AMC 25.1713 Fire protection: EWIS

• ED Decision 2008/006/R found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

AMC 25.1713 Fire protection: EWIS ED Decision 2008/006/R The intent of [CS 25.1713](#_DxCrossRefBm1709821367) is to ensure that the EWIS does not fail in such a way as to propagate fire and produce hazardous quantities of smoke and toxic fumes. 1 Subparagraph 25.1713(a) requires that all EWIS components meet the applicable fire and smoke protection requirements of [CS 25.831(c)](#_DxCrossRefBm1709821304). After reasonably probable failures or malfunctions, EWIS components should not cause harmful or hazardous concentrations of gases or vapors in excess of the levels prescribed in [CS 25.831(b)(1) and (2)](#_DxCrossRefBm1709821304). 2 Subparagraph 25.1713(b) requires that EWIS components located in designated fire zones and are used during emergency procedures must be at least fire resistant. This requirement is intended to help ensure that emergency services on the aeroplane are available in the event of a fire. EWIS components in regions immediately behind firewalls and in engine pod attachment structures should be made of such materials and installed at such a distance from the firewall that they will not suffer damage that could hazard the aeroplane if the surface of the firewall adjacent to the fire is heated to 1100° C for 15 minutes. 3 Subparagraph 25.1713(c) requires that insulation on electrical wire and electrical cable installed anywhere in the aeroplane be self-extinguishing when tested in accordance with the applicable portions of [part I](#_DxCrossRefBm1709821333) of Appendix F of CS 25. In addition, to protect against propagation of a fire, EWIS components other than wire and cable should be designed using non‑flammable and self‑extinguishing materials as tested to meet the intent of Part I of Appendix F. [Amdt 25/5]