Ice And Rain Protection Flashcards

1
Q

How is anti-icing provided to the aircraft?

A
  • Bleed air
  • Electrical heating
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2
Q

Which components of the aircraft have anti-icing?

A
  • 3 outboard wing slats (bleed)
  • leading edge of engine nacelles (bleed)
  • pitot tubes (electrical)
  • Static ports (electrical)
  • waste water drain masts (electrical)
  • Flight deck windows (electrical)
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3
Q

When do icing conditions exist?

A
  • OAT is 10°C or below
  • Visible moisture is present
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4
Q

Can wing anti-ice be used with slats extend it?

A

Yes, but should be avoided

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5
Q

How is window heating controlled?

A

With the two window heat computers (WHC)

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6
Q

When are the windows heated?

A
  • Automatically on the ground with one engine running
  • in-flight
  • When the probe/window heat pb is pushed
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7
Q

What is the limitation for using the windshield wipers?

A
  • 230 kts
  • Do not use on dry window
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8
Q

What’s a limitation exists for the rain repellent?

A
  • Do not use on dry window
  • use only on moderate to heavy rain conditions
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9
Q

How is probe heating controlled?

A

Probe heat computer (1/2/3)

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10
Q

When are the probes heated?

A
  • On the ground with one engine running
  • in-flight
  • when probe/window heat pb is on
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