The centre of gravity near, but still within, the aft limit:4
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The speed for maximum endurance4
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On a long distance flight the gross mass decreases continuously as a consequence of the fuel consumption. The result is:4
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To minimize the risk of hydroplaning during landing the pilot should:4
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Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT 24 °CPressure Altitude: 3000' RWY, 12LWind· 080/12 KTTake-off Mass: 3800 lbsOther conditions as associated in the header of the graph. What is the take-off distance over a 50 ft obstacle?4
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Which of the following is true according to regulations for turbo propeller powered aeroplanes not performing a steep approach?4
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The approach climb requirement has been established to ensure:4
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According to CS 25 the landing reference speed VREF may not be less than:4
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Is there any difference between the vertical speed versus forward speed curves for two identical aeroplanes having different masses ? (assume zero thrust and wind)4
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According to PART-CAT, for turbo-prop aeroplanes, the required runway length at a destination airport is:4
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