AMM 71-00-00/201).

 S 432-018
 S 032-019
 S 432-020
 S 862-021
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 792-014
 (8) Examine the filter and connections for leaks.
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 29-15-91
 ALL  ú ú 01 Page 208 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 EDP SUPPLY SHUTOFF VALVE - REMOVAL/INSTALLATION
_______________________________________________
 1.  General_______
 A.  Supply shutoff valves for the hydraulic fluid are installed in the supply lines to each engine-driven pump (EDP). The supply shutoff valves (referred to as the valves) are mounted in the rear spar area immediately outboard of the wheel wells. A container of about 4.5-gallon capacity will be necessary to catch fluid when removing the valve.
　
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 液壓 HYDRAULIC POWER(126)