[FAR Part § 23.641: [Wings] - Proof of strength -- FAA FARS, 14 CFR] -- Flightsim Aviation Zone - Number 1 Flight Simulation and Aviation Resource! Information, Tools, Downloads, Databases, FAQ, Aviation Humour, Glossaries, Directory, FS2006, Multimedia, Screenshots, Free Flight Planner, Weather Reports | Aviation Databases - aircraft, airports, airlines, countries, timezones | Flight Simulator X
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FAA Federal Aviation Regulations (FARS, 14 CFR)

FARs   >   Part 23   >   Section 641 - Proof of strength

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The strength of stressed-skin wings must be proven by load tests or by combined structural analysis and load tests.

 

 

 

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