14 CFR 23.2215
§ 23.2215 Flight load conditions.
United States · 14 CFR — Aeronautics and Space · Status: effective
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- Citation
- 14 CFR 23.2215, § 23.2215 Flight load conditions, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/53907
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Full text
The applicant must determine the structural design loads resulting from the following flight conditions:
(a) Atmospheric gusts where the magnitude and gradient of these gusts are based on measured gust statistics.
(b) Symmetric and asymmetric maneuvers.
(c) Asymmetric thrust resulting from the failure of a powerplant unit.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.