14 C.F.R. · Aeronautics and Space
14 C.F.R. § 25.395

Control system.

Title 14 C.F.R. ● ACTIVE Primary Source
Regulatory Text

14 C.F.R. § 25.395 — Control system.

§ 25.395 Control system. (a) Longitudinal, lateral, directional, and drag control system and their supporting structures must be designed for loads corresponding to 125 percent of the computed hinge moments of the movable control surface in the conditions prescribed in § 25.391. (b) The system limit loads of paragraph (a) of this section need not exceed the loads that can be produced by the pilot (or pilots) and by automatic or power devices operating the controls. (c) The loads must not be less than those resulting from application of the minimum forces prescribed in § 25.397(c). [Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-23, 35 FR 5672, Apr. 8, 1970; Amdt. 25-72, 55 FR 29776, July 20, 1990; Amdt. 25-141, 79 FR 73468, Dec. 11, 2014]

Source: ecfr.gov · govinfo.gov — public domain Official Source ↗
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14 C.F.R. § 25.395
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The regulatory text of 14 C.F.R. § 25.395 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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boisestandard.org United States Law CFR Title 14 14 C.F.R. § 25.395