VTOL.2325 Fire Protection

• n/a found in: Small Category VCA (Revision 0) SC-VTOL (Oct 2024)

VTOL.2325 Fire Protection n/a (a) The aircraft must be 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). (4) a survivable emergency landing. (b) The aircraft must be 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 [VTOL.2330](#_DxCrossRefBm1877490365).