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Airbus > Ice And Rain > Flashcards

Ice And Rain Flashcards

1
Q

Q 01: The ______ on each wing are anti-iced with pneumatic bleed air.
A: Slats
B: Flaps
C: Three outboard slats

A

C

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2
Q

Q 02: Electrical heating is provided for the protection of:
A: Pitots and Angle Of Attack (AOA) probes
B: Pitots, static ports and TAT probes
C: Pitots, static ports, AOA probes, and TAT probes.
D: Pitots and static ports

A

C

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3
Q

Q 03: When a pneumatic leak is detected, the wing anti-ice valves:
A: Close automatically.
B: Open automatically.
C: Remain in position.

A

A

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4
Q

Q 04: When either engine anti-ice valve is open:
A: Maximum N1 is increased.
B: Minimum idle rpm is increased.
C: Minimum idle rpm is reduced.

A

B

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5
Q

Q 05: Window heat operates at what power level in flight?
A: Low
B: High

A

B

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6
Q

Q 06: On the ground the wing anti-ice valves will:
A: Open during a test sequence (30 seconds); provided pneumatic supply is available.
B: Not open at anytime.
C: Open any time the switch is pushed “ON”.

A

A

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7
Q

Q 07: Probe heat comes on automatically when:
A: The AC ESS bus is powered.
B: Electrical power is applied to the aircraft.
C: When at least one engine is running

A

C

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8
Q

Q 08: With reference to the PROBE/WINDOW HEAT pushbutton, which of the following is true?
A: The system should only be selected ON in icing conditions.
B: When in AUTO mode, the windows are heated only when necessary.
C: The system should only be selected ON after first engine start.
D: Window heating comes on automatically after first engine start

A

D

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9
Q

Q 09: The drain masts are heated after first engine start.
A: True.
B: False

A

B

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10
Q

Q 10: Where do the wing anti-ice indications appear on ECAM? A: There is no indication on ECAM bleed page for wing anti-ice B: An amber triangle appears on the ECAM bleed page
C: WING A.ICE appears on ECAM status page.
D: 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

A

D

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11
Q

Q 11: The Fault light on the engine anti-ice switches indicates the valve:
A: Is closed.
B: Position disagrees with switch position.
C: Is open.

A

B

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12
Q

Q 12: What is the difference between the engine and wing anti-ice fault lights?
A: Both indicate valve in transit, or valve position disagrees with selected position. Wing light also could indicate low pressure.
B: Both indicate low pressure, or valve position disagrees with selected position. Wing light might indicate valve in transit.
C: Both indicate valve in transit, or low pressure. Wing light also could indicate valve position disagrees with selected position.
D: Both indicate valve in transit, or overheat

A

A

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13
Q

Q 13: If one engine anti-ice system fails, the second one takes over and provides anti-icing for both engines.
A: True.
B: False.

A

B

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14
Q

Q 14: What happens when either engine anti-ice is open?
A: Maximum N1 is limited, continuous ignition is provided, maximum idle RPM is increased.
B: Maximum N1 is limited, continuous ignition is provided, minimum RPM is increased.
C: Minimum N1 is limited, continuous ignition is provided, minimum idle RPM is increased

A

B

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15
Q

Q 15: In the event of loss of electrical supply the engine anti-ice valve:
A: Opens when the engine is shut down.
B: Closes when the engine is running.
C: Opens when the engine is running.
D: Open when the OAT is < 10 deg.C with the engine running

A

C

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16
Q

Q 16: With the loss of electrical power the wing anti-ice valves:
A: Fail in their current position.
B: Fail to the open position.
C: Fail to the closed position.

A

C

17
Q 
Q 17: What is the speed limit to operate the windscreen wipers? 
A: 185 kts.
B: 200 kts.
C: 230 kts.
D: 250 kts.
A

C

18
Q

Q 18: In the event of an electrical power loss:
A: The engine anti-ice valves will open automatically, anti-icing is ensured.
B: The engine anti-ice valves will close automatically, anti-icing is lost.
C: The engine anti-ice valves will be controlled by the wing anti-ice controls.
D; The engine anti-ice valves remain in the position they were before.

A

A

19
Q

Q 19: At what power level does window heat operate while airborne?
A: High power while airborne.
B: Shifts from low to high as window temperature requires.
C: Low power above 18,000 ft.
D: Low power above 25,000 ft.

A

A

20
Q

Q 20: What happens to engine RPM when either engine anti-ice valve is open?
A: There is a fixed RPM increase.
B: The N1 limit for that engine is automatically increased.
C: The N1 limit for that engine is automatically reduced
D: There is a fixed RPM increase (3% of nominal N1)

A

C

21
Q

Q 21: Window heat operation begins:
A: Automatically after the first engine start.
B: if the PROBE/WINDOW HEAT push button is selected ON by the crew prior to engine start.
C: Both are correct.

A

C

22
Q

Q 22: Rain protection is provided by:
A: Warm bleed air blowing across the windshield.
B: Rain repellent and Windshield wipers.
C: Both are correct.

A

B

23
Q

Q 23: Can the wing anti-ice be tested on the ground?
A: Yes, with valves only open for 30 seconds.
B: Yes. Valves stay open till selected off.
C: No.

A

A

24
Q

Q 24: Anti-ice and de-icing protection is provided for:
A: The engine nacelle’s and three outboard wing slats.
B: The engine nacelle’s, the horizontal stabilizer, and three outboard wing slats.
C: The engine nacelle’s, the horizontal stabilizer, the vertical stabilizer and three outboard wing slats.

A

A

25
Q

Q 25: The probe heaters can be activated manually prior to engine start by placing the PROBE/WINDOW HEAT pushbutton.
A: True.
B: False.

A

A

26
Q

Q 26: What happens to the heat at the drain masts when the aircraft is on the ground?
A: Nothing.
B: The heat is reduced to prevent injury to ground personnel.
C: Some of them are automatically switched off (pitot, AOA).

A

B

27
Q

Q 27: The RAIN RPLNT (rain repellent) pushbutton is inhibited on the ground when the engines stopped.
A: True.
B: False.

A

A

28
Q

Q 28: TAT probes are heated on the ground.
A: True.
B: False.

A

B

29
Q

Q 29: The ON light illuminates on the wing anti-ice P/B:
A: When the anti-ice valves open
B: When the P/B is set to ON
C: When the fault light goes out
D: When the anti-ice valves open and the fault light goes out.

A

B

30
Q

Q 30: How is window heating regulated?
A: Manually by flight crew
B: Window heat is not regulated!
C: One Window Heat Computer (WHC) as master, the other as slave
D: By two independent Window Heat Computers (WHC), one for each side

A

D

31
Q

Q 31: The Window Heat Computer provides two power levels for the windshield:
A: High power when above 20,000 ft, low power when below 20,000 ft
B: High power when OAT < 10 deg.C, low power when OAT> 10 deg.C
C: High power in flight, low power on the ground
D: High power in icing conditions (flight only), low power in other conditions.

A

C

32
Q

Q 32: The engine nacelle is anti-iced by:
A: Air bleed from the high pressure compressor
B: Air bleed from low pressure compressor
C: AC system and air bleed from low pressure compressor
D: DC system and air bleed from low pressure compressor.

A

A

33
Q

Q 33: When an engine anti-ice valve is open:
A: N1 limit is automatically reduced and the idle N1 is automatically increased
B: N2 of the associated engine is automatically decreased
C: N2 limit is automatically reduced and N1 limit is automatically increased
D: There is no change in the N1 and N2 limits.

A

A

34
Q

Q 34: In the event of a low air pressure:
A: The engine anti-ice valve opens automatically
B: There is no effect on the anti-ice valve position
C: The engine anti-ice valve must be manually closed
D: The engine anti-ice valve closes automatically

A

D

35
Q

Q 35: How can you check that engine anti-ice has been selected on?
A: 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
B: You can observe the amber warning on the ECAM memo display and the amber anti-ice light on the overhead panel
C: You can observe the ENGINE ANTI-ICE message on the ECAM STATUS page
D: 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

A

D

36
Q

Q 36: The electric windshield wipers are controlled:
A: Automatically when in heavy rain
B: By two individual pushbuttons
C: By one rotary selector for both windshields
D: By two individual rotary selectors

A

D

37
Q

Q 37: The wipers can operate at different speeds:
A: Low speed and high speed
B: Speed 1 and speed 2
C: Low, medium and high speed.
D: Speed is automatically adjusted depending on rain intensity.

A

A

38
Q

Q 38: When the wiper is turned off:
A: The PARK position must be selected to stow the wiper
B: It continues to run for approximately 6 seconds
C: The wiper may stop in the pilots view
D: The wiper stops out of view

A

D

Airbus (16 decks)

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