Chapter 3 - Anti-Ice & Rain Flashcards

1
Q

What is the consequence of a failure of the windshield wiper?

A

Revert to CAT I only.

Don’t use on dry surfac.e

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2
Q

How are the pitot, TAT and alpha vanes heated?
- What’s the power source?

A

Electronically, AC power.

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3
Q

What is the effect of a total loss of AC power on the pitot probe?

A

Only the Captain’s is heated by AC standby bus.

Light won’t illuminate for subsequent failures.

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4
Q

Which windows are heated?

A

L1, L2, R1, R2.

L3 and R3 are not.

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5
Q

Regarding the green window heat light, what happens on very warm days?

A

Extinguishes, as power is automatically removed if there is an OVERHEAT.

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6
Q

Where is engine bleed sourced from on the NG, and on the MAX?

A

5th and 9th stage of the engine compressor.

6th and 10th on the MAX.

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7
Q

How is the engine bleed system controlled and operated?

A

Controlled electronically, operated pneumatically

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8
Q

What is the effect of a COWL ANTI-ICE light?

A

Signifies duct pressure exceeds a certain limit.

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9
Q

What is the effect of the bleed valve failed closed?

A

Dispatch only to no known or forecast icing conditions

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10
Q

What is the effect of a bleed valve failed open?

A

More serious.

  • CAT I only
  • Minimum 50% N1 on the affected engine during icing
  • Cannot be guaranteed with A/T
  • Fuel penalty too.
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11
Q

How is the wing anti-ice system powered?

A

By AC.

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12
Q

What is the effect of selecting WAI in flight?

A

Changes stall logic for the remainder of the flight, regardless of position.

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13
Q

Above what FL should WAI not be used?

A

Above FL350 - bleed trip off & loss of cabin pressure is possible.

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14
Q

When is use of the WAI recommended?

A

During holding, moderate / severe icing.

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