A330F Test

If the ADIRS does not send aircraft attitude information to the Fuel Control Monitoring System (FCMS). Thus, on battery refuel, theere coud be a difference up to 750 kg (1653.6445 lb) between the set fuel quantity and the actual fuel quantity. True. False.

The main fuel pump system has 2 main fuel pumps and 2 standby fuel pumps. True. False.

Automatic transfer from the outer tanks to the inner tans occurs when the center tank have been emptied and either inner tank reaches ______ kg. 2,5000 kg (5,500 lbs). 3,000 kg (6,600 lbs). 3,500 kg (7,700 lbs).

How many surge vent tanks are there?. Five. Two. Three.

Suction feed to the engines is possible from: The wing and tip tanks. The outer tank transfer valve only. The inner tanks only. The outer tanks only.

The AC powered aft auxiliary fuel boost pump from the APU operates whenever the APU is operating and no other pump is on. It has an alternate power source an the AC Static Inverter bus for battery-only starts. True. False.

To perform a correct pressure fueling in A330's aircraft is important: Battery SW ON and perform low level test. ADIRU´s must be started. The fueling panel must be energized.

From which tanks will fuel gravity feed?. Outer TANK of the wings tank, TO inner TANK of the wing tanks. Inner cell of the wing tanks, and center tank. Outer cell of the wing tanks, inner cell of the wing tanks, and/or center tank. The center tank only,.

What is the purpose of the trim fuel transfer system?. Control the center of gravity position. Burn the fuel from the trim tank. Control all transfers of engine feed.

What is the purpose of fuel control and monitoring system?. The FCMS control refuel, transfers, CG, FQI and sensing. The FCMS calculates ZFW, CFCG, and indicates AFT CG Warning. The FCMS only measures fuel quantity and gives indications.

The main fuel pump system supplies fuel from the ____ tanks to the engines. Inner tank. Outer tank. Center tank. All of the above.

Automatic control of CG (center of gravity): Begins when climbing through FL 255. Is terminated when descending through FL 245. Is terminated when FMGES time to destination is below 35 minutes. All of the above.

Before preselect the Quantity on 990VU refuel panel, you first must do: Start the pump on the fuel tanker unit. Stop the pump on the fuel tanker unit. Lift the guard, then push (in) and hold the HI LEVEL TEST switch 3QJ for 10 seconds.

There are ___ fuel pumps in each A330 wing tank collector cell. 1. 2. 3. 4.

If you want the automatic fueling in a correct time you must: Preselect 3,000 kg more than of required. Preselect 3,000 kg more than of required. Preselect exactly the required fuel on board, or 200 kg more than the required.

What doe an amber line across the las tow digits of the fuel quantity mean?. A fuel quantity indication is inaccurate. The fuel quantity is not good and should be checked. A disagreement between fuel measured and fuel entered in the MCDU has been detected. Not all the fuel aboard is usable.

The engine low pressure fuel valves are controlled by: Engine MASTER switch. ENG FIRE pb. BATT Switch. Engine MASTER switch and ENG FIRE pb.

What happens when fuel is collected in a surge vent tank?. Fuel is drained back into tank. Overpressure protector breaks open. Fuel is sucked by dedicated jet pump.

If is necessary transfer to DMI any fuel valve actuator, you must remove the actuator and then: - Reinstall the actuator. - Install the connectors removed form the actuator,. - Reinstall the actuator. - Install DUMMY plug and receptacle on the connectors removed from the actuator. - Align dowl and install the valve locking tool. - Install DUMMY plug and receptacle on the connectors removed from the actuator.

Automatic transfer of fuel from the outer tanks to the inner tanks is performed by gravity. True. False.