S 434-082
(5)
Safety the pressure switch with a wire.
S 434-083
(6)
Connect the electrical connector to the pressure switch.
J.
Put the Airplane Back to Its Usual Condition
S 864-084
(1)
Push the indicator button, on the differential pressure indicator, until it aligns with the adjacent surface.
S 864-085
(2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:
(a) 11K16, HYDRAULICS ELEC PUMP RIGHT
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(b) 11K25, HYDRAULICS ELEC PUMP LEFT
(3) S 864-086Pressurize the applicable hydraulic system and the reservoir (AMM 29-11-00/201).
(4) S 794-087Make sure there are no leaks at the filter module.
S 114-088
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 614-089
(6)
Fill the reservoir in the applicable hydraulic system (AMM 12-12-01/301)
S 094-090 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.
(7)
Remove door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
S 864-091
(8)
Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
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CENTER SYSTEM ALTERNATING CURRENT MOTOR PUMP (ACMP) PRESSURE AND CASE DRAIN
___________________________________________________________________________ FILTER MODULE AND COMPONENTS - REMOVAL/INSTALLATION
___________________________________________________
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本文鏈接地址：757 AMM 飛機維護手冊 液壓 CHAPTER 29 - HYDRAULIC POWER 1(223)
