Performance and flight planning - EASA PPL(A) Exam Prep

Which climb speed may be used to optimize the rate of climb (e.g. to reach a desired altitude within minimum time)?	4 Answers
For a take-off from runway 22 and a reported wind of 250°/10 kt, the longitudinal wind component equals...	4 Answers
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	4 Answers
For take-off on runway 36 with wind 240°/12 kt, what are the approximate wind components?	4 Answers
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)	4 Answers
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)	4 Answers
For landing on runway 36 with wind 240°/12 kt, which wind component combination applies?	4 Answers
Given the following conditions, the fuel consumption equals... Pressure altitude: 2000 ft Temperature: 31° C RPM: 2400 See annex (PFP-012)	4 Answers
Given the following conditions, the climb speed equals... Outside air temperature: -20° C Pressure altitude: 10000 ft See annex (PFP-011)	4 Answers
What range can be achieved at the following conditions? Outside air temperature: 6° C Pressure Altitude: 6000 ft Power: 65 % See annex (PFP-013)	4 Answers

Performance and flight planning - EASA PPL(A) - Private Pilot License