14 C.F.R. · Aeronautics and Space
14 C.F.R. § 29.1509

Rotor speed.

Title 14 C.F.R. ● ACTIVE Primary Source
Regulatory Text

14 C.F.R. § 29.1509 — Rotor speed.

§ 29.1509 Rotor speed. (a) Maximum power-off (autorotation). The maximum power-off rotor speed must be established so that it does not exceed 95 percent of the lesser of— (1) The maximum design r.p.m. determined under § 29.309(b); and (2) The maximum r.p.m. shown during the type tests. (b) Minimum power-off. The minimum power-off rotor speed must be established so that it is not less than 105 percent of the greater of— (1) The minimum shown during the type tests; and (2) The minimum determined by design substantiation. (c) Minimum power-on. The minimum power-on rotor speed must be established so that it is— (1) Not less than the greater of— (i) The minimum shown during the type tests; and (ii) The minimum determined by design substantiation; and (2) Not more than a value determined under § 29.33 (a)(1) and (c)(1).

Source: ecfr.gov · govinfo.gov — public domain Official Source ↗
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14 C.F.R. § 29.1509
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The regulatory text of 14 C.F.R. § 29.1509 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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