Anti Ice Flashcards

1
Q

When is power to the electrically heated probes applied?

A

Engine running

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2
Q

Wing anti-ice protection is applied to the ____ of each wing

A

Three outboard slat

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3
Q

Wing Anti-ice is on, what will the Wing Anti-ice VALVE lights do when the airplane lands?

A

Illuminate and remain on until wing anti-ice switch is turned off

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4
Q

If the left engine anti-ice switch is blank and its VALVE light is illuminated, what is the condition of the
left Engine Anti-ice Valve?

A

Signaled closed, and not closed

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5
Q

Wing anti-ice is on, what will the wing anti-ice valves do when the airplane lands?

A

Close

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6
Q

What is used to compute engine thrust limit corrections for engine anti-ice?

A

Engine anti-ice switch position

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7
Q

If the right wing anti-ice valve is stuck in the open position, why is the engine bleed air switch turned
off after landing?

A

Prevent engine bleed airflow to the right wing

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8
Q

How are the wing anti-ice valves controlled and operated?

A

Controlled electrically, operated pneumatically (pressure actuated)

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9
Q

The ICE DET light indicates that:

A

A fault has been detected in both ice detector units

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10
Q

Engine anti-ice automatic operation does not work on the ground.

A

True

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11
Q

The total air temperature (TAT) probe is only heated when airborne

A

T

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12
Q

In flight, when the Nacelle Anti-Ice switches and Wing Anti-Ice switches are in AUTO, and icing
conditions are detected, the respective anti-ice valves are commanded open.

A

T

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13
Q

In flight on the -300F when icing conditions are detected the respective anti-ice valves are
commanded open.

A

Automatically, if the switches are in the auto position

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14
Q

The ICING light on the -300F is an indication the engine or wing anti-ice is manually selected OFF or
an anti-ice valve is closed and engine/wing icing is detected.

A

T

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15
Q

What happens when Nacelle Anti-Ice is commanded on?

A

NAI valve opens and engine igniters operate continuously

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