S 865-392
 (54)
 Remove the DO-NOT-CLOSE tag and close this circuit breaker on the overhead circuit breaker panel, P11:

 (a)
11A20, AFT FUEL CROSSFEED

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 S 215-393
 (55)
 Make sure the FUEL XFEED VALVE - AFT switch-light goes off.

 S 215-394

 (56)
 Make sure the EICAS message AFT FUEL X-FEED does not show on the EICAS display.

 S 435-395

 (57)
 Install the electrical connector (D1828) to the pressure switch on the right override pump, installed on the rear spar at RBL 13.

 S 865-411

 (58)
 Push the FUEL XFEED VALVE - FWD switch-light on the P5 panel to the off position.

 S 215-410

 (59)
 Make sure the FUEL XFEED VALVE - FWD switch-light on the P5 panel comes on while the valve moves to the closed position for 6 seconds and then goes off.

 S 865-434

 (60)
 Push the FUEL XFEED VALVE - AFT switch-light on the P5 panel to the off position.

 S 215-398

 (61)
 Make sure the FUEL XFEED VALVE - AFT switch-light on the P5 panel comes on while the valve moves to the closed position for 6 seconds and then goes off.

 S 865-399

 (62)
 Open these circuit breakers on the P11 panel:

 (a)
11A19, FWD FUEL CROSSFEED

 (b)
11A20, AFT FUEL CROSSFEED

 (c)
11D36, FUEL XFEED IND

 F.  
Test the Fuel Boost Pumps and Fuel Override Pumps (WET) - Control and Indication

 (1)
Supply the electrical power to the airplane (AMM 24-22-00/201).

 S 655-034
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MAINTENANCE MANUAL

 (2)  S 615-481Refuel the center or main fuel tanks (AMM 12-11-01/301).
 (3)  S 655-487Make sure there is a minimum fuel quantity of 2000 pounds (900 kilograms) in the applicable main fuel tanks.
 (4)  S 655-483Make sure there is a minimum fuel quantity of 20,000 pounds (9,000 kilograms) in the center wing tank.
　
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