cfr_sections: 14:14:1.0.1.3.16.2.243.26

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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
14:14:1.0.1.3.16.2.243.26	14	Aeronautics and Space	I	C	29	PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT	B	Subpart B—Flight	29.85	§ 29.85 Balked 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, 64 FR 45338, Aug. 19, 1999]	For Category A rotorcraft, the balked landing path with the critical engine inoperative must be established so that— (a) The transition from each stage of the maneuver to the next stage can be made smoothly and safely; (b) From the LDP on the approach path selected by the applicant, a safe climbout can be made at speeds allowing compliance with the climb requirements of § 29.67(a)(1) and (2); and (c) The rotorcraft does not descend below 15 feet above the landing surface. For elevated heliport operations, descent may be below the level of the landing surface provided the deck edge clearance of § 29.60 is maintained and the descent (loss of height) below the landing surface is determined.