Take-off performance data, for the ambient conditions, show the following limitations with flap 10° selected: - runway limit: 5270 kg - obstacle limit: 4630 kg. Estimated take-off mass is 5000 kg. Considering a take-off with flaps at:4
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What effect has a tailwind on the maximum endurance speed?4
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Maximum Tyre Speed can limit the Lift-off Speed. Which kind of speed can be directly used to determine this limitation?4
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A higher pressure altitude at ISA temperature:4
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An aeroplane executes a steady glide at the speed for minimum glide angle. If the forward speed is kept constant, what is the effect of a lower mass? Rate of descent / Glide angle / CL / CD ratio4
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Which of the following factors leads to the maximum flight time of a glide?4
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An aircraft has two certified landing flaps positions, 25° and 35°. If a pilot chooses 25° instead of 35°, the aircraft will have:4
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If accelerate-stop distance data assume take-off power is set before brake release, will the published accelerate-stop distance still be achieved if the brakes are released before take-off power is set?4
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What is the result of a large take-off flap setting compared to a small take-off flap setting on required Take-off Distance (TOD) and the field length limited Take-off Mass (TOM)?4
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During certification test flights for a turbojet aeroplane, the actual measured take-off runs from brake release to a point equidistant between the point at which VLOF is reached and the point at which the aeroplane is 35' above the take-off surface are: - 1747 m, all engines operating; - 1950 m, with the critical engine failure recognized at V1, the other factors remaining unchanged. Considering both possibilities to determine the take-off run (TOR). What is the correct distance?4
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Other exam subjects ATPL - Airline Transport Pilot license