cfr_sections: 14:14:1.0.1.3.16.2.243.17

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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
14:14:1.0.1.3.16.2.243.17	14	Aeronautics and Space	I	C	29	PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT	B	Subpart B—Flight	29.64	§ 29.64 Climb: General.	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.	[Doc. No. 24802, 61 FR 21900, May 10, 1996]	Compliance with the requirements of §§ 29.65 and 29.67 must be shown at each weight, altitude, and temperature within the operational limits established for the rotorcraft and with the most unfavorable center of gravity for each configuration. Cowl flaps, or other means of controlling the engine-cooling air supply, will be in the position that provides adequate cooling at the temperatures and altitudes for which certification is requested.