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The take-off mass of an aeroplane is 117 000 kg, comprising a traffic load of 18 000 kg and fuel of 46 000 kg. What is the Dry Operating Mass?
  • A
    53 000 kg
  • B
    99 000 kg
  • C
    64 000 kg
  • D
    71 000 kg
Dry Operating mass = TOM — [traffic load + useable fuel]
DOM = 117000 — [18000 +46000] = 53000 kg

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