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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757
MAINTENANCE MANUAL
S 864-094
(8) Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
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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本文链接地址：757 AMM 飞机维护手册 液压 CHAPTER 29 - HYDRAULIC POWER 1(216)
