Chapter 16C - AOA Sensors and Stall Warning Systems Flashcards

1
Q

What types of AoA sensors are there?

A

Probe and Vane

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2
Q

Stalling is based on..?

A

AoA

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3
Q

How does a conical probe work?

A

Changes in air pressure cause a rotary motion of the probe

Stagnation point is between the 2 slots

Uses an internal paddle to stay aligned

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4
Q

How do you prevent icing on a conical probe?

A

Heated electrically

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5
Q

What is a stick shaker?

A

Stall warning system

Comes in at Vs + higher of 5kts of 5%

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6
Q

What is Minimum manoeuvring speed?

A

1.3G low speed buffet margin

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7
Q

Orange hockey stick on a PFD is?

A

The minimum manoeuvring speed

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8
Q

What are the inputs into a stall warning computer (SWC)?

A

AoA

Configuration (Flaps & Slats)

Air/ground logic (Weight on wheels)

Thrust

ADC - Airspeed, Mach No, or corrected AoA

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9
Q

What are the outputs of a stall warning computer (SWC)?

A

Stick Shaker

Audio warning

Flight Envelope Protection

Red lines on the display and orange hockey stick

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10
Q

Systems using the Angle of Attack measurement include:

A
  • Air Data Computer – position error
  • Stall Warning and Protection Systems critical AoA
  • Flight Envelope Protection – stall protection
  • Wind Shear Detection System – warning of unusual airflow
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11
Q

Stall warnings must be?

A

unambiguous

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12
Q

Detail some stall protection systems?

A
  • Operational during manual and/or automatic flight
  • “Stick push” and/or automatic deployment of leading edge devices operate on activation of stall warning in non fly-by-wire aircraft
  • FBW aircraft protect from the stall by Flight Envelope Protection
  • A/P maintains pitch attitude below and speed above stall attitude and stall speed
  • SPS prevents the stall, SWS only provides a warning
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13
Q

SPS … the stall, SWS provides a …..

A

Prevents and warning

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