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REFUEL VALVES.......................................................................................NORM and GUARDED
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 11/38
FCOM 19 AUG 10
Set cockpit FUEL panel to normal configuration.
DEFUELING
Applicable to: ,
, MSN,,
Note: Defueling by suction is not possible. Fuel can be removed from wing tank only. To defuel
center tank, first transfer fuel to the wing tanks.
ACCESS PLATFORM.......................................................................................................IN POSITION
SAFETY PRECAUTIONS............................................................................................................APPLY
Make certain that no HF transmission (including HF transmission via the HF DATA LINK pb) is
performed during defueling and that the tanker and the aircraft are properly grounded.
Connect the tanker ground cable to the parking ground point before connecting it to a grounding
point on the aircraft. In the cockpit, check that the PARK BRK is ON and that the ACCU PRESS has
sufficient pressure. Do not defuel, if a fire or engine overheat warning is displayed. During defueling,
do not operate the external lighting.
Note: For APU start/shutdown during defueling, Refer to PER-LOD-FUL APU
START/SHUTDOWN DURING REFUELING/DEFUELING.
MAX DEFUELING PRESSURE..................................................................................11 PSI (0.75 bar)
On cockpit overhead FUEL panel :
PUMPS....................................................................................................................................OFF
On refueling control panel :
REFUEL VALVES................................................................................................................. NORM
MODE SELECT (OPEN light comes on)...................................................................DEFUEL/XFR
On cockpit overhead FUEL panel :
PUMPS (of the tank(s) to be defueled)......................................................................................ON
X FEED (OPEN light comes on)................................................................................................ ON
FUEL QTY.......................................................................................................................MONITOR
When tank contents reach required level
Corresponding PUMPS.............................................................................................................OFF
On refueling control panel :
MODE SELECT (OPEN light goes out)..........................................................OFF and GUARDED
REFUEL VALVES.......................................................................................NORM and GUARDED
Set cockpit FUEL panel to normal configuration.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 12/38
FCOM 19 AUG 10
OVERWING GRAVITY REFUELING
Applicable to:
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 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.
FUEL/XFR VALVE 1/WING/R C/B (A11 on 49VU) and FUEL/XFR VALVE 2/WING/R C/B (M23
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(102)
