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Given:

Maximum Structural Take-off Mass: 8350 kg
Maximum Structural Landing Mass: 8350 kg
Zero Fuel Mass: 6210 kg
Taxi Fuel: 10 kg
Contingency Fuel: 90 kg
Alternate Fuel: 300 kg
Final Reserve Fuel: 400 kg
Trip Fuel: 780 kg

The expected Landing Mass at destination will be…

  • A
    7000 kg
  • B
    8350 kg
  • C
    7780 kg
  • D
    7790 kg

1) Take-off Fuel = 780 (trip) + 90 (conti) + 300 (alternate) + 400 (final res) => 1570 kg

2) Take-off Mass (TOM) = 6210 (ZFM) + 1570 (Take-off Fuel) => 7780 kg

3) Expected Landing Mass (LM) = 7 780 (TOM) - 780 (Trip Fuel) => 7000 kg

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