31-02. LOADING
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1. Given:
Dry Operating Mass: 29.800 kg
Maximum Takeoff Mass: 52.400 kg
Maximum Zero Fuel Mass: 43.100 kg
Maximum Landing Mass: 46.700 kg
Trip Fuel: 4.000 kg
Fuel quantity at brakes release: 8.000 kg
The maximum Traffic Load is:
2. The Maximum Certificated Takeoff Mass is:
3. Determine the Zero Fuel Mass for the following single engine aeroplane. Given:
Standard Empty Mass: 1.764 lbs
Optional Equipment: 35 lbs
Pilot + Front seat passenger: 300 lbs
Cargo Mass: 350 lbs
Ramp Fuel (Block Fuel): 60 Gal
Trip Fuel: 35 Gal
Fuel density: 6 lbs/Gal
4. The following data is extracted from an aeroplane loading manifest:
Performance Limited Takeoff Mass: 93.500 kg
Expected Landing Mass at destination: 81.700 kg
Maximum Certificated Landing Mass: 86.300 kg
Fuel on board: 16.500 kg
During the flight a diversion is made to an enroute alternate which is not performance limited for landing.
Fuel remaining at landing is 10.300 kg.
The Landing Mass:
5. Which of the following alternatives corresponds to Zero Fuel Mass?
