33-03. FUEL PLANNING
All questions: 158
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1. (Refer to figure 033-53)
Determine the estimated trip fuel and trip time using the simplified flight planning. Given:
Ground distance: 1.600 NM
Headwind component: 50 kts
Cruise: FL330
Mach 0,78
ISA +20 °С
Estimated landing weight: 55.000 kg
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2. The fuel burn – off is 200 kg/hrs with a relative fuel density of 0,8. If the relative fuel density is 0,75, the fuel burn will be:
3. Following in-flight depressurization, a turbine powered aeroplane is forced to divert to an enroute alternate airfield. If actual flight conditions are as forecast, the minimum quantity of fuel remaining on arrival at the airfield will be:
4. (Refer to figure 033-14)
Find the climb fuel. Given:
Mass at brake release: 57.500 kg
Temperature: ISA -10 °С
Average headwind component: 16 kts
Initial cruise: FL280
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5. (Refer to figure 033-16)
An aircraft climbs out from an aerodrome at MSL to FL250, under ISA +20 °С conditions. If the brake re lease weight is 60.000 kg, what is the fuel and ground distance covered with a 40 kts tailwind?
