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Fatigue Certification of General Aviation Aircraft in Australia Department of Civil Aviation, Australia

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
O'Brien, K., author.
Conference Name:
National Business Aircraft Meeting and Engineering Display (1972-03-15 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1972
Summary:
This paper deals broadly with three aspects of the fatigue substantiation of general aviation aircraft structures. It describes the development of the Australian fatigue substantiation requirements for general aviation aircraft; it presents the results of local work in the acquisition of loads spectra for a range of aircraft, including pressurized and nonpressurized light twins, and it discusses some specific problems affecting the safe life and fail-safe substantiation of general aviation aircraft structures. Recent Australian work on ground taxi load spectra and on the endurance and radiographic inspectability of laminated spar caps is described
Notes:
Vendor supplied data
Publisher Number:
720311
Access Restriction:
Restricted for use by site license

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