This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Recognition of Damage - Tolerance in Civil Airworthiness Standards
Annotation ability available
Sector:
Event:
Aerospace Meeting
Language:
English
Abstract
Amendments relating to the structural fatigue evaluation requirements are described. The amendments improve and update the air-worthiness standards applicable to the type certification of civil transport category airplanes. They take into account state-of-the-art developments and accumulated service experience. The authority for and origin of the related rules is also briefly traced. The interest in world-wide acceptance of these new standards is noted.
Recommended Content
Technical Paper | A Paradigm for Developing Operational Decision-Making (ODM) Training |
Technical Paper | AIRCRAFT STRUCTURAL TESTING |
Technical Paper | Damage-Tolerance Practices Applied to Transport Aircraft Structures |
Authors
Citation
Dougherty, J., "Recognition of Damage - Tolerance in Civil Airworthiness Standards," SAE Technical Paper 781019, 1978, https://doi.org/10.4271/781019.Also In
References
- Federal Aviation Regulations, Part 25 “Airworthiness Standards Transport Category Airplanes.”
- Federal Aviation Agency Civil Aeronautics Manual 4b, Appendix H “Fatigue Evaluation of Flight Structure September 1962
- Federal Aviation Administration Transport Category Airplane Fatigue Regulatory Review Program Fatigue Proposals DOT/FAA
- Dougherty James E. FAA Fatigue Strength Criteria and Practices Proceedings of the 4th Symposium of the International Committee on Aeronautical Fatigue Munich 16-18 June 1965