Maneuver Load Alleviation (MLA) A 330
7 Questions
0 Views

Choose a study mode

Play Quiz
Study Flashcards
Spaced Repetition
Chat to lesson

Podcast

Play an AI-generated podcast conversation about this lesson

Questions and Answers

What is the primary purpose of MLA in aircraft operation?

  • To increase engine power for better performance
  • To redistribute lift and relieve structural loads on the outer wing surfaces (correct)
  • To improve fuel efficiency during flight
  • To enhance passenger comfort during turbulence
  • Under what conditions does the MLA become active?

  • When the ailerons are symmetrically deflected upwards
  • When the aircraft speed is below 250 kt and flaps are deployed
  • When the aircraft is in a steep climb
  • When the sidestick is pulled more than 8° and the load factor is more than 2 g (correct)
  • Which surfaces are utilized by the MLA to relieve structural loads?

  • Ailerons and flaps only
  • Elevators and rudder only
  • Spoilers 4, 5, 6 and ailerons (correct)
  • All wing surfaces equally
  • What happens to the ailerons when MLA is activated?

    <p>They are symmetrically deflected upwards, adding up to 11° to roll demand</p> Signup and view all the answers

    What condition is NOT required for load alleviation to be available?

    <p>The aircraft is below 10,000 feet altitude</p> Signup and view all the answers

    What maximum additional roll demand can be caused by the symmetrical deflection of spoilers 4, 5, and 6?

    <p>9 °</p> Signup and view all the answers

    What is the relationship between the deflection of spoilers and the load factor during MLA activation

    <p>Deflection is proportional to the load factor, above 2 g.</p> Signup and view all the answers

    Study Notes

    Meaningful Load Alleviation (MLA) System

    • MLA redistributes lift over the wing, reducing bending moment on outer wing surfaces while maintaining the desired load factor.
    • MLA uses spoilers 4, 5, and 6, and ailerons.
    • MLA activates when the sidestick is pulled more than 8° and load factor exceeds 2 g.
    • Ailerons deflect symmetrically upward, up to a maximum of 11° (additional roll demand).
    • Spoilers 4, 5, and 6 deflect symmetrically, adding up to a maximum of 9° (additional roll demand). Deflection increases proportionally with load factor above 2 g.
    • Elevator control simultaneously compensates for pitching moments from spoilers and ailerons.
    • Load alleviation is available if: Aircraft speed is above 250 kt. FLAPS lever is in the "0" position. Normal or alternate law flight mode selected.
    • MLA has priority over the speedbrakes.

    Studying That Suits You

    Use AI to generate personalized quizzes and flashcards to suit your learning preferences.

    Quiz Team

    Description

    Test your knowledge on the Meaningful Load Alleviation (MLA) system, which redistributes lift to reduce bending moments on aircraft wings. This quiz covers the functionality, activation conditions, and control mechanisms of the MLA system. Ensure you understand how it interacts with flight controls and operational limits.

    More Like This

    Load Classifications in Structures
    6 questions
    08 Load Balancers Overview GHP ✓
    21 questions

    08 Load Balancers Overview GHP ✓

    DecisiveGreatWallOfChina1467 avatar
    DecisiveGreatWallOfChina1467
    Use Quizgecko on...
    Browser
    Browser