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

Aircraft fatigue life is most directly affected by:

Steady cruise loads only The number and magnitude of cyclic (fluctuating) loads The static ultimate load applied once Outside air temperature during cruise

Correct Answer:

The number and magnitude of cyclic (fluctuating) loads

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