(23)
Safety the electrical connectors (1, 2) with a lockwire.
S 864-042
(24)
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 864-043
(25)
Pressurize the applicable hydraulic system and the reservoir with the ACMP's (AMM 29-11-00/201).
S 794-044
(26)
Make sure there are no leaks at the hydraulic connections while the hydraulic pump (28) is in operation.
S 114-045
CAUTION: QUICKLY CLEAN THE INSTALLATION AREA OF ALL HYDRAULIC
_______ FLUID. HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE AIRPLANE EQUIPMENT.
(27) Clean all hydraulic fluid from the installation area (AMM 12-25-01/301).
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S 614-046
(28) Fill the applicable hydraulic reservoir (AMM 12-12-01/301).
S 094-047 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.
(29)
Remove door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
S 864-048
(30)
Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
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CENTER SYSTEM ALTERNATING CURRENT MOTOR PUMP (ACMP) - REMOVAL/INSTALLATION
__________________________________________________________________________
1. General_______
A. This procedure contains two tasks. One task removes the alternating current motor pumps for the center system. The other task installs the alternating current motor pumps for the center system.
NOTE: If the ACMP is being replaced, you will be required to replace
____ only the pressure and case drain filters associated with the ACMP, (P1F and CD1F or P2F and CD2F), as marked on the filter module case. Do not replace the filters due to external pump leakage alone.
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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(179)
