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CS 25.1182 Nacelle areas behind firewalls, and engine pod attaching structures containing flammable fluid lines
Available versions for ERULES-1963177438-8546
ED Decision 2003/2/RM
found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)
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CS-25 Amdt 27 - La... (Jan 2023)
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CS 25.1182 Nacelle areas behind firewalls, and engine pod attaching structures containing flammable fluid lines ED Decision 2003/2/RM (a) Each nacelle area immediately behind the firewall, and each portion of any engine pod attaching structure containing flammable fluid lines, must meet each requirement of [CS 25.1103(b)](#_DxCrossRefBm1709821513), [25.1165(e)](#_DxCrossRefBm1709821536), [25.1183](#_DxCrossRefBm1709821170), [25.1185(c)](#_DxCrossRefBm1709821169), [25.1187](#_DxCrossRefBm1709821542), [25.1189](#_DxCrossRefBm1709821402) and [25.1195](#_DxCrossRefBm1709821357) to [25.1203](#_DxCrossRefBm1709821356), including those concerning designated fire zones. However, engine pod attaching structures need not contain fire detection or extinguishing means. (b) For each area covered by sub-paragraph (a) of this paragraph that contains a retractable landing gear, compliance with that sub-paragraph need only be shown with the landing gear retracted.