Code of Federal Regulations (Last Updated: April 5, 2024) |
Title 14 - Aeronautics and Space |
Chapter I - Federal Aviation Administration, Department of Transportation |
SubChapter C - Aircraft |
Part 23 - Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes |
Subpart D - Design and Construction |
Wings |
§ 23.641 - Proof of strength.
Latest version.
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§ 23.641 Proof of strength.
The strength of stressed-skin wings must be proven by load tests or by combined structural analysis and load tests.