Regulatory Text
14 C.F.R. § 27.71 — Autorotation performance.
§ 27.71 Autorotation performance. For single-engine helicopters and multiengine helicopters that do not meet the Category A engine isolation requirements of Part 29 of this chapter, the minimum rate of descent airspeed and the best angle-of-glide airspeed must be determined in autorotation at— (a) Maximum weight; and (b) Rotor speed(s) selected by the applicant. [Amdt. 27-21, 49 FR 44433, Nov. 6, 1984]
Source: ecfr.gov · govinfo.gov — public domain
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Root-LD v1.0 · boisestandard.org
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BS-CFR14-SEC-03BBBA
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Citation
14 C.F.R. § 27.71
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CFR — Code of Federal Regulations
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The regulatory text of 14 C.F.R. § 27.71 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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Title 14 — Aeronautics and Space
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14 C.F.R. — public domain
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