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An aircraft is performance limited to a landing mass of 7550 kg.
The Basic Empty Mass is 5200 kg, the Dry Operating Mass is 5500 kg and the Zero Fuel Mass is 5980 kg. If the take-off mass is 7980 kg, the traffic load is:
  • A
    480 kg.
  • B
    2480 kg.
  • C
    2780 kg.
  • D
    2000 kg.
Zero Fuel Mass (ZFM) = Dry Operating Mass (DOM) + Traffic Load (TL)
Traffic load = ZFM - DOM = 5980 - 5500 = 480 kg

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