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EN Flight Performance and Planning - EASA PPL(A) - Private Pilot Licence (Aeroplane)
Questions Flight Performance and Planning - EASA PPL(A) aeroplane theory
Which climb speed may be used to optimize the rate of climb (e.g. to reach a desired altitude within minimum time)?
Assuming runway magnetic direction 220° and a wind from magnetic direction 250° at 10 kt, what is the approximate longitudinal wind component?
Given the following conditions, the take-off distance equals... Outside air temperature: -20° C Pressure Altitude: 5000 ft Aeroplane mass: 750 kg Headwind: 10 kt
For runway magnetic direction 360° and wind from magnetic direction 240° at 12 kt, what are the approximate components?
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)
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)
For landing on runway magnetic direction 360° with wind from magnetic direction 240° at 12 kt, which component combination applies?
Given the following conditions, the fuel consumption equals... Pressure altitude: 2000 ft Temperature: 31° C RPM: 2400 See annex (PFP-012)
Using PFP-011, approximately what rate of climb is shown at OAT −20 °C and pressure altitude 10 000 ft?
What range can be achieved at the following conditions? Outside air temperature: 6° C Pressure Altitude: 6000 ft Power: 65 % See annex (PFP-013)
