S 424-032
(16)
Install the bolts (24) and the washers (25).
S 644-033
(17)
Apply hydraulic lubricant or hydraulic fluid to the threads of the fittings on the hydraulic lines.
S 434-034
(18)
Connect the hydraulic lines (10, 13) to the pump (28).
S 644-046
(19)
Apply a thin layer of hydraulic lubricant or hydraulic fluid to the surfaces which make a seal on the self seal coupler (7).
(20)
Connect the supply hose (6) at the self-seal coupler.
S 434-035
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757 MAINTENANCE MANUAL
S 434-036
(21)
Connect the electrical connectors (1, 2) to the pump (28).
S 434-037
(22)
Safety the electrical connectors (1, 2) with a lockwire.
S 864-038
(23)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:
(a)
11K15, HYDRAULICS ELEC PUMP C1
(b)
11K24, HYDRAULICS ELEC PUMP C2
S 864-039
(24)
Pressurize the center hydraulic system and the reservoir with the ACMPs (AMM 29-11-00/201).
S 794-040
(25)
Make sure there are no leaks at the hydraulic line connections while the pump (28) is in operation.
S 864-041
(26)
Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
S 114-042
(27)
Clean all hydraulic fluid from the installation area (AMM 12-25-01/301).
S 414-043
(28)
If you removed the ACMP access panel, 197ML, install this panel (AMM 06-41-00/201, 53-66-01/401
CAUTION:_______ QUICKLY CLEAN THE INSTALLATION AREA OF ALL HYDRAULIC
FLUID. HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE AIRPLANE
EQUIPMENT.
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