33-03. FUEL PLANNING
All questions: 50
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Questions for exams: 30
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1. (Refer to figure 033-02) Given: •FL75 • OAT +10 °С • 23,0 in. Hg (or full throttle) at 2.300 RPM Find the fuel flow in gallons per hour (GPH) and TAS.
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2. You are required to uplift 40 US Gallons of AVGAS with specific gravity of 0,72. How many litres and kilograms is this?
3. A turbine-engine aircraft burns fuel at 200 gallons per hour (GPH) with a Fuel Density of 0,8. What is the fuel flow if Fuel Density is 0,75?
4. Given:
Maximum Allowable Takeoff Mass: 64.400 kg
Maximum Landing Mass: 56.200 kg, Maximum Zero Fuel Mass: 53.000 kg
Dry Operating Mass: 35.500 kg, Estimated load: 14.500 kg
Estimated Trip Fuel: 4.900 kg, Minimum takeoff fuel: 7.400 kg
Find maximum additional load:
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5. (Refer to figure 033-65) Finish the endurance / fuel calculations and determine ATC endurance for a twin jet aeroplane, with the help of the table provided. Contingency is 5% of the planned Trip Fuel and fuel flow for extra fuel is 2.400 kg/hr:
