14 C.F.R. § 25.869 Fire protection: systems.
Title 14 - Aeronautics and Space
(a) Electrical system components: (1) Components of the electrical system must meet the applicable fire and smoke protection requirements of §§25.831(c) and 25.863. (2) Electrical cables, terminals, and equipment in designated fire zones, that are used during emergency procedures, must be at least fire resistant. (3) Main power cables (including generator cables) in the fuselage must be designed to allow a reasonable degree of deformation and stretching without failure and must be— (i) Isolated from flammable fluid lines; or (ii) Shrouded by means of electrically insulated, flexible conduit, or equivalent, which is in addition to the normal cable insulation. (4) Insulation on electrical wire and electrical cable installed in any area of the airplane must be self-extinguishing when tested in accordance with the applicable portions of part I, appendix F of this part. (b) Each vacuum air system line and fitting on the discharge side of the pump that might contain flammable vapors or fluids must meet the requirements of §25.1183 if the line or fitting is in a designated fire zone. Other vacuum air systems components in designated fire zones must be at least fire resistant. (c) Oxygen equipment and lines must— (1) Not be located in any designated fire zone, (2) Be protected from heat that may be generated in, or escape from, any designated fire zone, and (3) Be installed so that escaping oxygen cannot cause ignition of grease, fluid, or vapor accumulations that are present in normal operation or as a result of failure or malfunction of any system. [Amdt. 25–72, 55 FR 29784, July 20, 1990, as amended by Amdt. 25–113, 69 FR 12530, Mar. 16, 2004]
Title 14: Aeronautics and Space
PART 25—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES
Subpart D—Design and Construction
Fire Protection
§ 25.869 Fire protection: systems.
