cfr_sections: 14:14:1.0.1.3.16.2.243.23

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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
14:14:1.0.1.3.16.2.243.23	14	Aeronautics and Space	I	C	29	PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT	B	Subpart B—Flight	29.79	§ 29.79 Landing: Category A.	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]	(a) For Category A rotorcraft— (1) The landing performance must be determined and scheduled so that if the critical engine fails at any point in the approach path, the rotorcraft can either land and stop safely or climb out and attain a rotorcraft configuration and speed allowing compliance with the climb requirement of § 29.67(a)(2); (2) The approach and landing paths must be established with the critical engine inoperative so that the transition between each stage can be made smoothly and safely; (3) The approach and landing speeds must be selected by the applicant and must be appropriate to the type of rotorcraft; and (4) The approach and landing path must be established to avoid the critical areas of the height-velocity envelope determined in accordance with § 29.87. (b) It must be possible to make a safe landing on a prepared landing surface after complete power failure occurring during normal cruise.