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

The limit load of an aircraft structure is defined as:

The load at which the structure fails completely The maximum load expected in normal service operation The limit load multiplied by the safety factor The load that produces 50% permanent deformation

Correct Answer:

The maximum load expected in normal service operation

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