Fatigue testing encompasses the cyclic loading of airframe structures, landing gear assemblies, rotorcraft components, and fastener joints to characterise crack initiation, propagation rates, and residual strength under representative flight-load spectra, applying methodologies such as constant-amplitude and variable-amplitude testing, da/dN analysis, S-N curve generation, and compliance with ASTM, JSSG, and FAR/CS fatigue certification requirements.
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