Aircraft Systems: Flight Director Disengagement
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Questions and Answers

What happens to the lateral and vertical modes when all FDs disengage without any AP engaged?

  • They remain engaged and the A/THR switches to MAN mode.
  • They remain engaged, and the A/THR becomes inoperative.
  • They disengage, and the A/THR reverts to SPEED or MACH mode. (correct)
  • They disengage and the A/THR switches to FLIGHT mode.
  • Under what condition does the FD automatically disengage during ROLL OUT?

  • If the difference between the aircraft track and runway track is more than 20°. (correct)
  • If the aircraft speed is below VLS.
  • If any AP is engaged.
  • If the A/THR reverts to SPEED mode.
  • What should a flight crew do to manually disengage an onside FD?

  • Turn off the A/THR.
  • Switch to the opposite FD.
  • Press the onside FD pb. (correct)
  • Activate a backup FD.
  • Which condition causes the FD to disengage due to speed protection?

    <p>When no AP is engaged and the aircraft speed is out of VLS to VMAX range.</p> Signup and view all the answers

    Which of the following is NOT a reason for the FD to disengage due to failures?

    <p>The aircraft ascends beyond the cruising altitude.</p> Signup and view all the answers

    What condition causes the pitch bar to flash for 10 seconds?

    <p>Automatic reversion to V/S or FPA mode occurs.</p> Signup and view all the answers

    What occurs if the FD guidance orders are not available while engaged?

    <p>FD bars disappear and a FD flag appears.</p> Signup and view all the answers

    Under which condition does the roll bar flash for 10 seconds?

    <p>When lateral deviation is above 15 ft RA during approach.</p> Signup and view all the answers

    What is indicated if the pitch bar is flashing due to inability to compute vertical deviation?

    <p>There is an issue with the MMR that cannot calculate deviation while approaching.</p> Signup and view all the answers

    What happens to the autopilots (APs) if one of the engagement conditions is lost?

    <p>The APs automatically disengage.</p> Signup and view all the answers

    During an approach with FINAL APP mode engaged, at what altitude do the APs disengage if the MDA/MDH is entered?

    <p>50 ft below MDA/MDH</p> Signup and view all the answers

    At what bank angle will the APs disengage in normal law?

    <p>45 °</p> Signup and view all the answers

    Study Notes

    Aircraft Systems - Auto Flight - Flight Guidance - Flight Director - FD Disengagement

    • General Disengagement: If all Flight Directors (FDs) disengage while no Auto Pilot (AP) is engaged, lateral and vertical modes disengage, and the Automatic Thrust (A/THR) reverts to (or remains in) SPEED or MACH mode.
    • AP Engaged Disengagement: If all FDs disengage while at least one AP is engaged, lateral and vertical modes remain engaged, and the A/THR remains engaged in the current mode.
    • Manual Disengagement: The flight crew can manually press the on-side FD pushbutton to disengage the on-side FD.
    • Automatic Disengagement (Roll Out): The FD disengages if, during the roll-out phase, the difference between the aircraft track and the runway track is more than 20 degrees.
    • Automatic Disengagement (Due to Failures): The FD disengages if the FD, Flight Control Unit (FCU), or any engine fails.
    • Automatic Disengagement (Speed Protection): The FD disengages if no AP is engaged and the aircraft speed is either below the Vertical Speed Limit (VLS) in Decending (DES) or Op Decending (OP DES) or above the Maximum Speed (VMAX) in Climb (CLB) or Op Climb (OP CLB).
    • Post-Disengagement Action: After the FD disengages, the A/THR reverts to SPEED or MACH mode and adjusts the thrust to recover the target speed or keep the speed within the range from VLS to VMAX, if the target speed is out of this range.

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    Description

    This quiz covers various aspects of Flight Director disengagement in aircraft systems. It includes general disengagement scenarios, automatic and manual disengagement procedures, and the impact of failures on flight guidance. Test your knowledge on critical flight guidance concepts and ensure safe operation of autopilot systems.

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