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
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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
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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°C4
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The following parameters affect the take off ground run: 1 decreasing take off mass2 increasing take off mass 3 increasing density4 decreasing density5 increasing flap setting 6 decreasing flap setting7 increasing pressure altitude 8 decreasing pressure altitudeWhich parameters will decrease the take off ground run?4
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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 715002nd segment climb limitation: 72200 69000 61800Wind correction:Headwind: +120 kg / KT Tailwind: -360 kg / KTGiven that the tailwind component is equal to 5 KT, the maximum mass on brake release and corresponding flap angle will be:4
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The use of reduced take-off thrust is permitted, only if:4
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Which statement about reduced thrust is correct?4
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Field length is balanced when:4
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In case of an engine failure which is recognized at or above V1:4
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The speed V2 is defined for jet aeroplane as:4
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