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Performance - ATPL - Airline Transport Pilot license

Questions Performance - ATPL

Which of the following factors will lead to an increase of ground distance during a glide, while maintaining the appropriate minimum glide angle speed? 4 Answers Considering a rate of climb diagram (ROC versus TAS) for an aeroplane. Which of the diagrams shows the correct curves for 'flaps down' compared to 'clean' configuration? 4 Answers The climb gradient of an aircraft after take-off is 6% in standard atmosphere, no wind, at 0' pressure altitude. Using the following corrections: '± 0.2 % / 1000' field elevation'; '± 0.1 % / °C from standard temperature' '- 1 % with wing anti-ice'; '- 0.5% with engine anti-ice'. The climb gradient after take-off from an airport situated at 1000', 17°C; QNH 1013.25 hPa, with wing and engine anti-ice operating for a functional check is: 4 Answers The following parameters affect the take-off ground run: 1. decreasing take-off mass 2. increasing take-off mass 3. increasing density 4. decreasing density 5. increasing flap setting 6. decreasing flap setting 7. increasing pressure altitude 8. decreasing pressure altitude. Which parameters will decrease the take-off ground run? 4 Answers The determination of the maximum mass on brake release, of a certified turbojet aeroplane with 5°, 15° and 25° flap angles on take-off, leads to the following values: Flap angle: 5° 15° 25°; Runway limitation (kg): 66000 69500 71500; 2nd segment climb limitation: 72200 69000 61800; Wind correction: Headwind: +120 kg / KT Tailwind: -360 kg / KT; Given that the tailwind component is equal to 5 KT, the maximum mass on brake release and corresponding flap angle will be: 4 Answers The use of reduced take-off thrust is permitted, only if: 4 Answers Which statement about reduced thrust is correct? 4 Answers Field length is balanced when: 4 Answers In case of an engine failure which is recognized at or above V1: 4 Answers The speed V2 is defined for jet aeroplane as: 4 Answers

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