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Division 26.304 Corrosion prevention and control programmeF1F2

Original text. Later amendments are not shown.

  1. (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 a baseline corrosion prevention and control programme (CPCP).

  2. (b)

    Unless the baseline CPCP referred to in point (a) has already been approved by the CAA in accordance with point 21.A.3B(c)(1) of Annex 1 to Regulation (EU) No 748/2012 or in a maintenance review board report (MRBR) approved by the CAA, the holder of a type-certificate (TC) or a restricted TC shall submit the CPCP to the CAA before 26 February 2024, for approval.

  3. (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 a baseline corrosion prevention and control programme (CPCP) prior to the TC being issued.

Annotations

Textual amendments

F1

Substituted by Commission Implementing Regulation (EU) 2019/133 of 28 January 2019 amending Regulation (EU) 2015/640 as regards the introduction of new additional airworthiness specifications.

F2

Annex 1 points 26.300-26.370 inserted (20.11.2021) by The Aviation Safety (Amendment) (No. 3) Regulations 2021 (S.I. 2021/1203), regs. 1(2), 21(7)