cfr_sections: 14:14:1.0.1.3.16.3.249.12
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| section_id | title_number | title_name | chapter | subchapter | part_number | part_name | subpart | subpart_name | section_number | section_heading | agency | authority | source_citation | amendment_citations | full_text |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 14:14:1.0.1.3.16.3.249.12 | 14 | Aeronautics and Space | I | C | 29 | PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT | C | Subpart C—Strength Requirements | 29.391 | § 29.391 General. | FAA | 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704. | Docket No. 5084, 29 FR 16150, Dec. 3, 1964, unless otherwise noted. | [Amdt. 29-26, 55 FR 8002, Mar. 6, 1990, as amended by Amdt. 29-41, 62 FR 46173, Aug. 29, 1997] | Each auxiliary rotor, each fixed or movable stabilizing or control surface, and each system operating any flight control must meet the requirements of §§ 29.395 through 29.399, 29.411, and 29.427. |