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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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 (7)  S 862-055Supply electrical power (Ref 24-22-00/201).
 (8)  S 862-056Remove the DO-NOT-CLOSE tags and close these circuit breakers: (a) P6-11 Circuit Breaker Panel 1) STBY HYD PUMP NORMAL (b) P6-12 Circuit Breaker Panel 1) STBY HYD PUMP (ALT)

 S 862-057
 (9) Put one of these switches on the P5 panel to the specified position:
 (a)
The FLT CONTROL A switch to STDBY RUD

 (b)
The FLT CONTROL B switch to STDBY RUD

 (c)
The ALTERNATE FLAPS arm switch to ARM


 S 792-058
 (10)
 Examine the relief valve for leaks.

 S 862-059

 (11)
 Put the FLIGHT CONTROL A or B switch to ON or the ALTERNATE FLAPS arm switch to OFF.

 S 612-060

 (12)
 Do the servicing for system B and the standby hydraulic reservoirs (Ref 12-12-00/301).

 S 862-061

 (13)
 Remove electrical power (Ref 24-22-00/201).


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 29-15-81
 ALL  ú ú 01 Page 211 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 EDP CASE DRAIN FILTER - MAINTENANCE PRACTICES
_____________________________________________
 1.  General
_______
 A.  There are four tasks in this procedure. There is a task for the removal and a task for the installation of the EDP case drain filter element. There is also a task for the removal and a task for the installation of the EDP case drain filter.
 TASK 29-15-91-002-002
 2.  EDP Case Drain Filter Element Removal
_____________________________________
 A.  References
 (1)  
AMM 29-09-00/201, Hydraulic Reservoir Pressurization System

 (2)  
AMM 29-15-11/401, Hydraulic System A and B Engine-Driven Pump (VICKERS EDP).


 B.  Access
 (1)  Location Zone 309 Wing Trailing Edge Inboard Flap and Spoilers, LH 409 Wing Trailing Edge Inboard Flap and Spoilers, RH
 C.  Procedure
 S 862-045
 (1)  Get access to the case drain filter.
 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 862-046
 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.
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 29-15-91
 ALL  ú ú 03 Page 201 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL


CASE DRAIN FILTER FOR THE SYSTEM A EDP

SPOILER HINGE (REF)
TUBE (REF)
FLAP DRIVE TORQUE

SEE


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 29-15-91
 ALL  ú ú 01 Page 202 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

OUT
IN
CASE DRAIN FILTER (SYSTEM A IS SHOWN, SYSTEM B IS OPPOSITE)


EDP Case Drain Filter
Figure 201 (Sheet 2)

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 29-15-91
 ALL  ú ú 01 Page 203 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 862-047
 (3)
Remove hydraulic power from systems A and B (AMM 29-15-00/201).
 
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