NOTE: This will remove the pressure from the refuel/jettison
____ manifold. The blue indication lights for the refuel valves in the No. 2 and No. 3 main tanks will come on if the refuel/jettison manifold pressure is more than 6 psig and the refuel valve is operational.
 1)  If a blue indication light did not come on, it is possible that the refuel valve did not operate electrically. a) Use the manual method to open the applicable refuel
 valve(s) (AMM 12-11-01/301). b) Wait for 5 minutes. c) Close the refuel valve(s) that were opened manually
 (AMM 12-11-01/301).
 (g)  
After the blue indication lights for the refuel valves go off, wait for 5 minutes.

 (h)
Put the refuel valve switches, MAIN 2 and MAIN 3, to the CLOSED position.

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 S 714-020
 (9)  
Set the nozzle valve switch on the fuel jettison module to the ON position.

 S 214-039

 (10)
 Make sure the manual override lever moves to the OPEN position.

 S 714-021

 (11)
 Set the nozzle valve switch to the OFF position.

 S 214-040

 (12)
 Make sure the manual override lever moves to the CLOSED position.

 E.
Put the Airplane Back to Its Usual Condition

 S 414-022
 (1)  
Install the wingtip dry bay access door, 556AB or 656AB.

 S 414-051

 (2)  
Close access door 521CB if access to the refuel control panel, P42, is not needed.

 S 864-049
 WARNING:_______DO THE PROCEDURE IN AMM 27-81-00/201 TO REMOVE THE LOCKS. THE FLAPS MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (3)  Remove the leading edge flap safety locks, if installed
 (AMM 27-81-00/201).

 S 864-050
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING
_______ EDGE AND TRAILING EDGE FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER.
 (4)
Retract the leading edge flaps, if extended (AMM 27-81-00/201).

 S 864-035

 (5)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
On the left power distribution center, P414:
 1) 414C5, FUEL OVRD/JTSN PUMP FWD 3
 2) 414C2, FUEL OVRD/JTSN PUMP FWD 2
 3) 414D2, OVRD/JTSN PUMP CTR L

 (b)  
On the right power distribution center, P415: 1) 415A38, FUEL OVRD/JTSN PUMP AFT 2 2) 415B38, FUEL OVRD/JTSN PUMP AFT 3 3) 415M32, OVRD/JTSN PUMP CTR R

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 S 864-023
 (6) Remove electrical power, if it is not necessary (AMM 24-22-00/201).
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747-400 MAINTENANCE MANUAL
 FUEL JETTISON TRANSFER VALVE ACTUATOR - REMOVAL/INSTALLATION
____________________________________________________________
 1.  General_______
 A.  This procedure contains instructions to remove and install the actuator of a fuel jettison transfer valve. There are different tasks for the actuators in the center wing tank and the inboard main tank installations.
 B.  Access to the actuators is through the wheel well in the wing landing gear. No access door/panel removal is necessary.
　
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