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on 121VU)......................................................................................................................................
.......................................................................................... PULL for a minimum of 5 s then PUSH
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
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 13/38
FCOM 19 AUG 10
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. Fuel is delivered directly
into the outer cell from which the inner cell is filled by opening the intercell transfer valves. 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.
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.
TRANSFER VALVES (on ECAM FUEL page)........................................................ CHECK POSITION
If transfer valves closed :
MODE SELECT (on the refuel control panel)............................................................... Check OFF
FUEL/XFR VALVE 1/WING/L C/B (A10 on 49VU) and FUEL/XFR VALVE 2/WING/L C/B (M22 on
121VU)............................................................................................................................................
.......................................................................................... PULL for a minimum of 5 s then PUSH
The refuel control panel door must be closed when the C/B’s are being pulled.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 14/38
FCOM 19 AUG 10
FUEL/XFR VALVE 1/WING/R C/B (A11 on 49VU) and FUEL/XFR VALVE 2/WING/R C/B (M23
on 121VU)......................................................................................................................................
.......................................................................................... PULL for a minimum of 5 s then PUSH
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(103)
