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Code · CFR · Title 14 — Aeronautics and Space · Part 23 — Airworthiness Standards: Normal Category Airplanes · § 23.2230

§ 23.2230. Limit and ultimate loads.

49 words·~1 min read·/us/cfr/t14/s§ 23.2230·

A research copy — for the controlling text, always check the official state or federal source. Not legal advice.

The applicant must determine—
(a)The limit loads, which are equal to the structural design loads unless otherwise specified elsewhere in this part; and
(b)The ultimate loads, which are equal to the limit loads multiplied by a 1.5 factor of safety unless otherwise specified elsewhere in this part.
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