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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 = 1000 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: 146 900 kg
  • MSLM + trip fuel: 93 800 + 27 500 = 121 300 kg
  • MZFM + take-off fuel: 86 400 + (35 500 - 1000) = 120 900 kg

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