Design/Certification Considerations in Civil Composite Aircraft Structure

871846

10/01/1987

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
Federal Aviation Administration (FAA) Advisory Circular AC 20-107A, Composite Aircraft Structure, issued in 1984 provides updated guidance material for use in demonstrating compliance with the provisions of the applicable Federal Aviation Regulations, (FAR) regarding airworthiness type certification requirements for composite aircraft structure. This paper identifies and reviews a number of issues related to each of the major sections of this advisory circular that have been given special consideration in recent certification programs. Specific recommendations are given in each case.
Meta TagsDetails
DOI
https://doi.org/10.4271/871846
Pages
10
Citation
Soderquist, J., "Design/Certification Considerations in Civil Composite Aircraft Structure," SAE Technical Paper 871846, 1987, https://doi.org/10.4271/871846.
Additional Details
Publisher
Published
Oct 1, 1987
Product Code
871846
Content Type
Technical Paper
Language
English