Regarding take-off, the take-off decision speed V1:4
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A lower airspeed at constant mass and altitude requires:4
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The point at which a tangent out of the origin touches the power required curve4
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The maximum indicated air speed of a piston engine aeroplane without turbo charger, in level flight, is reached:4
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A headwind component increasing with altitude, as compared to zero wind condition, (assuming IAS is constant):4
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At a given mass, the reference stall speed of a twin engine turboprop aircraft is 100 KT in the landing configuration. The minimum speed a pilot must maintain in short final is:4
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If other factors are unchanged, the fuel mileage (nautical miles per kg) is:4
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The angle of climb with flaps extended, compared to that with flaps retracted, will normally be:4
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The speed for maximum lift/drag ratio will result in:4
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The maximum rate of climb that can be maintained at the absolute ceiling is:4
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