S 794-054

 (21)
 Make sure there is no leakage at the connections to the reservoir (17).

 S 114-055
 CAUTION:  QUICKLY CLEAN THE INSTALLATION AREA OF ALL HYDRAULIC FLUID.
_______ HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE AIRPLANE EQUIPMENT.
 (22) Clean all hydraulic fluid from the installation area (AMM 12-25-01/301).
 S 094-056
 WARNING:  USE THE PROCEDURE IN AMM 32-00-15 TO REMOVE THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (23) Remove door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
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757
MAINTENANCE MANUAL

 S 864-057
 (24) Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
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 ALL  ú ú 01 Page 410 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 CENTER SYSTEM HYDRAULIC RESERVOIR - REMOVAL/INSTALLATION
________________________________________________________
 1.  General_______
 A. This procedure has two tasks. One task removes the reservoir in the center hydraulic system. The other task installs the reservoir.
 TASK 29-11-21-004-001
 2.  Remove the Reservoir in the Center Hydraulic System___________________________________________________
 A. References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems

 (3)  
AMM 29-11-22/401, Reservoir Drain Valve

 (4)  
AMM 29-11-23/401, Reservoir Sampling Valve

 (5)  
AMM 29-11-24/401, Reservoir Pressure Relief Valve

 (6)  
AMM 29-11-25/401, Reservoir Manual Depressurization Valve

 (7)  
AMM 29-32-03/401, Reservoir Temperature Transmitter

 (8)  
AMM 29-33-01/401, Hydraulic System Fluid Quantity Transmitter

 (9)  
AMM 29-35-01/401, Hydraulic Reservoir Pressure Switch
　
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