14 CFR 25.371
§ 25.371 Gyroscopic loads.
United States · 14 CFR — Aeronautics and Space · Status: effective
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- Citation
- 14 CFR 25.371, § 25.371 Gyroscopic loads, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/54030
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Full text
The structure supporting any engine or auxiliary power unit must be designed for the loads, including gyroscopic loads, arising from the conditions specified in §§ 25.331, 25.341, 25.349, 25.351, 25.473, 25.479, and 25.481, with the engine or auxiliary power unit at the maximum rotating speed appropriate to the condition. For the purposes of compliance with this paragraph, the pitch maneuver in § 25.331(c)(1) must be carried out until the positive limit maneuvering load factor (point A2 in § 25.333(b)) is reached.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.