M25.4 Airworthiness limitations and procedures

• ED Decision 2009/010/R found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

M25.4 Airworthiness limitations and procedures ED Decision 2009/010/R The FRM shall be subject to analysis using conventional processes and methodology to ensure that the minimum scheduled maintenance tasks required for securing the continuing airworthiness of the system and installation are identified and published as part of the [CS 25.1529](#_DxCrossRefBm1709821031) compliance. Maintenance tasks arising from either the Monte Carlo analysis or a [CS 25.1309](#_DxCrossRefBm1709820691) safety assessment shall be dealt with in accordance with the principles laid down in [AMC 25.1309](#_DxCrossRefBm1709821113). (a) If FRM is used to comply with paragraph [M25.1](#_DxCrossRefBm1709821991), Airworthiness Limitations must be identified for all maintenance or inspection tasks required to identify failures of components within the FRM that are needed to meet paragraph [M25.1](#_DxCrossRefBm1709821991). (b) Maintenance procedures must be developed to identify any hazards to be considered during maintenance of the fuel system and of the FRM. These procedures must be included in the instructions for continued airworthiness (ICA). [Amdt 25/6]