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PPL(A) English - Private Pilot License (Aircraft) - Performance and flight planning Page 6

Domande Performance and flight planning - Private Pilot (Aircraft)Page 6

Which climb speed may be used to optimize the rate of climb (e.g. to reach a desired altitude within minimum time)?4
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For a take-off from runway 22 and a reported wind of 250°/10 kt, the longitudinal wind component equals...4
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Given the following conditions, the take-off distance equals... Outside air temperature: -20° C Pressure Altitude: 5000 ft Aeroplane mass: 750 kg Headwind: 10 kt4
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A pilot wants to take off on runway 36, the reported wind is 240 degrees, 12 knots. What is the value of the wind components acting on the aircraft on take-off and landing?4
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What is the take-off distance at 750 kg take-off mass, standard (ISA) conditions at an elevation of 4000 ft with 5 kt tailwind? See annex (PFP-009) (1,00 P.) Siehe Anlage 94
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What is the take-off distance at 705 kg take-off mass, OAT 20° C, QNH 1013 hPa at an elevation of 3500 ft with 5 kt tailwind? See annex (PFP-009) (1,00 P.) Siehe Anlage 94
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A pilot wants to take off on runway 36, the reported wind is 240 degrees 12 knots. What are the wind components acting on the aircraft on take-off and landing?4
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Given the following conditions, the fuel consumption equals... Pressure altitude: 2000 ft Temperature: 31° C RPM: 2400 See annex (PFP-012) (1,00 P.) Siehe Anlage 104
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Given the following conditions, the climb speed equals... Outside air temperature: -20° C Pressure altitude: 10000 ft See annex (PFP-011) (1,00 P.) Siehe Anlage 114
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What range can be achieved at the following conditions? Outside air temperature: 6° C Pressure Altitude: 6000 ft Power: 65 % See annex (PFP-013) (1,00 P.) Siehe Anlage 124
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PPL(A) English - Private Pilot License (Aircraft)Allenamento!
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