Aircraft Lateral Control Modes Quiz
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Questions and Answers

What happens to roll control when the aircraft transitions from ground mode to in flight mode?

  • The flight crew must manually manage roll and bank angles without assistance
  • Rudder is used independently for all roll maneuvers
  • The sidestick combines control of ailerons, spoilers, and rudder for turn coordination (correct)
  • Control is limited to a single surface for enhanced stability
  • During the decrab phase, what does the aircraft system do to assist the flight crew?

  • Eliminates the need for pedal input altogether
  • Limits induced roll after pedal input (correct)
  • Reverts to manual flight without restrictions
  • Increases roll rate to match pedal input
  • How is the roll rate affected by the sidestick deflection during flight?

  • It is proportional to sidestick deflection, with a maximum of 15 °/s (correct)
  • It is inversely proportional to sidestick deflection
  • It can exceed 20 °/s in specific conditions
  • It is fixed regardless of sidestick position
  • What is a key factor in determining how much control surface deflection occurs on ground mode lateral movement

    <p>Aircraft speed during operation</p> Signup and view all the answers

    Which of the following is impacted by sidestick deflection in an aircraft?

    <p>Control surface actuation</p> Signup and view all the answers

    What happens to control surface effectiveness as aircraft speed changes?

    <p>Effectiveness increases with changes in speed</p> Signup and view all the answers

    What surfaces can be deflected to increase yaw efficiency in the event of an engine failure during takeoff?

    <p>Spoiler and ailerons</p> Signup and view all the answers

    In the case of engine failure, which wing's surfaces are primarily adjusted to manage yaw?

    <p>The wing opposite to the failed engine spoiler 6 and aileron</p> Signup and view all the answers

    What is the purpose of deflecting control surfaces on the opposite wing during an engine failure?

    <p>To increase yaw efficiency</p> Signup and view all the answers

    How does increasing yaw efficiency during an engine failure on ground affect VMCG?

    <p>It reduces VMCG.</p> Signup and view all the answers

    What is the primary benefit of reducing VMCG in the event of an engine failure during takeoff?

    <p>It improves takeoff performance.</p> Signup and view all the answers

    When will the spoiler 6 and ailerons be deflected during takeoff?

    <p>When pedal order is more than 2/3 of full pedal deflection and the speed is above 60 kt and pitch att below 2.5 , ground spoilers not activated and on ground</p> Signup and view all the answers

    Which of the following is NOT a condition for deflecting the spoiler 6 and ailerons during engine failure on ground

    <p>The speed is approximately 50 kt</p> Signup and view all the answers

    What happens to the bank angle when the sidestick is released at an angle greater than 33 °in normal law

    <p>The bank angle reduces to 33 °.</p> Signup and view all the answers

    How does the system respond when the sidestick is held at neutral up to a bank angle of 33 °?

    <p>The system holds the roll attitude constant.</p> Signup and view all the answers

    What is the maximum bank angle achieved with full lateral sidestick deflection?

    <p>67 °</p> Signup and view all the answers

    Which statement about spiral static stability is true?

    <p>It is maintained for bank angles greater than 33 °.</p> Signup and view all the answers

    What action must the PF take to maintain bank in steep turns?

    <p>Apply lateral pressure on the sidestick and aft pressure</p> Signup and view all the answers

    During steep turns, what must be done to maintain level flight?

    <p>Aft pressure on the sidestick is required</p> Signup and view all the answers

    What is the minimum bank angle required to qualify as a steep turn?

    <p>Greater than 33°</p> Signup and view all the answers

    What is the maximum bank angle when angle-of-attack protection is operative and full lateral deflection is maintained?

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

    What is prevented when high speed protection is active?

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

    What happens when the sidestick is released in high speed protection mode?

    <p>The aircraft returns to a bank angle of 0 °</p> Signup and view all the answers

    Which of the following describes the effect of high speed protection on spiral static stability?

    <p>It maintains positive spiral static stability from a bank angle of 0 °</p> Signup and view all the answers

    What occurs when the bank angle exceeds 45 ° during an angle of attack protection and bank angle protection ?

    <p>The autopilot disconnects and FD bars disappear.</p> Signup and view all the answers

    What happens to the FD bars when the bank angle decreases to less than 40 ° during bank angle protection .

    <p>The FD bars return.</p> Signup and view all the answers

    What is the status of auto trim when bank angle protection is active?

    <p>Auto trim is inactive.</p> Signup and view all the answers

    What color does the sideslip index change to on the PFD in the event of engine failure during takeoff?

    <p>Blue</p> Signup and view all the answers

    What is the expected pilot response when the beta target cannot be zeroed with full rudder during flight?

    <p>Accelerate to improve stability</p> Signup and view all the answers

    What state should the ailerons be in to achieve optimum climb performance after an engine failure?

    <p>Neutral</p> Signup and view all the answers

    What does the lateral normal law command to minimize sideslip during flight?

    <p>Rudder surface deflection</p> Signup and view all the answers

    What is the purpose of the PRIM during flight in the context of engine failure?

    <p>To compute and provide the beta target value</p> Signup and view all the answers

    Study Notes

    Ground Mode Lateral Control

    • Sidestick controls ailerons and roll spoilers.
    • Control surface deflection varies with aircraft speed.
    • Pedals control rudder directly.

    In-Flight Mode Lateral Control

    • Normal law combines ailerons, spoilers (except spoiler 1), and rudder for turn coordination.
    • Flight crew does not use rudder for turn coordination.
    • Flight control system limits roll rate & bank angle, coordinates turns, and dampens dutch roll.
    • Roll rate is proportional to sidestick deflection (max 15°/s).

    Flare Mode Lateral Control

    • Lateral control is the same as in "in flight" mode.

    Decrab Phase Lateral Control

    • Aircraft limits induced roll after pedal input to ease control.

    Transition Between Modes

    • Aircraft smoothly transitions to/from "in flight" and "ground" modes.

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    Description

    Test your knowledge on the various lateral control modes of aircraft operations. This quiz covers ground, in-flight, flare, and decrab phase lateral control, along with the transition between these modes. Discover how sidestick and pedal inputs affect roll and coordination in different flight phases.

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