Regulatory Text
14 C.F.R. § 25.171 — General.
§ 25.171 General. The airplane must be longitudinally, directionally, and laterally stable in accordance with the provisions of §§ 25.173 through 25.177. In addition, suitable stability and control feel (static stability) is required in any condition normally encountered in service, if flight tests show it is necessary for safe operation. [Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-7, 30 FR 13117, Oct. 15, 1965]
Source: ecfr.gov · govinfo.gov — public domain
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Root-LD v1.0 · boisestandard.org
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BS-CFR14-SEC-CD2B19
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REGULATION / FEDERAL-CFR-SECTION
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boisestandard.org
Citation
14 C.F.R. § 25.171
Corpus
CFR — Code of Federal Regulations
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PRIMARY-SOURCE
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The regulatory text of 14 C.F.R. § 25.171 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
14 C.F.R. § 1.114 C.F.R. § 1.214 C.F.R. § 1.314 C.F.R. § 3.114 C.F.R. § 3.514 C.F.R. § 3.20014 C.F.R. § 3.20514 C.F.R. § 5.114 C.F.R. § 5.314 C.F.R. § 5.514 C.F.R. § 5.2114 C.F.R. § 5.2314 C.F.R. § 5.2514 C.F.R. § 5.2714 C.F.R. § 5.5114 C.F.R. § 5.5314 C.F.R. § 5.5514 C.F.R. § 5.7114 C.F.R. § 5.7314 C.F.R. § 5.7514 C.F.R. § 5.9114 C.F.R. § 5.9314 C.F.R. § 5.9514 C.F.R. § 5.9714 C.F.R. § 11.114 C.F.R. § 11.314 C.F.R. § 11.514 C.F.R. § 11.714 C.F.R. § 11.914 C.F.R. § 11.11
14 C.F.R. — public domain
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