Which statement is correct for a side slip condition at constant speed and side slip angle, where the geometric dihedral of an aeroplane is increased ?4
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Rolling is the rotation of the aeroplane about the:4
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An example of differential aileron deflection during initiation of left turn is:4
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If the nose of an aeroplane yaws left, this causes:4
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Which statement about a jet transport aeroplane is correct during take-off with the cg at the forward limit and the trimmable horizontal stabiliser (THS) positioned at the maximum allowable aeroplane nose down position?4
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Which load factor determines VA?4
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The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.4. An increase in angle of attack of 1 degree will increase CL by 0.09. A vertical up gust instantly changes the angle of attack by 5 degrees. The load factor will be:4
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Which of the following statements is true?4
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If you increase the propeller pitch during a glide with idle-power at constant IAS the lift to drag ratio will4
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The correct drag formula is:4
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