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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.
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