cfr_sections: 14:14:1.0.1.3.16.2.244.32
Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API
This data as json
| 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 14:14:1.0.1.3.16.2.244.32 | 14 | Aeronautics and Space | I | C | 29 | PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT | B | Subpart B—Flight | 29.171 | § 29.171 Stability: 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. | The rotorcraft must be able to be flown, without undue pilot fatigue or strain, in any normal maneuver for a period of time as long as that expected in normal operation. At least three landings and takeoffs must be made during this demonstration. |