31-02. LOADING
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1. At the flight preparation stage, the following parameters in particular are available for determining the mass of the aircraft: 1) Dry Operating Mass 2) Operating Mass Which statement is correct?
2. A MRJT is about to make a scheduled European flight, using the following information calculate the most limiting TOM for the aircraft:
MZFM: 56.000 kg
MLM: 58.600 kg
MTOM: 66.800 kg
PLLM: 59.000 kg
PLTOM: 65.000 kg
Takeoff Fuel: 13.400 kg
Trip Fuel: 8.100 kg
3. The Maximum Zero Fuel Mass is:
4. Given:
Zero Fuel Mass: 4.920 kg
Trip Fuel: 880 kg
Block Fuel: 1.330 kg
Taxi Fuel: 25 kg
The actual Takeoff Mass is equal to:
5. Given:
Maximum Structural Takeoff Mass: 146.000 kg
Maximum Structural Landing Mass: 93.900 kg
Actual Zero Fuel Mass: 86.300 kg
Trip Fuel: 27.000 kg
Taxi Fuel: 1.000 kg
Contingency Fuel: 1.350 kg
Alternate Fuel: 2.650 kg
Final Reserve Fuel: 3.000 kg
Determine the actual Takeoff Mass:
