# Commission Regulation (EU) 2015/640 of 23 April 2015 on additional airworthiness specifications for a given type of operations and amending Regulation (EU) No 965/2012, Division 26.305: Validity of the continuing structural integrity programme


(a)A holder of a type-certificate (TC) or a restricted TC for a turbine-powered large aeroplane certified on or after 1 January 1958, for which the application for TC was submitted before 1 January 2019, shall establish and implement a process that ensures that the continuing structural integrity programme remains valid throughout the operational life of the aeroplane, taking into account service experience and current operations.
(b)The holder of a type-certificate (TC) or a restricted TC shall submit a description of the process referred to in point(a) to the CAA before 26 February 2024 for approval. The holder of a type-certificate (TC) or a restricted TC shall implement the process within 6 months after its approval by the CAA.
(c)An applicant for a TC or restricted TC as referred to in Article 1 paragraph 2(c) for a turbine-powered large aeroplane, shall establish and implement a process that ensures that the continuing structural integrity programme remains valid throughout the operational life of the aeroplane, taking into account service experience and current operations. It shall submit a description of the process to the CAA before 26 February 2024, or before the issuance of the certificate, whichever occurs later, for approval and shall implement the process within 6 months after its approval by the CAA.

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Source: https://www.legislation.gov.uk/eur/2015/640/annex/I/division/subpart+b/division/26.305 (the official version)
Page: https://openlegislation.uk/eu-regulation-2015-640/annex-I/division-subpart+b/division-26.305
Contains public sector information licensed under the Open Government Licence v3.0. Source: legislation.gov.uk, The National Archives.