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refueling, do not operate the external lighting.
Make certain that the slats are retracted, and the flight control safety locks with their warning
notices are in position.
Note: For APU start/shutdown during refueling, Refer to PER-LOD-FUL APU
START/SHUTDOWN DURING REFUELING/DEFUELING.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A330/A340 FLEET PER-LOD-FUL P 19/24
FCOM 19 AUG 10
Applicable to: ALL
INNER TANK REFUELING PROCEDURE
OVERWING REFUEL CAP.................................................................................................REMOVE
REFUELING.......................................................................................................................... START
The approximate flowrate per refueling fill is 200 liters/minute.
�� If outer tank to be refueled :
GROUND FUEL TRANSFER PROCEDURE................................................................... APPLY
Note: This procedure is not applicable for trim tank refueling.
REFUELING WITH ONE ENGINE RUNNING
Applicable to:
‐ Refuel with one engine running, only at airports where no external ground pneumatic power is
available, and only when APU is unserviceable.
‐ Only the RH fuel couplings can be used.
‐ Overwing gravity filling is not permitted.
‐ Disembark all passengers.
‐ Obtain airport authorization.
The Airport Fire Department should standby at the aircraft during the entire refueling procedure.
‐ Point the aircraft into the wind, at a location where the slope is negligible.
Set the parking brake and check its pressure.
Run engine 2 at ground idle with its generator connected.
Do not start engine 1, 3, 4, shut down engine 2, or attempt ‐ to start the APU before all fueling
operations have been completed.
‐ Position the fuel truck under the extremity of the right wing. Its pressure should not exceed 50 PSI.
‐ Follow automatic or manual refueling procedure.
Note: The refuel system must be fully operational.
OPERATION MONITORING
DURING THE ENTIRE REFUELING PROCEDURE :
‐ Monitor the fuel truck shut-off valve.
‐ Be sure that the fueling company is keeping permanent control of the emergency fuel shut off
device.
‐ Have a flight crewmember in the cockpit, to monitor all systems and the running engine.
‐ Have a qualified ground crewmember at the fueling station, to operate the refuel valve
switches.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A330/A340 FLEET PER-LOD-FUL P 20/24
FCOM 19 AUG 10
REFUELING WITH ONE ENGINE RUNNING
Applicable to: ,
‐ Refuel with one engine running, only at airports where no external ground pneumatic power is
available, and only when APU is unserviceable.
‐ Only the RH fuel couplings can be used.
‐ Overwing gravity filling is not permitted.
‐ Disembark all passengers.
‐ Obtain airport authorization.
The Airport Fire Department should standby at the aircraft during the entire refueling procedure.
‐ Point the aircraft into the wind, at a location where the slope is negligible.
Set the parking brake and check its pressure.
Run engine n° 1 at ground idle with its generator connected.
‐ Do not start engine n° 2, shut down engine n° 1, or attempt to start the APU before all fueling
operations have been completed.
‐ Position the fuel truck under the extremity of the right wing. Its pressure should not exceed 50 PSI.
‐ Follow automatic or manual refueling procedure.
Note: The refuel system must be fully operational.
OPERATION MONITORING
DURING THE ENTIRE REFUELING PROCEDURE :
‐ Monitor the fuel truck shut-off valve.
‐ Be sure that the fueling company is keeping permanent control of the emergency fuel shut off
device.
Have a flight crewmember in the cockpit, to monitor all ‐ systems and the running engine.
‐ Have a qualified ground crewmember at the fueling station, to operate the refuel valve
switches.
USE OF MANUAL MAGNETIC INDICATORS (MMI)
Applicable to:
Indicators are installed in each wing tank and in the center tank.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A330/A340 FLEET PER-LOD-FUL P 21/24
FCOM 19 AUG 10
AIRCRAFT ATTITUDE..................................................................................................................NOTE
Note the grid square letter and grid square number shown by the bubble on the attitude monitor.
ACCESS PLATFORM.......................................................................................................IN POSITION
MMI..............................................................................................................UNLOCK and WITHDRAW
　
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