cfr_sections: 14:14:1.0.1.3.15.4.176.28

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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
14:14:1.0.1.3.15.4.176.28	14	Aeronautics and Space	I	C	27	PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT	D	Subpart D—Design and Construction	27.687	§ 27.687 Spring devices.	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.		(a) Each control system spring device whose failure could cause flutter or other unsafe characteristics must be reliable. (b) Compliance with paragraph (a) of this section must be shown by tests simulating service conditions.