Ice and Rain Protection Flashcards

1
Q

How many Ice Detector Probes are installed?

A

2

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2
Q

How many wing inspection lights are there?

A

2

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3
Q

Does the wing heat source switch automatically transfer to the operating engine in the event of an engine failure?

A

Yes

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4
Q

Does the Anti-Icing system use Intermediate or High pressure bleed air?

A

High pressure bleed air …regulated to ~ 36 psi

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5
Q

What surfaces are being heated by High Pressure Bleed air?

A

Wing leading edges and engine inlets.

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6
Q

With the updated ice detect probes (CL350 and CL300’s modified with SB 100-30-04), at what speed must the wing heat be on?

A

In icing conditions and the airspeed is less than 210 KIAS or the Ice Detected CAS message is On.

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7
Q

What happens to the wing anti-ice valves when electrical power is lost?

A

The valve is spring loaded to fail closed.

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8
Q

What happens to the engine anti-ice valve when electrical power is lost?

A

The valve is spring loaded to fail open.

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9
Q

Which ice protection components, probes, and sensors are heated electrically?

A
L/R Pitot/Static probes
L/R AOA
Standby pitot probe
L/R stby static ports
TAT probe(with weight off wheels),
windshield/windows
T2 sensors.
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10
Q

When are the ice detect probes receiving DC power?

A

When the batteries are on.

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11
Q

Amber “ICE DETECTED” CAS means what?

A

Ice is detected and 1 or more anti-ice systems are not on

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12
Q

After being de-iced/anti-iced with Type 2, 3, or 4, when do you turn on the wing anti-ice?

A

Just prior to setting TO power.

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13
Q

What controls the anti-ice protection system?

A

Integrated Air System Controllers(IASC) 1 and 2

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14
Q

Which window is heated during Essential Power Only condition?

A

L. (side)Window only

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15
Q

What surfaces are considered “critical” ?

A

Wings and winglets, horizontal and vertical stabilizers, all control surfaces, upper fuselage, and engine inlets

(Clean aircraft concept: frost on the upper fuselage is not limiting and up to 1/8 inch (3mm) frost due to cold soaked
fuel on the underside of the wing is acceptable, otherwise all surfaces must be free of contamination)

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