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Intercell transfer valves will stay open until the next refuel selection.
FUEL/XFR VALVE 1/WING/L and R C/B’s (A10 and A11 on 49VU), and FUEL/XFR VALVE 2/WING/L
and R C/B’s (M22 and M23 on 121 VU)................................................................................................
..................................................................................................................................................... PULL
The refuel control panel door must be closed when the C/B’s are being pulled. Then it could be
opened for subsequent procedures.
RH WING TANK REFUELING PROCEDURE
OVERWING REFUEL CAP.................................................................................................REMOVE
REFUELING.......................................................................................................................... START
�� If the center tank is to be refueled :
GROUND FUEL TRANSFER PROCEDURE................................................................... APPLY
�� When the wing tank reaches the required level :
* REFUELING....................................................................................................................STOP
* OVERWING REFUEL CAP....................................................................................... INSTALL
LH WING REFUELING PROCEDURE
Perform the steps for RH wing refueling procedure marked * then :
FUEL/XFR VALVE 1/WING/L and R C/B’s (A10 and A11 on 49VU) and FUEL/XFR VALVE 2/WING/L
and R C/B’s (M22 and M23 on 121VU).............................................................................................
.................................................................................................................................................PUSH
MODE SELECT................................................................................................... REFUEL then OFF
Check on FUEL page that the intercell transfer valves close.
Note: The overwing refuel point is not at the highest point of the wing and therefore the wing
tanks cannot be filled to full.
OVERWING GRAVITY REFUELING
Applicable to: ,
, MSN,,
Overwing gravity refueling is done at the refuel point in the top of each wing. Fill center tank by
transfer from the right wing tank (open the X FEED valve in case of transfer from the left wing tank).
SAFETY PRECAUTIONS............................................................................................................APPLY
Disembark all passengers.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 15/38
FCOM 19 AUG 10
Make certain that no HF transmission (including HF transmission via the HF DATA LINK pb) is
performed during refueling and that the tanker and the aircraft are properly grounded. Connect a
tanker grounding cable to the aircraft’s grounding point on the main landing gear. Refer to 99 Duref
Cible AMM for detailed safety procedures.
Note: For APU start/shutdown during refueling, Refer to PER-LOD-FUL APU
START/SHUTDOWN DURING REFUELING/DEFUELING.
RH WING TANK REFUELING PROCEDURE
* OVERWING REFUEL CAP.............................................................................................REMOVE
* REFUELING...................................................................................................................... START
�� If the center tank is to be refueled :
GROUND FUEL TRANSFER PROCEDURE................................................................... APPLY
�� When the wing tank reaches the required level :
* REFUELING....................................................................................................................STOP
* OVERWING REFUEL CAP....................................................................................... INSTALL
LH WING REFUELING PROCEDURE
Perform the steps for RH wing refueling procedure marked * then :
MODE SELECT................................................................................................... REFUEL then OFF
Note: The overwing refuel point is not at the highest point of the wing and therefore the wing
tanks cannot be filled to full.
REFUELING WITH ONE ENGINE RUNNING
Applicable to:
MSN,
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.
　
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