Regulatory Text
14 C.F.R. § 25.371 — Gyroscopic loads.
§ 25.371 Gyroscopic loads. 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 A 2 in § 25.333(b)) is reached. [Amdt. 25-141, 79 FR 73468, Dec. 11, 2014]
Source: ecfr.gov · govinfo.gov — public domain
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14 C.F.R. § 25.371
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The regulatory text of 14 C.F.R. § 25.371 is reproduced from the official Code of Federal Regulations as published by the Office of the Federal Register and the National Archives and Records Administration.
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