Source: https://www.law.cornell.edu/cfr/text/14/23.337
Timestamp: 2017-01-20 00:01:58
Document Index: 332093278

Matched Legal Cases: ['art 23', '§ 106', '§ 40113', '§ 44701', '§ 44702', '§ 44704']

14 CFR 23.337 - Limit maneuvering load factors. | US Law | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 23 › Subpart C › Section 23.337 14 CFR 23.337 - Limit maneuvering load factors.
(a) The positive limit maneuvering load factorn may not be less than - (1) 2.1 (24,000 ÷ (W 10,000)) for normal and commuter category airplanes, where W = design maximum takeoff weight, except that n need not be more than 3.8;
(2) 4.4 for utility category airplanes; or (3) 6.0 for acrobatic category airplanes. (b) The negative limit maneuvering load factor may not be less than - (1) 0.4 times the positive load factor for the normal utility and commuter categories; or (2) 0.5 times the positive load factor for the acrobatic category. (c) Maneuvering load factors lower than those specified in this section may be used if the airplane has design features that make it impossible to exceed these values in flight. [Doc. No. 4080, 29 FR 17955, Dec. 18, 1964, as amended by Amdt. 23-7, 34 FR 13088, Aug. 13, 1969; Amdt. 23-34, 52 FR 1829, Jan. 15, 1987; Amdt. 23-48, 61 FR 5144, Feb. 9, 1996] This is a list of United States Code sections, Statutes at Large, Public Laws, and Presidential Documents, which provide rulemaking authority for this CFR Part.This list is taken from the Parallel Table of Authorities and Rules provided by GPO [Government Printing Office].It is not guaranteed to be accurate or up-to-date, though we do refresh the database weekly. More limitations on accuracy are described at the GPO site.United States CodeU.S. Code: Title 49 - TRANSPORTATION§ 106 - Federal Aviation Administration§ 40113 - Administrative§ 44701 - General requirements§ 44702 - Issuance of certificates§ 44704 - Type certificates, production certificates, airworthiness certificates,,11 So in original. and design and production organization certificates
14 CFR 91.323 — Increased Maximum Certificated Weights for Certain Airplanes Operated in Alaska.
14 CFR 23.333 — Flight Envelope.
14 CFR 23.373 — Speed Control Devices.
14 CFR 23.343 — Design Fuel Loads.