FAA AC 20-107:2009

FAA AC 20-107:2009 Composite Aircraft Structure Specifies an acceptable means, but not the only means of showing compliance with the provisions of Title 14 of the Code of Federal Regulations (14 CFR) parts 23, 25, 27, and 29 regarding airworthiness

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Table of Contents

1.PurposeofthisAdvisoryCircular(AC)
2.ToWhomthisACApplies
3.Cancellation
4.RelatedRegulationsandGuidance
5.General
6.MaterialandFabricationDevelopment
7.ProofofStructure-Static
8.ProofofStructure-FatigueandDamageTolerance
9.ProofofStructure-FlutterandOtherAeroelastic
Instabilities
10.ContinuedAirworthiness
11.AdditionalConsiderations
Appendix1-ApplicableRegulationsandRelevantGuidance
Appendix2-Definitions
Appendix3-ChangeofCompositeMaterialand/orProcess

Abstract

Specifies an acceptable means, but not the only means of showing compliance with the provisions of Title 14 of the Code of Federal Regulations (14 CFR) parts 23, 25, 27, and 29 regarding airworthiness type certification requirements for composite aircraft structures involving fiber reinforced materials, e.g., carbon and glass fiber reinforced plastics.

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