cfr_sections: 14:14:1.0.1.3.15.3.166.1

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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
14:14:1.0.1.3.15.3.166.1	14	Aeronautics and Space	I	C	27	PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT	C	Subpart C—Strength Requirements	27.301	§ 27.301 Loads.	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) Strength requirements are specified in terms of limit loads (the maximum loads to be expected in service) and ultimate loads (limit loads multiplied by prescribed factors of safety). Unless otherwise provided, prescribed loads are limit loads. (b) Unless otherwise provided, the specified air, ground, and water loads must be placed in equilibrium with inertia forces, considering each item of mass in the rotorcraft. These loads must be distributed to closely approximate or conservatively represent actual conditions. (c) If deflections under load would significantly change the distribution of external or internal loads, this redistribution must be taken into account.