cfr_sections: 14:14:1.0.1.3.15.2.163.17
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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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 14:14:1.0.1.3.15.2.163.17 | 14 | Aeronautics and Space | I | C | 27 | PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT | B | Subpart B—Flight | 27.151 | § 27.151 Flight controls. | FAA | 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704. | Docket No. 5074, 29 FR 15695, Nov. 24, 1964, unless otherwise noted. | [Amdt. 27-21, 49 FR 44433, Nov. 6, 1984] | (a) Longitudinal, lateral, directional, and collective controls may not exhibit excessive breakout force, friction, or preload. (b) Control system forces and free play may not inhibit a smooth, direct rotorcraft response to control system input. |