cfr_sections: 14:14:1.0.1.3.16.3.249.15

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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
14:14:1.0.1.3.16.3.249.15	14	Aeronautics and Space	I	C	29	PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT	C	Subpart C—Strength Requirements	29.399	§ 29.399 Dual control system.	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.		Each dual primary flight control system must be able to withstand the loads that result when pilot forces not less than 0.75 times those obtained under § 29.395 are applied— (a) In opposition; and (b) In the same direction.