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CS 23.2325 Fire protection
Available versions for ERULES-1963177438-6798
ED Decision 2017/013/R
found in: CS-23 Amdt 6 AMC-GM Issue 4 - Normal-Category Aeroplanes (Mar 2023)
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CS 23.2325 Fire protection ED Decision 2017/013/R (a) The aeroplane is designed to minimise the risk of fire initiation due to: (1) anticipated heat or energy dissipation or system failures or overheat that are expected to generate heat sufficient to ignite a fire; (2) ignition of flammable fluids, gases or vapours; and (3) fire-propagating or -initiating system characteristics (e.g. oxygen systems). (b) The aeroplane is designed to minimise the risk of fire propagation by: (1) providing adequate fire or smoke awareness and extinguishing means when practical; (2) application of self-extinguishing, flame-resistant, or fireproof materials that are adequate to the application, location and certification level; or (3) specifying and designing designated fire zones that meet the specifications of [CS 23.2330](#_DxCrossRefBm1265640852).
CS 23.2325 Fire protection ED Decision 2017/013/R (a) The aeroplane is designed to minimise the risk of fire initiation due to: (1) anticipated heat or energy dissipation or system failures or overheat that are expected to generate heat sufficient to ignite a fire; (2) ignition of flammable fluids, gases or vapours; and (3) fire-propagating or -initiating system characteristics (e.g. oxygen systems). (b) The aeroplane is designed to minimise the risk of fire propagation by: (1) providing adequate fire or smoke awareness and extinguishing means when practical; (2) application of self-extinguishing, flame-resistant, or fireproof materials that are adequate to the application, location and certification level; or (3) specifying and designing designated fire zones that meet the specifications of [CS 23.2330](#_DxCrossRefBm916685721).
#### CS 23.2325 Fire protection *ED Decision 2017/013/R* (a) The aeroplane is designed to minimise the risk of fire initiation due to: (1) anticipated heat or energy dissipation or system failures or overheat that are expected to generate heat sufficient to ignite a fire; (2) ignition of flammable fluids, gases or vapours; and (3) fire-propagating or -initiating system characteristics (e.g. oxygen systems). (b) The aeroplane is designed to minimise the risk of fire propagation by: (1) providing adequate fire or smoke awareness and extinguishing means when practical; (2) application of self-extinguishing, flame-resistant, or fireproof materials that are adequate to the application, location and certification level; or (3) specifying and designing designated fire zones that meet the specifications of [CS 23.2330](#_DxCrossRefBm470704029).