Source: https://www.law.cornell.edu/cfr/text/14/29.25
Timestamp: 2016-07-24 03:44:53
Document Index: 699274554

Matched Legal Cases: ['art 29', '§ 29', '§ 29', '§ 29', '§ 29', '§ 106', '§ 40113', '§ 44701', '§ 44702', '§ 44704']

14 CFR 29.25 - Weight limits. | US Law | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 29 › Subpart B › Section 29.25 14 CFR 29.25 - Weight limits.
§ 29.25 Weight limits.
Maximum weight. The maximum weight (the highest weight at which compliance with each applicable requirement of this part is shown) or, at the option of the applicant, the highest weight for each altitude and for each practicably separable operating condition, such as takeoff, enroute operation, and landing, must be established so that it is not more than - (1) The highest weight selected by the applicant; (2) The design maximum weight (the highest weight at which compliance with each applicable structural loading condition of this part is shown); or (3) The highest weight at which compliance with each applicable flight requirement of this part is shown.
(4) For Category B rotorcraft with 9 or less passenger seats, the maximum weight, altitude, and temperature at which the rotorcraft can safely operate near the ground with the maximum wind velocity determined under § 29.143(c) and may include other demonstrated wind velocities and azimuths. The operating envelopes must be stated in the Limitations section of the Rotorcraft Flight Manual.
Minimum weight. The minimum weight (the lowest weight at which compliance with each applicable requirement of this part is shown) must be established so that it is not less than - (1) The lowest weight selected by the applicant; (2) The design minimum weight (the lowest weight at which compliance with each structural loading condition of this part is shown); or (3) The lowest weight at which compliance with each applicable flight requirement of this part is shown. (c)
(2) Structural component approval for external load operations under either § 29.865 or under equivalent operational standards is obtained,
(5) Operation of the rotorcraft at a total weight greater than the maximum certificated weight established under paragraph (a) of this section is limited by appropriate operating limitations under § 29.865 (a) and (d) of this part.
[Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as amended by Amdt. 29-12, 41 FR 55471, Dec. 20, 1976; Amdt. 29-43, 64 FR 43020, Aug. 6, 1999; Amdt. 29-51, 73 FR 11001, Feb. 29, 2008] 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