An artificial feel unit is necessary in the pitch channel of a flight control system when:4
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On a large transport aeroplane, the auto-slat system:4
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Which of these statements about rudder limiting are correct or incorrect? 1) A rudder ratio changer system reduces the rudder deflection for a given rudder pedal deflection as the IAS increases. 2) A variable stop system limits both rudder and rudder pedal deflection as the IAS decreases.4
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An aeroplane equipped with reversible flight controls:4
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On an airplane, the Krueger flaps are:4
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Which of these statements about rudder limiting are correct or incorrect? 1) A rudder ratio changer system reduces the rudder deflection for a given rudder pedal deflection as the IAS decreases. 2) A variable stop system limits both rudder and rudder pedal deflection as the IAS increases.4
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The purpose of a trim tab (device) is to:4
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The advantages of fly-by-wire control: are 1. reduction of the electric and hydraulic power required to operate the control surfaces2. lesser sensitivity to lightning strike3. direct and indirect weight saving through simplification of systems4. immunity to different interfering signals5. improvement of piloting quality throughout the flight envelop The combination regrouping all the correct statements is:4
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An artificial feel unit is necessary in the pitch channel when:4
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In a steep turn to the left, when using spoilers ...4
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