CS 26.301 Compliance plan for (R)TC holders and applicants

• ED Decision 2020/023/R found in: CS-26 Additional Airworthiness Specifications for Operations (No 2015/640) Part-26 (Mar 2023)

CS 26.301 Compliance plan for (R)TC holders and applicants ED Decision 2020/023/R/R Compliance with point [26.301](#_DxCrossRefBm881534111) of Part-26 is demonstrated when a compliance plan exists that includes the following: (a) a project schedule identifying all the major milestones for meeting the compliance dates as specified in points [26.302](#_DxCrossRefBm881534095) to [26.309](#_DxCrossRefBm881534081) of Part-26, as applicable; (b) a proposed means of compliance with the applicable requirements as specified in points [26.302](#_DxCrossRefBm881534095) to [26.309](#_DxCrossRefBm881534081) of Part-26, including as appropriate, methods and procedures for: (1) performing the damage tolerance evaluation (DTE) of baseline structure, modified structure and published repairs; (2) identifying the aeroplane structural configuration to be evaluated; (3) identifying widespread fatigue damage (WFD)-susceptible structure; (4) identifying the source of engineering data that will be used to perform the required evaluations; (5) performing the WFD evaluation of structure; (6) establishing a limit of validity (LOV) and plans for distribution upon approval (including incorporation of the LOV into the (airworthiness limitation section) ALS); (7) identifying and developing the maintenance actions required to support the LOV; (8) developing a baseline corrosion prevention and control programme (CPCP); (9) establishing a process to ensure the continuing structural integrity programme remains valid; (10) establishing the list of fatigue-critical baseline structures (FCBSs); (11) developing the repair evaluation guidelines (REGs); (c) a plan for submitting a draft of all the required compliance items for review by EASA not less than 60 days before the applicable compliance date. [Issue: 26/3] #### CS 26.301 Compliance plan for (R)TC holders and applicants *ED Decision 2020/023/R/R* Compliance with point [26.301](#_DxCrossRefBm783605511) of Part-26 is demonstrated when a compliance plan exists that includes the following: (a) a project schedule identifying all the major milestones for meeting the compliance dates as specified in points [26.302](#_DxCrossRefBm783605495) to [26.309](#_DxCrossRefBm783605481) of Part-26, as applicable; (b) a proposed means of compliance with the applicable requirements as specified in points [26.302](#_DxCrossRefBm783605495) to [26.309](#_DxCrossRefBm783605481) of Part-26, including as appropriate, methods and procedures for: (1) performing the damage tolerance evaluation (DTE) of baseline structure, modified structure and published repairs; (2) identifying the aeroplane structural configuration to be evaluated; (3) identifying widespread fatigue damage (WFD)-susceptible structure; (4) identifying the source of engineering data that will be used to perform the required evaluations; (5) performing the WFD evaluation of structure; (6) establishing a limit of validity (LOV) and plans for distribution upon approval (including incorporation of the LOV into the (airworthiness limitation section) ALS); (7) identifying and developing the maintenance actions required to support the LOV; (8) developing a baseline corrosion prevention and control programme (CPCP); (9) establishing a process to ensure the continuing structural integrity programme remains valid; (10) establishing the list of fatigue-critical baseline structures (FCBSs); (11) developing the repair evaluation guidelines (REGs); (c) a plan for submitting a draft of all the required compliance items for review by EASA not less than 60 days before the applicable compliance date. [Issue: 26/3]