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时间:2011-10-11 13:08来源:蓝天飞行翻译 作者:航空
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 S 794-021

 (4)  
Make sure there are no leaks at the relief valve.


 S 114-022
 CAUTION: QUICKLY CLEAN THE INSTALLATION AREA OF ALL HYDRAULIC FLUID.
_______ HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE AIRPLANE EQUIPMENT.
 (5)  Clean all hydraulic fluid from the installation area
 (AMM 12-25-01/301).

 S 094-023
 WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (6)  
Remove door locks from the landing gear doors and close the doors (AMM 32-00-15/201).

 (7)
Remove hydraulic power if it is not necessary (AMM 29-11-00/201).


 S 864-024
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-29
 ALL  ú ú 02 Page 404 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 RESERVOIR PRESSURIZATION CHECK VALVE - ADJUSTMENT/TEST
______________________________________________________
 1.  General_______
 A.  There is one task in this subject. This task is a reservoir
 pressurization check valve test.

 TASK 29-11-30-705-001
 2.  Reservoir Pressurization Check Valve Test_________________________________________
 A.  General
 (1)  This procedure does a test of the check valves which keep air pressure in the hydraulic system reservoirs after the pneumatic power is removed. This is a test of each main hydraulic system.
 B.  Equipment
 (1)  
Air pressure gage - 0 to 100 psi range -commercially available


 (2)  
A source of clean, dry air or nitrogen, that is
 controlled from 0 to 100 psi maximum pressure -commercially available

 

 C.  References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 24-22-00/201, Electrical Power - Control

 (3)  
AMM 36-00-00/201, Pneumatic Control


 D.  Access
 (1)  
Location Zone
 139 Forward Keel Beam
 193/194 Wing to Body Fairings
 212 Control Cabin


 (2)  
Access Panels 193HL/194ER Environmental Control System Components


 E.  Procedure (Fig. 501)
 S 865-008
 (1)  Supply electrical power (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-30
 ALL  ú ú 01 Page 501 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

SEE  A 
FILTER 
PRESSURE  SUPPORT 
GAGE PORT  BRACKET 
FWD 
PNEUMATIC 
SUPPLY LINE 
PRESSURIZATION RESERVOIR  MANUAL  (2 LOCATIONS) 
LINE  BLEED VALVE 
(3 LOCATIONS) 
RESERVOIR PRESSURIZATION MODULE 

MOISTURE 
VENT TRAP 
CHARGING 
VALVE  VENT 
MOISTURE VENT TRAP  DEPRESSURIZATION VALVE MODULE 
 
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