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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757 MAINTENANCE MANUAL
　
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