During a glide at constant Mach number, the pitch angle of the aeroplane will:4
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Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT 24 °CPressure Altitude: 3000 ft RWY 30RWind· 060/04 KTTake-off Mass: 3800 lbsOther conditions as associated in the header of the graph. What is the Ground Roll Distance under the conditions given?4
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Density Altitude:4
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The rate of climb:4
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If the aircraft mass, in a horizontal unaccelerated flight, decreases:4
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When compared to still air conditions, a constant headwind component:4
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The pilot of a single engine aircraft has established the climb performance.The carriage of an additional passenger will cause the climb performance to be:4
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The maximum speed in horizontal flight occurs when:4
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The result of a higher flap setting up to the optimum at take-off is:4
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A twin engine aeroplane in cruise flight with one engine inoperative has to fly over high ground. In order to maintain the highest possible altitude the pilot should choose:4
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