Ice and Rain Flashcards

1
Q

Which areas of the wings and engines are provided ice protection

A

1) Wings- outboard 3 slats (3,4,5)
2) Engines - engine nacelle leading edge

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2
Q

Does an engine’s bleed valve need to be open to use its engine anti-ice system

A

No - it is plumbed independently from the HP compressor so the EBV does not have to be open use engine anti ice

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3
Q

What are the indications when engine anti-ice is selected on

A

1) ON (blue) - on the respective ENG 1(2) pb
2) ENG A.ICE and IGNITION (green) - on the E/WD memo section

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4
Q

What are the indications of wing anti-ice being selected on

A

1) ON (blue) - illuminates the WING pb
2) WING A. ICE (green) - appears on the E/WD memo section
3) ANTI ICE (white) - appears on each side of the BLEED page

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5
Q

When does the FAULT (amber) light in the WING and ENG 1(2) ANTI ICE pbs appear and what does it indicate?

A

1) Appears momentarily during valve transition.
2) Represents disagreement between the selected position and actual valve position
3) On the WING pb also indicates low bleed air pressure is being detected.

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6
Q

How will the PROBE WINDOW HEAT pb operate in the AUTO (light out) mode on the ground and in the air

A

1) On the ground with at least one engine running all flight deck windows/ windshields, pitot and AOA probes and static ports are automatically heated at a low heat level

-TAT probes are not heated on the ground

2) In the Air - heat levels are increased and the TAT probes are heated.

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7
Q

How will the PROBE WINDOW HEAT pb operate when selected to ON mode on the ground with engines not running

A

All flight deck windows/ windshields, pitot and AOA probes and static ports are automatically heated at a low heat level

-TAT probes are not heated on the ground

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