33-03. (H) FUEL PLANNING
Всего заданий: 35
В режиме ОБУЧЕНИЕ показываются все задания дисциплины с предъявлением правильных ответов. Для перехода к следующему заданию нажать кнопку «Далее».
Заданий на экзамен: 30
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1. Given:
Dry Operating Mass (DOM): 33.500 kg
Load: 7.600 kg
Maximum Allowable Takeoff Mass: 66.200 kg
Standard taxi fuel: 200 kg
Tank capacity: 16.100 kg
The maximum possible takeoff fuel is:
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2. For a flight to an offshore platform, an alternate aerodrome is compulsory, except if:
1) flight duration does not exceed two hours
2) during the period from two hours before to two hours after the estimated landing time, the forecast conditions of ceiling and visibility are not less than one and a half times the applicable minima
3) the platform is available and no other flight either from or to the platform is expected between the estimated time of departure and one half hour after the estimated landing time
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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 033-40) Using the following information, calculate the range. Given: Aeroplane mass at start up: 3.663 lbs Fuel load (density 6 lbs/gal): 74 gal Takeoff altitude: sea level Headwind: 40 kts Cruise altitude: 8.000 ft Power setting: full throttle 2.300 RPM 20 °С lean of peak
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5. To carry out a VFR flight to an off-shore platform, the minimum fuel quantity on board is:
