14 C.F.R. · Aeronautics and Space
14 C.F.R. § 25.977

Fuel tank outlet.

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

14 C.F.R. § 25.977 — Fuel tank outlet.

§ 25.977 Fuel tank outlet. (a) There must be a fuel strainer for the fuel tank outlet or for the booster pump. This strainer must— (1) For reciprocating engine powered airplanes, have 8 to 16 meshes per inch; and (2) For turbine engine powered airplanes, prevent the passage of any object that could restrict fuel flow or damage any fuel system component. (b) [Reserved] (c) The clear area of each fuel tank outlet strainer must be at least five times the area of the outlet line. (d) The diameter of each strainer must be at least that of the fuel tank outlet. (e) Each finger strainer must be accessible for inspection and cleaning. [Amdt. 25-11, 32 FR 6913, May 5, 1967, as amended by Amdt. 25-36, 39 FR 35460, Oct. 1, 1974]

Source: ecfr.gov · govinfo.gov — public domain Official Source ↗
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14 C.F.R. § 25.977
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The regulatory text of 14 C.F.R. § 25.977 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. § 25.977