F320

Refueling is possible if the aircraft batteries are the only source of power. A: True. B: False.

Fuel transfer from the outer compartment to the inner compartment of the wing tanks occurs when the inner compartment quantity decreases to: A: 250 kilograms. B: 450 kilograms. C: 750 kilograms. D: 5000 kilograms.

What indication will you see on the overhead fuel panel if the center tank has more than 250 kilograms of fuel and the left- or right-wing tank have less than 5,000 kilograms. A: Auto feed fault. B: Fuel imbalance. C: Mode select fault. D: Fuel - Auto feed fault.

The Fuel Used indication on ECAM is reset: A: Manually by the pilot. B: Automatically at engine start on the ground. C: Automatically at electric power up of the aircraft.

An amber line appears across the last two digits of the ECAM FOB indication when: A: Fuel quantity is unreliable. B: The center tank pumps are switched off. C: The center tank pumps have failed.

The fuel crossfeed valve is controlled by a double motor. A: True. B: False.

From which tanks will fuel gravity feed?. A: Outer cell of the wing tanks, inner cell of the wing tanks, and/or center tank. B: Inner cell of the wing tanks, and center tank. C: Inner cell of the wing tanks. D: The center tank only.

The APU fuel system: A: Uses its own dedicated DC powered fuel pump. B: Obtains fuel from either center tank pump. C: Obtains fuel from the left fuel manifold via the left side fuel pumps or if needed, the APU fuel pump. D: Obtains fuel from the left fuel manifold via the right side fuel pumps.

Refueling time at normal pump pressure is _____ minutes for the wing tanks and _____ minutes for all tanks. A: 15 & 25. B: 17 & 20. C: 15 & 20. D: 25 & 35.

. After engine shutdown, what are your actions to close the fuel transfer valves?. A: You have to switch the inner tank pumps off. B: You have to call maintenance to close the valves. C: No action is required. The valves will close automatically during the next refueling.

What is the minimum fuel quantity for takeoff?. A: 1,000 kg. B: 1,200 kg. C: 1,500 kg. D: 2,000 kg.

The fuel recirculation System ensures the IDG cooling when the oil temperature is high, the ____ controls the fuel return valve. A: Cross feed valve. B: Suction valve. C: Transfer valve. D: FADEC.

. The fuel feed sequence is: A: Outer tanks - Inner tanks - Center tank. B: Inner tanks - Outer tanks- Center tank. C: Center tank - Inner tanks- Outer tanks.

. Electrical transients (caused by switching among the APU, the external and the engine electrical supply) during automatic refueling may stop the process. A: False. B: True.

The ____ is a computerized system that controls automatic refueling. A: FADEC. B: FQI. C: Cross Feed.

When fuel quantity in one wing tank goes below ____, the low-level sensor triggers the LO LVL warning on ECAM. A: 650 Kg. B: 1500 Kg. C: 750 Kg. D: 700 Kg.

The Fuel Tank Inerting System only is installed in the center tank. A: True. B: False.

An advisory appears when the temperature is below _____. A: -30° C. B: -10° C. C: -40° C. D: 10° C.

. The outer indication is boxed amber, if both transfer valves fail to open when the inner is at low level. A: False. B: True.

. An advisory appears in flight phases 2 and 6, when the difference between the fuel quantities in the two wings is greater than ______. A: 1500 kg. B: 750 kg. C: 1350 kg. D: 2250 kg.