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Transport i infrastruktura · 1.12.2011

Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures

This rule revises airworthiness standards for type certification requirements of normal and transport category rotorcraft. The amendment requires evaluation of fatigue and residual static strength of composite rotorcraft structures using a damage tolerance evaluation, or a fatigue evaluation if the applicant establishes that a damage tolerance evaluation is impractical. The amendment addresses advances in composite structures technology and provides internationally harmonized standards.

Source: Federal Register — Transportation DepartmentOpen original release →