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ATPL - Airline Transport Pilot license - Performance Page 12

Questions Performance - ATPL Page 12

Which combination of circumstances or conditions would most likely lead to a tyre speed limited take-off?4
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The minimum climb gradient required on the 2nd flight path segment after the take-off of a jet aeroplane is defined by the following parameters:1 Gear up2 Gear down3 Wing flaps retracted4 Wing flaps in take-off position 5 N engines at the take-off thrust6 (N- 1) engines at the take-off thrust7 Speed over the path equal to V2 + 10 kt 8 Speed over the path equal to 1.3 VS9 Speed over the path equal to V210 At a height of 35 ft above the runway The correct statements are:4
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Regarding the obstacle limited take-off mass, which of the following statements is correct?4
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The take-off mass of an aeroplane is restricted by the climb limit. What would be the effect on this limit of an increase in the headwind component?4
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For a jet aeroplane, the maximum climb angle is achieved at a speed corresponding to:4
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As long as an aeroplane is in a positive climb:4
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Two identical turbojet aeroplane (whose specific fuel consumptions are considered to be equal) are at holding speed at the same altitude.The mass of the first aircraft is 130000 kg and its hourly fuel consumption is 4300 kg/h. The mass of the second aircraft is 115000 kg and its hourly fuel consumption is:4
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Which data can be extracted from the Buffet Onset Boundary Chart?4
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With regard to the drift down performance of the twin jet aeroplane, what is meant by 'equivalent gross weight at engine failure'?4
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The intersections of the thrust available and the drag curve are the operating points of the aeroplane4
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