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Given:

Dry Operating Mass = 38 000 kg
Maximum Structural Take-off Mass = 72 000 kg
Maximum Landing Mass = 65 000 kg
Maximum Zero Fuel Mass = 61 000 kg
Trip Fuel = 8 000 kg Take-off Fuel = 10 300 kg

The maximum allowed take-off mass and traffic load are respectively:

  • A
    71 300 kg and 23 000 kg
  • B
    73 000 kg and 24 700 kg
  • C
    71 300 kg and 25 300 kg
  • D
    73 000 kg and 27 000 kg

First we need to get actual TOM which is the smallest of:

1- MSTOM: 72000 kg
2- MLM + trip fuel (as trip fuel will be consumed during the flight): 65000 + 8000 = 73000 kg
3- MZFM + total fuel = 61000 + 10300 = 71300 kg (Actual TOM)(smallest number)

Traffic load = TOM — (DOM + Takeoff fuel) = 71300 — (38000 + 10300) = 23000 kg

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