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747-400 MAINTENANCE MANUAL
 2)  Do the continuity/resistance checks again for the new fuel
 pump. 3) Start with this procedure: Fuel Pump Continuity Check. 4) Record the continuity/resistance values for the replacement
 pump on the 747 Fuel Pump Inspection Data Sheet -Replacement Pump (Figure 603).
 (c)  If any resistance measured between pin 4 and pins 1, 2, and 3 is between 1 an 5 megohm, do these steps: 1) It is recommended that the motor/impeller unit be replaced.
 NOTE: Refer to Table 602 for the applicable AMM reference
____
 procedure.

 2)  If the motor/impeller unit is not replaced, continue to do the insulation resistance checks.
 NOTE: Do the checks of the fuel pumps at the maintenance
____ interval in SB 747-28A2194, Revision 1 (every A-check).
 S 766-051
 (4)  
Continue to do the visual and insulation resistance checks for the remaining fuel pumps.

 S 976-059

 (5)  
Keep the 747 Fuel Pump Inspection Data Sheet for your records (Fig. 602, 603, and 604).

 NOTE: It is not necessary to send the data sheets to Boeing.
____
 K.  Put the Airplane Back to the Usual Condition
 S 086-025
 (1)  
Remove the plywood sheet (platform) from the pressure relief panel on the inboard leading edge.

 (2)
Go out of and close the applicable access door, 511FB or 611FB.

 S 416-026
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747-400 MAINTENANCE MANUAL
 S 096-027
 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 (AMM 27-81-00/201).
 S 866-036
 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 necessary (AMM 27-81-00/201).
 S 096-029
 WARNING:_______DO THE PROCEDURE IN AMM 32-00-30/201 TO REMOVE THE LOCKS. THE DOORS MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (5)  
Remove the wing and body gear door locks (AMM 32-00-30/201).

 S 866-035

 (6)  
Close these circuit breakers and remove DO-NOT-CLOSE tags:

 (a)  
P414 Power Distribution Center - Left
 1) 414A8 FUEL BOOST PUMP MAIN FWD 4
 2) 414B5 FUEL BOOST PUMP MAIN AFT 1
 3) 414C2 FUEL OVRD/JTSN PUMP FWD 2
 4) 414C5 FUEL OVRD/JTSN PUMP FWD 3
 5) 414D2 FUEL OVRD/JTSN PUMP CTR LEFT
 6) 414J5 FUEL BOOST PUMP MAIN FWD 3
 7) 414R18 FUEL BOOST PUMP MAIN AFT 2

 (b)  
P415 Power Distribution Center - Right
 1) 415B35 FUEL BOOST PUMP MAIN FWD 1
 2) 415A35 FUEL BOOST PUMP MAIN AFT 4
 3) 415M32 FUEL OVRD/JTSN PUMP CTR RIGHT

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747-400 MAINTENANCE MANUAL
 4) 415A38 FUEL OVRD/JTSN PUMP AFT 2
 5) 415B38 FUEL OVRD/JTSN PUMP AFT 3
 6) 415M29 FUEL BOOST PUMP MAIN AFT 3
 7) 415G29 FUEL BOOST PUMP MAIN FWD 2
　
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