During a descent at constant Mach number, the margin to low speed buffet will:4
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Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT -15 °CPressure Altitude: 4000' RWY 12RWind· 080/12 KTTake-off Mass: 4000 lbs Runway Surface: tarred and dryWhat is the minimum runway length? No stopway or clearway is available.4
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Density altitude is the:4
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What is the equation for the climb gradient expressed in percentage during unaccelerated flight (applicable to small angles only)?4
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With regard to an unaccelerated horizontal flight, which of the following statements is correct?(no compressibility effects)4
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A constant headwind:4
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If there is a tail wind, the climb limited TOM will:4
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What is the effect of increased mass on the performance of a gliding aeroplane?4
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Considering TAS for maximum range and maximum endurance, other factors remaining constant:4
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Which of the following provides maximum obstacle clearance during climb?4
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