FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 23 > Section 627 - Fatigue strength
section 23.625 |
section 23.629

The structure must be designed, as far as practicable, to avoid points of stress concentration where variable stresses above the fatigue limit are likely to occur in normal service.
  
Current page: FARs > Part 23 > Section 627 - Fatigue strength
section 23.625 |
section 23.629

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