EASA ATPL 021 AGK Practice Questions - EASA ATPL Theory - Aircraft General Knowledge Airframe, Systems, Electrics And Powerplant (021) Exam

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A structure designed so that, after the failure of a single principal structural member, the remaining structure can carry the limit load without catastrophic failure, is described as:

Safe-life Damage-tolerant Fail-safe Stiffness-critical

Correct Answer:

Fail-safe

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