During landing of a low-winged jet aeroplane, the greatest elevator up deflection is normally required when the flaps are:4
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The 'short period mode' is an:4
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The aerodynamic contribution to the static longitudinal stability of the nacelles of aft fuselage mounted engines is:4
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The effect of a ventral fin on the static stability of an aeroplane is as follows: (1=longitudinal, 2=lateral, 3=directional)4
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Static lateral stability should not be too small, because:4
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Which of the following statements concerning control is correct?4
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Examples of aerodynamic balancing of control surfaces are:4
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What should be usually done to perform a landing with the stabilizer jammed in the cruise flight position ?4
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Increase of the delta load factor due to a given vertical upgust at a given EAS occurs when:4
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Does the pitch angle of a constant speed propeller alter in medium horizontal turbulence?4
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