Given an aeroplane with irreversible primary flight controls, how is control maintained if one hydraulic system is lost due to a hydraulic leak?4
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The purpose of the primary stops in a flying control system is to:4
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The expression "secondary flight control" applies to the: 1) elevator 2) speed brake 3) lift-augmentation devices 4) roll spoilersThe combination that regroups all of the correct statements is:4
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The expression "secondary flight control" applies to the: 1) trimmable stabilizer 2) rudder 3) speed brake 4) aileronThe combination that regroups all of the correct statements is:4
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The Ram Air Turbine (RAT) provides emergency hydraulic power for:4
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Which of these statements about a gust lock system are correct or incorrect? 1) A gust lock can be used in flight to reduce the effects of turbulence. 2) There is no need for a gust lock on reversible flight controls.4
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What is the name of the control surface that rotates an aeroplane about its longitudinal axis?4
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Given a conventional transport aeroplane with irreversible flight controls on the ground with engines running. Which of these statements about rudder trim actuation is correct?4
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An aeroplane equipped with fully powered flight controls (irreversible type):4
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Aircraft is descending in straight flight with the spoilers deployed. If a pilot initiates a descending turn to the left the:4
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