Regulatory Text
14 C.F.R. § 25.391 — Control surface loads: General.
§ 25.391 Control surface loads: General. The control surfaces must be designed for the limit loads resulting from the flight conditions in §§ 25.331, 25.341(a) and (b), 25.349, and 25.351, considering the requirements for— (a) Loads parallel to hinge line, in § 25.393; (b) Pilot effort effects, in § 25.397; (c) Trim tab effects, in § 25.407; (d) Unsymmetrical loads, in § 25.427; and (e) Auxiliary aerodynamic surfaces, in § 25.445. [Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-86, 61 FR 5222, Feb. 9, 1996; Amdt. 25-141, 79 FR 73468, Dec. 11, 2014]
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14 C.F.R. § 25.391
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The regulatory text of 14 C.F.R. § 25.391 is reproduced from the official Code of Federal Regulations as published by the Office of the Federal Register and the National Archives and Records Administration.
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Title 14 — Aeronautics and Space
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