EN
L 205/118
Official Journal of the European Union
5.8.2022
(ii) the CRS and detailed maintenance records for the last accomplishment of any scheduled maintenance and any subsequent unscheduled maintenance of all life-limited parts and time-controlled components until the scheduled maintenance has been superseded by another scheduled maintenance of equivalent scope and detail but covering a period not shorter than 36 months; (iii) the CRS and owner’s acceptance statement for any component that is fitted to an ELA2 aircraft without an EASA Form 1 in accordance with point 21.A.307(b)(2) of Annex I (Part 21) to Regulation (EU) No 748/2012 but covering a period not shorter than 36 months; (iv) the CRS and owner’s acceptance statement for any component that is fitted to an aircraft without an EASA Form 1 in accordance with point 21L.A.193(b)(2) of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012 but covering a period not shorter than 36 months.’; (4)
point (b) in point M.A.401 is replaced by the following: ‘(b) For the purposes of this Annex, applicable maintenance data is any of the following: (1) any applicable requirement, procedure, standard or information issued by the competent authority or the Agency; (2) any applicable airworthiness directive; (3) the applicable instructions for continuing airworthiness and other maintenance instructions, issued by the type-certificate holder, supplemental type-certificate holder, a declarant of a declaration of design compliance and any other organisation that publishes such data in accordance with Annex I (Part 21) or, as applicable, Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012; (4) for components approved for installation by the design approval holder or declarant of a declaration of design compliance, the applicable maintenance instructions published by the component manufacturers and acceptable to the design approval holder or declarant of a declaration of design compliance; (5) any applicable data issued in accordance with point 145.A.45(d).’;
(5)
point (a)(1) in point M.A.501 is replaced by the following: ‘(1) Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of Annex I (Part 21) or, as applicable, Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012, unless otherwise specified in point 21.A.307 of Annex I (Part 21) or point 21L.A.193 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012 or in this Annex (Part-M) or in Annex Vd (Part-CAO).’;
(6)
point M.A.502 is amended as follows: (i)
point (a) is replaced by the following: ‘(a) The maintenance of components other than the components referred to in points (b)(2) to (b)(6) of point 21.
A.307 of Annex I (Part 21) or, as applicable, points (b)(2) to (b)(6) of point 21L.A.193 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012 shall be performed by maintenance organisations approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO), as applicable.’;
(ii) point (d) is replaced by the following: ‘(d) The maintenance of components referred to in point (b)(2) of point 21.A.307 of Annex I (Part 21) or in point (b)(2) of point 21L.A.193 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012, where the component is fitted to the aircraft or is temporarily removed to improve access, shall be performed by an aircraft maintenance organisation approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO), as applicable, by the certifying staff referred to in point (b)(1) of point M.A.801 or by the pilot-owner referred to in point (b)(2) of point M.A.801.
Component maintenance performed in accordance with this point shall not be eligible for the issuance of an EASA Form 1 and shall be subject to the aircraft release requirements provided for in point M.A.801.’;