According EASA CS-25 the worst effect of a CATASTROPHIC FAILURE on the flight crew could be:4
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Which of these statements about structural design principles are correct or incorrect? 1) The DAMAGE TOLERANCE principle takes cracking of the structure into account. 2) The SAFE LIFE principle is based on the replacement of parts after a given number of cycles or flight hours.4
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The principle of FAIL SAFE design of an aircraft is based on the:4
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According EASA CS the worst effect of a HAZARDOUS FAILURE on the occupants of an aeroplane excluding flight crew could be:4
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According to EASA CS-25 failure-condition classifications, the worst effect of a MAJOR failure condition on occupants excluding flight crew may be:4
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According to EASA CS-25 failure-condition classifications, the worst effect of a MINOR failure condition on the aeroplane may be:4
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A SAFE LIFE aircraft structural component:4
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According to EASA CS-25 failure-condition classifications, the worst effect of a MINOR failure condition on the flight crew may be:4
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According to EASA CS-25 failure-condition classifications, the worst effect of a MAJOR failure condition on the aeroplane may be:4
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The reason for the fact that an aeroplane designed for long distances cannot simply be used for short haul flights at higher frequencies is that4
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Other exam subjects ATPL - Airline Transport Pilot license