EASA ATPL Package (former JAA) Mass and Balance

Load and Trim Sheet

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Question 9501
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The following data relates to a planned flight of an aeroplane - Dry Operating Mass 60520 kg, Performance limited take-off mass 92750 kg, Performance limited landing mass 72250 kg, Maximum Zero Fuel mass 67530 kg, Fuel on board at take - off - Trip Fuel: 12 500 kg, Contingency and final reserve fuel 2300 kg, Alternate Fuel 1700 kg. Using this data, as appropriate, calculate the maximum traffic load that can be carried.
A
15 730 kg
B
11 730 kg
C
7 730 kg
D
7 010 kg