Stall Warning Flashcards

1
Q

In order for nitrogen to flow into the stick pusher actuator what must occur?

A

Both channels of the SW/SP computer must command the opening of their actuator solenoid valves.

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2
Q

Is there a stick pusher system installed on the 200 series?

A

No

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3
Q

Except during a system test, stall warning signals are inhibited when ?

A

On the ground

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4
Q

How many independent computer channels are incorporated into the stall warning/stick pusher computer?

A

2

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5
Q

Angle of attack vanes are heated by which electrical power source?

A

115 V a.c.

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6
Q

A centre reading of the fast/slow pointer on the EADI represents a nominal airspeed of what?

A

1.3Vs

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7
Q

To manually overpower the stick pusher a force of greater than how many kilograms is required?

A

36 kg

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8
Q

Does the stall warning/stick pusher system have lift transducers?

A

No

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9
Q

The failure of the left side angle of attack sensor vane will result in the illumination of what caution lights?

A

1 STALL SYST FAIL, PUSHER SYST FAIL

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10
Q

What conditions must be satisfied in order for a stick shaker signal to be generated by the stall warning/stick pusher computer?

A

True AOA exceeds reference AOA

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11
Q

What is the SW/SP system powered by?

A

Both channels are powered from the 28 V DC left and right essential buses respectively

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12
Q

When flying in icing conditions what can you do to increase the reference AOA?

A

Activating the propeller DE-ICE TIMER, or INCR REF SPEED switch

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13
Q

When is the stick pusher system inhibited?

A

Below 400 feet AGL, or when the air speed is greater than 200 kts

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14
Q

Does the 200 series have angle of attack vanes?

A

No they have left transducers

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15
Q

What are the lift transducer heaters powered by on the ground and in the air?

A

On the ground they are powered by 28 V DC and in the air they are powered by 115 V a.c.

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