9 / 20

Given:

Maximum structural take-off mass = 146 900 kg
Maximum structural landing mass = 93 800 kg
Maximum Zero Fuel Mass = 86 400 kg
Trip fuel = 27 500 kg
Block fuel = 35 500 kg
Engine starting and taxi fuel = 1 000 kg

The Maximum Take-off Mass is equal to:

  • A
    120 300 kg
  • B
    113 900 kg
  • C
    121 300 kg
  • D
    120 900 kg
Maximum allowable takeoff mass is the smallest of :
  • MSTOM: 146900 kg
  • MSLM + trip fuel: 93800 + 27500 = 121300 kg
  • MZFM + takeoff fuel: 86400 + (35500 — 1000) = 120900 kg

Your Notes (not visible to others)



This question has appeared on the real examination, you can find the related countries below.