31-02. LOADING
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1. The Basic Empty Mass is 4.960 kg, the Dry Operating Mass is 5.220 kg and the Zero Fuel Mass is 6.040 kg. If the Takeoff Mass is 7.630 kg the Useful Load is:
2. If the Maximum Structural Landing Mass is exceeded:
3. Define the Useful Load:
4. 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
5. The true Dry Operating Mass is the:
