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14 CFR 33.65

§ 33.65 Surge and stall characteristics.

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

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14 CFR 33.65, § 33.65 Surge and stall characteristics, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/55082
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When the engine is operated in accordance with operating instructions required by § 33.5(b), starting, a change of power or thrust, power or thrust augmentation, limiting inlet air distortion, or inlet air temperature may not cause surge or stall to the extent that flameout, structural failure, overtemperature, or failure of the engine to recover power or thrust will occur at any point in the operating envelope.

Legislative history

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