14 CFR 27.341

§ 27.341 Gust loads.

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

Cite this

Citation: 14 CFR 27.341, § 27.341 Gust loads, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54452
Permanent ID: ys:prov:54452@1
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Full text

The rotorcraft must be designed to withstand, at each critical airspeed including hovering, the loads resulting from a vertical gust of 30 feet per second.

Legislative history

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