S 653-079
(3)
Release the deadman switch to stop the fuel flow.
S 653-080
(4)
Make sure the onboard fuel load is in a valid pre-flight fuel distribution.
S 653-081
(5)
Transfer fuel to balance the fuel load if necessary (AMM 28-26-00/201).
S 653-082
(6)
Wait for one minute to let the FQIS system stabilize.
S 653-083
(7)
Record the actual fuel quantities from the fuel quantity indicators.
S 653-084
(8)
Record the actual fuel quantity from the fuel vehicle flow meter.
S 653-085
(9)
Do the discrepancy check and make sure it is within limits.
NOTE: Per operator's procedures.
____
S 653-086
(10)
Complete the Fuel Sheet.
(11)
Complete the Delivery Receipt if necessary.
S 653-087
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747-400 MAINTENANCE MANUAL
S 653-088
(12) Give a copy of the forms to the airline representative or flight crew.
J. Put the Airplane Back to the Usual Condition
S 653-089
(1)
Put the manual handle for the FUELING SHUTOFF VALVE to the CLOSED position (left and right wing).
S 653-091
(2)
Make sure all the P42 panel valve switches are in the CLOSED position.
S 653-092
(3)
Put the POWER switch to the NORM position (if necessary).
S 653-093
(4)
If the airplane battery power was used, set the BATTERY switch to the OFF position.
S 653-094
(5)
Disconnect the refuel nozzle from the airplane.
S 653-095
(6)
Remove the refuel nozzle bonding cable (if installed).
S 653-096
(7)
Make sure the defuel lever is correctly positioned in the recess for the refuel receptacle adapter.
(8)
Make sure the receptacle adapter is not damaged.
(9)
Install the refuel receptacle cap.
S 653-097
S 653-098
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747-400 MAINTENANCE MANUAL
S 653-099
(10)
Repeat the steps for each fuel hose.
S 413-100
(11)
Close and security latch these doors:
(a)
Fueling station access door, 521BB and 621BB
(b)
Fueling control panel access door, 521CB.
S 083-101
(12)
Disconnect the bonding/grounding cables (AMM 20-41-01/201).
S 653-102
(13)
Do the operator supplied procedures to remove the fuel vehicle.
S 083-103
WARNING: DO THE PROCEDURE IN AMM 27-81-00/201 TO REACTIVATE THE EXTENDED
_______ LEADING EDGE FLAPS. THE FLAPS MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(14)
Do this task for extended leading edge flaps: Safety Locks Removal and Extended Leading Edge Activation (AMM 27-81-00/201).
(15)
Remove the tail support equipment (AMM 07-11-08/201) (if installed).
S 083-104
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A
747-400 MAINTENANCE MANUAL
OVERWING REFUELING - SERVICING
中国航空网 www.aero.cn
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本文链接地址：747-400 AMM 飞机维护手册 SERVICING 1(16)
