Aircraft Stall Types Quiz
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Questions and Answers

What is the main cause of stall loss of lift on an airplane's wing?

  • Low density altitude
  • Excessive weight on the aircraft
  • High load factor
  • Disruption of smooth airflow over the wing (correct)
  • When does a power-off stall typically occur?

  • During go-arounds
  • During climb out
  • During normal landing approach (correct)
  • During take-off
  • What is a common symptom indicating an airplane stall is about to occur?

  • Higher airspeed
  • Increased control effectiveness
  • Mushy feeling in the flight controls (correct)
  • Harsh vibrations in the flight controls
  • What is the first step in stall recovery for an airplane?

    <p>Decrease the angle of attack</p> Signup and view all the answers

    In what situation is a Crossed Control Stall most likely to occur?

    <p>During a turn from base to final on-landing approach</p> Signup and view all the answers

    What is the primary cause of a stall that may develop into a spin?

    <p>Using not enough rudder control for the amount of aileron being used</p> Signup and view all the answers

    During an upright or erect spin, which direction do the rolling and yawing motions occur?

    <p>Rolling and yawing in the same direction</p> Signup and view all the answers

    What is the difference between an incipient spin and a fully developed spin?

    <p>The level of rotation rates, airspeed, and vertical speed stabilization</p> Signup and view all the answers

    In a flat spin, what type of motion is primarily observed?

    <p>Yawing only</p> Signup and view all the answers

    What is the key reason that makes recovery from a flat spin usually difficult to impossible?

    <p>Loss of reference points for orientation</p> Signup and view all the answers

    Study Notes

    Stalls

    • Stalls occur when the smooth airflow over the airplane's wing is disrupted, causing lift to degenerate rapidly.
    • This occurs when the wing exceeds its critical angle of attack.
    • The stalling speed of an airplane is not a fixed value for all flight situations, but the airplane will always stall at the same angle of attack regardless of airspeed, weight, load factor, or density altitude.

    Types of Stalls

    • Power-off stalls: can be encountered during normal landing approach.
    • Power-on stalls: normally encountered during take-off, climb out, and go-arounds.
    • Crossed control stall: most likely to occur when a pilot tries to compensate for overshooting a runway during a turn from base to final on-landing approach.

    Stall Recognition and Recovery

    • A typical indication of a stall is a mushy feeling in the flight controls and less control effect as the aircraft's speed decreases.
    • The reduction of control effectiveness is primarily due to reduced airflow over the flight control surfaces.
    • To recover from a stall:
      • Decrease the angle of attack.
      • Smoothly apply maximum allowable power.
      • Adjust the power as required.

    Spins

    • A stalled aircraft is a prerequisite for a spin.
    • Primary causes of spins include:
      • Exceeding the critical angle of attack while performing uncoordinated maneuvers.
      • Either too much or not enough rudder control for the amount of aileron being used, resulting in a crossed control condition.
    • Types of spins include:
      • Upright or erect spin: slightly nose down, rolling or yawing motion in the same direction.
      • Inverted spin: spinning upside down with roll and yaw in opposite directions.
      • Flat spin: yaw only, with recovery usually difficult to impossible.

    Spin Phases and Recovery

    • Incipient spin: the portion of a spin from the time the airplane stalls and rotation starts until the spin is fully developed.
    • Fully developed spin: occurs after the incipient stage, when the angular rotation rates, airspeed, and vertical speed are stabilized from turn to turn, and the flight path is close to vertical.
    • To recover from a spin:
      • Move the throttle to idle to eliminate thrust and minimize altitude loss.
      • Neutralize the ailerons.
      • Determine the direction of rotation using the turn coordinator.
      • Apply the full opposite rudder.
      • Apply the rudder opposite the turn.

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    Description

    Test your knowledge on different types of stalls that can occur in an aircraft, such as power-off and power-on stalls. Learn about the causes and factors affecting a stall, including the critical angle of attack and stalling speed variations. Understand how stalls can impact the lift generated by an aircraft's wing.

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