A climb gradient required is 3.3%. For an aircraft maintaining 100 KT true airspeed, no wind, this climb gradient corresponds to a rate of climb of approximately:4
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With an true airspeed of 194 KT and a vertical speed of 1000 fpm, the climb gradient is about:4
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Which of the following answers is true?4
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During certification flight testing on a four engine turbojet aeroplane the actual take-off distances measured are:3050 m with failure of the critical engine recognised at V12555 m with all engines operating and all other things being equal The take-off distance adopted for the certification file is:4
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Reduced take-off thrust should normally not be used when:4
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Which statement is correct?4
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The speed V2 is:4
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Can the length of a stopway be added to the runway length to determine the takeoff distance available?4
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If the take-off mass of an aeroplane is brake energy limited a higher uphill slope would:4
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In which of the following distances can the length of a stopway be included?4
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