Inspectability Criteria for Airframes Designed to Fatigue/Fail-Safe Requirements

Format:

Conference/Event

Author/Creator:

Weaver, Robert T., 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 covers inspection programs which will become a part of small airplane certification and operation as a result of Amendment 7 to FAR 23. Amendment 7 adds fatigue evaluation to wings and associated structure, reference paragraph 23.572.Paragraph 23.572 allows two basic methods of providing the required fatigue evaluation fatigue strength investigation or fail-safe strength investigation.The fail-safe strength investigation allows compliance with the regulations without running long and expensive fatigue analyses and/or tests but must be supplemented with proper inspections for complete FAR 23 compliance. Designing for inspectability and inspection methods will be covered

Notes:

Vendor supplied data

Publisher Number:

720310

Access Restriction:

Restricted for use by site license