Source: https://www.law.cornell.edu/cfr/text/14/23.63
Timestamp: 2017-01-23 04:54:21
Document Index: 354123373

Matched Legal Cases: ['art 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23']

14 CFR 23.63 - Climb: General. | US Law | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 23 › Subpart B › Section 23.63 14 CFR 23.63 - Climb: General.
(a) Compliance with the requirements of §§ 23.65, 23.66, 23.67, 23.69, and 23.77 must be shown - (1) Out of ground effect; and (2) At speeds that are not less than those at which compliance with the powerplant cooling requirements of §§ 23.1041 to 23.1047 has been demonstrated; and (3) Unless otherwise specified, with one engine inoperative, at a bank angle not exceeding 5 degrees. (b) For normal, utility, and acrobatic category reciprocating engine-powered airplanes of 6,000 pounds or less maximum weight, compliance must be shown with § 23.65(a), § 23.67(a), where appropriate, and § 23.77(a) at maximum takeoff or landing weight, as appropriate, in a standard atmosphere.
(c) For reciprocating engine-powered airplanes of more than 6,000 pounds maximum weight, single-engine turbines, and multiengine turbine airplanes of 6,000 pounds or less maximum weight in the normal, utility, and acrobatic category, compliance must be shown at weights as a function of airport altitude and ambient temperature, within the operational limits established for takeoff and landing, respectively, with - (1)Sections 23.65(b) and 23.67(b) (1) and (2), where appropriate, for takeoff, and (2)Section 23.67(b)(2), where appropriate, and § 23.77(b), for landing.
(d) For multiengine turbine airplanes over 6,000 pounds maximum weight in the normal, utility, and acrobatic category and commuter category airplanes, compliance must be shown at weights as a function of airport altitude and ambient temperature within the operational limits established for takeoff and landing, respectively, with - (1)Sections 23.67(c)(1), 23.67(c)(2), and 23.67(c)(3) for takeoff; and (2)Sections 23.67(c)(3), 23.67(c)(4), and 23.77(c) for landing. [Doc. No. 27807, 61 FR 5186, Feb. 9, 1996, as amended by Amdt. 23-62, 76 FR 75753, Dec. 2, 2011]
14 CFR 23.75 — Landing Distance.