Ice and Rain Flashcards

1
Q

What are anti iced by electrical power?

A

Windshield, pitot tubes, AOA sensor, pitot static tube, TAT probes, static ports.

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2
Q

When ice is detected what happens to the stall protection system?

A

The stick pusher speeds are increased.

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3
Q

What is considered icing conditions?

A

10 degrees or less and visible moisture is present.

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4
Q

What visibility is considered to be icing conditions?

A

1 mile or less and 10 degrees or less

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5
Q

How long is the icing signal produced for?

A

60 seconds

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6
Q

What powers the ice detection system?

A

DC bus 1 and 2

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7
Q

When are wing and stabilizer anti icing turned on?

A

On ground above 25kts, or in flight.

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8
Q

How is the spinner anti iced?

A

Off center rotation

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9
Q

How are the leading edges anti iced?

A

Piccolo tubes running through the leading edges of the surface.

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10
Q

How is piccolo tube pressure measured?

A

3 differential switches called piccolo drop switch. Located in each wing.

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11
Q

How are bleed leaks detected?

A

Thermostats near each duct connection.

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12
Q

Which side of the system is the horizontal stabilizer connected too?

A

Left side.

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13
Q

How is windshield heat accomplished?

A

Eclectically heated through and electric conductive film embedded between layers.

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14
Q

How many windshield heat sensors are there and what are they used for?

A

3
Temperature control
Overheat
A spare

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15
Q

When does the anti ice have to be on for takeoff?

A

When icing conditions exist at or below 1500’

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16
Q

What are the thrust percentages for T/O 1? ALT T/O 1, and Anti Icing?

A

T/O 1 - 100%
ALT T/O 1 - 90%
Anti icing - 80%

17
Q

Describe the 1 part ice test.

A

Engine bleeds on, APU bleeds off
Ice detector ALL
Thrust 83% N2
Test knob 1 then 2

18
Q

What are the EICAS messages for the ice test?

A

Ice det fail, bld 1(2) low temp, ice condition.

Cross bleed open

19
Q

What area are heated with hot bleed air?

A

Wing leading edges, horizontal stabilizer leading edges, engine air inlet lips.