33-03. FUEL PLANNING
Всего заданий: 158
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Заданий на экзамен: 30
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1. (Refer to figure 033-28) For a long distance flight at FL390, «Long Range» regime, divided into four flight legs with the following characteristics: Leg 1 Ground distance: 2.000 NM, Headwind component: 50 kts Leg 2 Ground distance: 1.000 NM, Headwind component: 30 kts Leg 3 Ground distance: 500 NM, Tailwind component: 100 kts Leg 4 Ground distance: 1.000 NM, Headwind component: 70 kts The air distance of the entire flight is approximately:
.
2. (Refer to figures 033-35 and 033-36) In standard atmosphere, assuming a mass of 197.500 kg, in order to fly at FL370 and to be at the optimum altitude, your Mach number should be:
3. (Refer to figure 033-47)
Using the simplified flight planning (alternate planning), find fuel required and trip time to alternate. Given:
Dry Operating Mass: 35.500 kg
Traffic Load: 14.500 kg
Final reserve fuel: 1.200 kg
Distance to alternate: 95 NM
Tailwind component: 10 kts
.
4. The required time for final reserve fuel for turbojet aeroplane is:
5. (Refer to figure 033-54)
What is the fuel required, given the following information?
Distance: 350 NM
Cruise: 300 KIAS
FL210
Tailwind component: 70 kts
Landing Mass: 53.000 kg
