On an aircraft, the Krueger flap is a:4
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The reason for the trim switch on a control column to consist of two separate switches is4
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On an aeroplane, spoilers are:4
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One design method to avoid control surface flutter is:4
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For most large aeroplanes, spoilers are:4
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To achieve control flutter damping the balance mass must be located:4
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Which of these statements about structure design principles are correct or incorrect? 1) In structural design, FAIL SAFE implies redundant load paths. 2) A SAFE LIFE structure is based on a declared number of cycles or time period.4
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According EASA CS25 the worst effect of a MINOR FAILURE on the occupants of an aeroplane excluding flight crew could be:4
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The principle of the SAFE LIFE design of an aircraft is based on the:4
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According EASA CS25 the worst effect of a MAJOR FAILURE on the flight crew could be:4
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