← All ADX Flashcard Decks

ADX Aircraft Performance and Weight Balance Flashcards

6 cards from real ADX practice questions. Tap to flip, then mark Knew It or Still Learning — missed cards come back until you master them.

Read the first 6 ADX Aircraft Performance and Weight Balance flashcards as text
  1. What is the primary purpose of a weight-and-balance manifest?

    Answer: To verify the aircraft's load distribution keeps the CG within certified limits before departure

    The weight-and-balance manifest documents how load is distributed so the dispatcher and captain can confirm the CG falls within safe limits prior to release.

  2. What is 'operating empty weight' (OEW)?

    Answer: Weight of the aircraft including crew, oil, and unusable fuel but excluding payload and usable fuel

    OEW includes the airframe, powerplants, fixed equipment, crew, operating fluids, and unusable fuel — the baseline before adding payload or usable fuel.

  3. Which factor is NOT a standard input for aircraft takeoff performance calculations?

    Answer: The age distribution of passengers aboard

    Passenger age has no bearing on performance calculations; temperature, altitude, and wind are the standard environmental inputs used in performance charts.

  4. What does 'payload' mean in aircraft weight terminology?

    Answer: The revenue-generating weight consisting of passengers, baggage, and freight

    Payload is the revenue portion of useful load — passengers, baggage, and cargo — and directly determines profitability of the flight.

  5. What is the primary hazard when an aircraft departs with its CG aft of the approved limit?

    Answer: The aircraft becomes pitch-unstable and may pitch up uncontrollably

    An aft CG beyond limits reduces or eliminates the nose-down pitching moment, making the aircraft dangerously unstable and potentially uncontrollable in pitch.

  6. What is 'maximum landing weight' (MLW)?

    Answer: The maximum weight at which the aircraft structure is certified to sustain a landing impact

    MLW is set by structural analysis of landing loads; exceeding it risks damaging the airframe, landing gear, or wing structure during touchdown.