33-03. FUEL PLANNING
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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:
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2. An operator shall ensure that calculation of usable fuel for an IFR flight with a turbojet aeroplane for which no destination alternate is required includes, taxi fuel, Trip Fuel, contingency fuel and fuel to fly for:
3. When calculating the fuel required to carry out a given flight, one must take into account: 1) the wind 2) foreseeable airborne delays 3) other weather forecasts 4) any foreseeable conditions which may delay landing The combination which provides the correct statement is:
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4. (Refer to figure 033-47)
In order to find alternate fuel and time to alternate, the aeroplane operating manual shall be entered with:
5. (Refer to figure 033-50)
For a flight of 2.800 ground nautical miles the following applies:
Headwind component: 15 kts
Temperature: ISA + 15 °С
Cruise altitude: 35.000 ft
Landing Mass: 50.000 kg
The Trip Fuel and trip time respectively are:
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