Contact|RisingUp Home


Federal Aviation Regulations

Sec. 23.627 — Fatigue strength.

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.

NEXT: Sec. 23.629 - Flutter.
PREVIOUS: Sec. 23.625 - Fitting factors.

Search the FARS for