33-03. FUEL PLANNING
All questions: 18
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Questions for exams: 15
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1. (Refer to figure 033-41) Given: Cruising: FL75 Mixture: lean Full throttle: 2.300 RPM Takeoff fuel: 444 lbs Takeoff from: MSL Find endurance in hours:
2. The fuel burn of an aircraft turbine engine is 220 l/hr with a fuel density of 0,80. If the density is 0,75, the fuel burn will be:
3. Given the following data determine the maximum possible takeoff fuel: Fuel density: 0,78 kg/l Dry Operating Mass: 33.500 kg Traffic Load: 10.600 kg Maximum Allowable Takeoff Mass: 66.200 kg Taxi Fuel: 200 kg Tank capacity:22.500 litres
4. (Refer to figure 033-42) A flight is to be made from one airport (elevation 3.000 ft) to another in a multi-engine piston aeroplane. The cruising level will be FL110. The temperature at FL110 is ISA-10 °С. The temperature at the departure aerodrome is -1 °С. Calculate the fuel to climb with mixture rich.
5. (Refer to figure 033-42) What is the fuel, time and distance to climb from an aerodrome at sea level up to FL100 where the outside air temperature is 0 °С?
