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14 CFR 35.24

§ 35.24 Strength.

United States · 14 CFR — Aeronautics and Space · Status: effective

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14 CFR 35.24, § 35.24 Strength, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/55169
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The maximum stresses developed in the propeller may not exceed values acceptable to the Administrator considering the particular form of construction and the most severe operating conditions.

Legislative history

This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.