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Fatigue in a shotgun is far less likely than say, a helicopter blade or any airframe parts experiencing harmonic and reversible loads. From an airframe design standpoint you use far lower allowable stress factors to improve the fatigue life than you would for conventional propulsion system.
For example, the wings on an F-105 are getting nearly 30,000 hours before major repairs/replacement due to stress/fatigue failures
Loads on a shotgun due to firing are neither harmonic nor reversible per se. More common is the wear and tear on hinge pins, top levers, action blocks, peening of firing pins, etc
For example, the wings on an F-105 are getting nearly 30,000 hours before major repairs/replacement due to stress/fatigue failures
Loads on a shotgun due to firing are neither harmonic nor reversible per se. More common is the wear and tear on hinge pins, top levers, action blocks, peening of firing pins, etc