S 434-078

 (7)  
Safety the check valve with a lockwire.

 J.
Put the Airplane Back to Its Usual Condition

 S 864-084
 (1)  Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:
 (a)  
11K16, HYDRAULICS ELEC PUMP RIGHT

 (b)  
11K25, HYDRAULICS ELEC PUMP LEFT

 S 614-085
 (2)  
Fill the reservoir in the applicable hydraulic system
 (AMM 12-12-01/301).

 S 864-086

 (3)  
Pressurize the applicable hydraulic system and the reservoir (AMM 29-11-00/201).

 S 794-087

 (4)  
Make sure there are no leaks at the filter module.

 S 164-088
 CAUTION: QUICKLY CLEAN THE INSTALLATION AREA OF ALL HYDRAULIC FLUID.
_______ THE HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE AIRPLANE EQUIPMENT.
 (5)  
Clean all the hydraulic fluid from the installation area
 (AMM 12-25-01/301).

 S 414-089

 (6)  
Close the applicable access panel for the hydraulic bay in the aft strut (AMM 06-43-00/201).

 S 444-093

 (7)  
Do this procedure: Thrust reverser activation procedure
 (AMM 78-31-00/201).

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A

757
MAINTENANCE MANUAL

 S 864-094
 (8) Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 LEFT AND RIGHT SYSTEM ALTERNATING CURRENT MOTOR PUMP (ACMP) PRESSURE AND CASE
_____________________________________________________________________________ DRAIN FILTER MODULE AND COMPONENTS - REMOVAL/INSTALLATION
_________________________________________________________
 1.  General_______
　
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