TEST A320 SERIES

The ______ on each wing are anti-iced with pneumatic bleed air. Three outboard slats. Flaps. slats.

Electrical heating is provided for the protection of: Pitots, static ports, AOA probes, and TAT probes. Pitots and static ports. Pitots, static ports and TAT probes. Pitots and Angle Of Attack (AOA) probes.

When a pneumatic leak is detected, the wing anti-ice valves: Close automatically. Open automatically. Remain in position.

When either engine anti-ice valve is open: Minimum idle rpm is increased. Minimum idle rpm is reduced. Maximum N1 is increased.

Window heat operates at what power level in flight?. High. Low.

Probe heat comes on automatically when: When at least one engine is running. Electrical power is applied to the aircraft. The AC ESS bus is powered.

On the ground the wing anti-ice valves will: Open during a test sequence (30 seconds); provided pneumatic supply is available. Not open at anytime. Open any time the switch is pushed "ON".

Where do the wing anti-ice indications appear on ECAM?. ANTI-ICE appears in white on the ECAM bleed page and W A.ICE appears in green on the ECAM memo when the wing P/B is pressed. WING A.ICE appears on ECAM status page. An amber triangle appears on the ECAM bleed page. There is no indication on ECAM bleed page for wing anti-ice.

The Fault light on the engine anti-ice switches indicates the valve: Position disagrees with switch position. Is open. Is closed.

What is the difference between the engine and wing anti-ice fault lights?. Both indicate valve in transit, or valve position disagrees with selected position. Wing light also could indicate low pressure. Both indicate valve in transit, or overheat. Both indicate valve in transit, or low pressure. Wing light also could indicate valve position disagrees with selected position. Both indicate low pressure, or valve position disagrees with selected position. Wing light might indicate valve in transit.

With reference to the PROBE/WINDOW HEAT pushbutton, which of the following is true?. Window heating comes on automatically after first engine start. The system should only be selected ON after first engine start. When in AUTO mode, the windows are heated only when necessary. The system should only be selected ON in icing conditions.

If one engine anti-ice system fails, the second one takes over and provides anti-icing for both engines. False. True.

What happens when either engine anti-ice is open?. Maximum N1 is limited, continuous ignition is provided, minimum RPM is increased. Minimum N1 is limited, continuous ignition is provided, minimum idle RPM is increased. Maximum N1 is limited, continuous ignition is provided, maximum idle RPM is increased.

In the event of loss of electrical supply the engine anti-ice valve: Opens when the engine is running. Open when the OAT is < 10 deg.C with the engine running. Closes when the engine is running. Opens when the engine is shut down.

With the loss of electrical power the wing anti-ice valves: Fail to the closed position. Fail to the open position. Fail in their current position.

The drain masts are heated after first engine start. False. True.

What is the speed limit to operate the windscreen wipers?. 230 kts. 250 kts. 200 kts. 185 kts.

In the event of an electrical power loss: The engine anti-ice valves will open automatically, anti-icing is ensured. The engine anti-ice valves will close automatically, anti-icing is lost. The engine anti-ice valves will be controlled by the wing anti-ice controls. The engine anti-ice valves remain in the position they were before.

At what power level does window heat operate while airborne. High power while airborne. Shifts from low to high as window temperature requires. Low power above 18,000 ft. Low power above 25,000 ft.

What happens to engine RPM when either engine anti-ice valve is open?. The N1 limit for that engine is automatically reduced. There is a fixed RPM increase. The N1 limit for that engine is automatically increased. There is a fixed RPM increase (3% of nominal N1).

Window heat operation begins: Both are correct. if the PROBE/WINDOW HEAT push button is selected ON by the crew prior to engine start. Automatically after the first engine start.

Rain protection is provided by: Rain repellent and Windshield wipers. Both are correct. Warm bleed air blowing across the windshield.

Can the wing anti-ice be tested on the ground?. Yes, with valves only open for 30 seconds. Yes.Valves stay open till selected off. No.

Anti-ice and de-icing protection is provided for: The engine nacelle's and three outboard wing slats. The engine nacelle's, the horizontal stabilizer, and three outboard wing slats. The engine nacelle's, the horizontal stabilizer, the vertical stabilizer and three outboard wing slats.

The probe heaters can be activated manually prior to engine start by placing the PROBE/WINDOW HEAT pushbutton. True. False.

What happens to the heat at the drain masts when the aircraft is on the ground?. The heat is reduced to prevent injury to ground personel. Some of them are automatically switched off (pitot, AOA). Nothing.

The RAIN RPLNT (rain repellent) pushbutton is inhibited on the ground when the engines stopped. True. False.

TAT probes are heated on the ground. False. True.

The ON light illuminates on the wing anti-ice P/B. When the P/B is set to ON. When the fault light goes out. When the anti-ice valves open and the fault light goes out. When the anti-ice valves open.

How is window heating regulated?. By two independent Window Heat Computers (WHC), one for each side. One Window Heat Computer (WHC) as master, the other as slave. Window heat is not regulated!. Manually by flight crew.

The Window Heat Computer provides two power levels for the windshield: High power in flight, low power on the ground. High power in icing conditions (flight only), low power in other conditions. High power when OAT < 10 deg.C, low power when OAT > 10 deg.C. High power when above 20,000 ft, low power when below 20,000 ft.

The engine nacelle is anti-iced by: Air bleed from the high pressure compressor. Air bleed from low pressure compressor. AC system and air bleed from low pressure compressor. DC system and air bleed from low pressure compressor.

When an engine anti-ice valve is open: N1 limit is automatically reduced and the idle N1 is automatically increased. There is no change in the N1 and N2 limits. N2 limit is automatically reduced and N1 limit is automatically increased. N2 of the associated engine is automatically decreased.

In the event of a low air pressure: The engine anti-ice valve closes automatically. The engine anti-ice valve must be manually closed. There is no effect on the anti-ice valve position. The engine anti-ice valve opens automatically.

How can you check that engine anti-ice has been selected on?. You can observe the blue ON light on the associated engine anti-ice P/B and the ENGINE ANTI-ICE memo on the E/WD. You can observe the ENGINE ANTI-ICE message on the ECAM STATUS page. You can observe the amber warning on the ECAM memo display and the amber anti-ice light on the overhead panel. You can observe the ON light on the associated engine anti-ice P/B and the ENGINE ANTI-ICE message on the ECAM engine page.

The electric windshield wipers are controlled: By two individual rotary selectors. By one rotary selector for both windshields. By two individual pushbuttons. Automatically when in heavy rain.

The wipers can operate at different speeds: Low speed and high speed. Speed 1 and speed 2. Low, medium and high speed. Speed is automatically adjusted depending on rain intensity.

When the wiper is turned off: The wiper stops out of view. The wiper may stop in the pilots view. It continues to run for approximately 6 seconds. The PARK position must be selected to stow the wiper.