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MAINTENANCE MANUAL
(4) S 144-038Clean the surfaces of the reservoir (17) to make a good electrical bond.
(5) S 624-039Apply corrosion preventive compound to the holes for the bolts in the reservoir.
(6) S 424-040Hold the reservoir (17) on the support bracket.
(7) S 424-041Install the bolts (13), the washers (14, 15) and the nuts (16).
(8) S 434-042Tighten the bolts (13) to 90-125 pound-inches.
(9) S 424-043Install the bolt (1), the washers (2, 3) and the nut (4) to connect the support rod to the reservoir (17).
S 434-044
(10)
Tighten the bolt (1) to 160-240 pound-inches.
S 434-045
(11)
Connect the electrical connectors to these components:
(a)
Fluid quantity transmitter
(b)
Pressure switch
(c)
Temperature transmitter.
S 434-058
(12)
Remove the caps from the hydraulic lines and the openings in the reservoir.
S 434-046
(13)
Connect the hydraulic supply lines and the hydraulic return lines to the reservoir (17).
S 434-047
(14)
Connect the tube to the pressure relief valve.
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MAINTENANCE MANUAL
S 434-048
(15)
Connect the reservoir pressurization line to the reservoir (17).
S 864-049
(16)
Close the drain valve on the reservoir (17).
S 434-050
(17)
Safety the drain valve with a lockwire.
S 614-051
(18)
Fill the reservoir (17) (AMM 12-12-01/301).
S 864-052
(19)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:
(a)
11K16, HYDRAULICS ELEC PUMP RIGHT
(b)
11K20, HYDRAULICS QTY LEFT
(c)
11K21, HYDRAULICS QTY RIGHT
(d)
11K25, HYDRAULICS ELEC PUMP LEFT
(e)
EICAS (6 locations)
S 864-053
(20)
Pressurize the applicable hydraulic system and the reservoir (AMM 29-11-00/201).
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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(235)
