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Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 This proposal would revise airworthiness standards for type certification requirements of normal and transport category rotorcraft. The amendment would require 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 would address advances in composite structures technology and provide internationally harmonized standards. This book contains: - The complete text of the Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section