Aircraft Energy Management Alert System
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Questions and Answers

What does the low energy aural alert 'SPEED SPEED SPEED' indicate to the pilot?

  • The aircraft energy is lower than a threshold. (correct)
  • The landing gear is not properly configured.
  • The aircraft is traveling too fast for safe flight.
  • The aircraft is entering a stall condition.
  • Under what conditions will the low energy aural alert NOT be triggered?

  • When the aircraft is airborne above 2000 ft RA. (correct)
  • When TOGA is selected. (correct)
  • When the aircraft is below 100 ft RA. (correct)
  • When alpha floor is triggered. (correct)
  • Which inputs does the low energy aural alert rely on for its computation?

  • Pilot's experience level, weather conditions, flight duration.
  • Aircraft weight, engine power, wind speed.
  • Aircraft configuration, pilot's altitude, throttle position.
  • Aircraft configuration, air speed deceleration rate, flight path angle. (correct)
  • What happens immediately after the low energy aural alert is triggered if nothing changes?

    <p>ALPHA Floor alert is activated.</p> Signup and view all the answers

    At what altitude range is the low energy aural alert available?

    <p>From 100 to 2,000 ft.</p> Signup and view all the answers

    What is the frequency of the low energy aural alert 'SPEED SPEED SPEED'?

    <p>Every 5 seconds</p> Signup and view all the answers

    At which altitudes is the low speed alert available?

    <p>100 to 2000 ft</p> Signup and view all the answers

    In which configurations can the low speed alert be activated?

    <p>Configuration 2, 3, and full</p> Signup and view all the answers

    Study Notes

    Low Energy Aural Alert

    • A low energy aural alert, repeating "SPEED SPEED SPEED" every 5 seconds, warns the pilot of decreasing aircraft energy below a recovery threshold.
    • The alert indicates the need to increase thrust to regain a positive flight path angle (FPA).
    • The alert is activated when aircraft energy falls below a threshold between 100 and 2,000 ft altitude.
    • Alert availability depends on configuration (2, 3, or full).
    • Alert triggering speed depends on the aircraft's flight path angle (FPA) during deceleration. For example, at -3° FPA, the alert triggers at approximately VLS -8; at -4° FPA, at approximately VLS -2.
    • The alert prioritizes prompting pilots to adjust thrust using the SPEED scale.
    • It occurs immediately before the ALPHA Floor alert.
    • The alert is calculated by the PRIM system using aircraft configuration, air speed deceleration rate, and flight path angle.

    Alert Limitations

    • The alert is disabled during:

      • TOGA selection
      • Below 100 ft or above 2,000 ft.
      • Alpha floor or GPWS alert activation.
      • Failed vertical speed (RA) sensors in alternate or direct law.
    • Alert timing relative to the ALPHA Floor depends on deceleration rate. Alert delay occurs if deceleration happens before ALPHA floor unless an ALPHA floor is triggered by stick deflection in which case there's no delay.

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    Description

    This quiz covers the functionalities and limitations of the Low Energy Aural Alert system used in aviation. It aims to educate pilots on recognizing the alert, understanding its activation criteria, and the importance of adjusting thrust to regain a positive flight path angle. Explore how this alert interacts with other systems and its role in flight safety.

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