EN
5.8.2022
Official Journal of the European Union
L 205/117
ANNEX I
Annex I (Part-M) to Commission Regulation (EU) No 1321/2014 is amended as follows: (1)
point M.A.302 is amended as follows: (i) point (d) is replaced by the following: ‘(d) The AMP shall demonstrate compliance with: (1) the instructions issued by the competent authority; (2) the instructions for continuing airworthiness: (i)
issued by the holders of the type certificate, restricted type certificate, supplemental type certificate, major repair design approval, ETSO authorisation or the declarant of a declaration of design compliance or the holder of any other relevant approval issued under Annex I (Part 21) or, as applicable, Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012;
(ii) included in the certification specifications referred to in point 21.A.90B or 21.A.431B of Annex I (Part 21) to Regulation (EU) No 748/2012, if applicable; (iii) included in the certification specifications referred to in point 21L.A.62, 21L.A.102, 21L.A.202 or 21L.A.222 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012, if applicable;’; (ii) point (h) is replaced by the following: ‘(h) The AMP shall be subject to periodic reviews and be amended accordingly when necessary.
Those reviews shall ensure that the AMP continues to be up to date and valid in light of the operating experience and instructions from the competent authority, while taking into account new or modified maintenance instructions issued by the type-certificate and supplemental type-certificate holders, 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.’; (2)
point M.A.304 is replaced by the following: ‘M.A.304 Data for modifications and repairs A person or organisation repairing an aircraft or a component, shall assess any damage.
Modifications and repairs shall be carried out using, as appropriate, the following data: (a) approved by the Agency; (b) approved by a design organisation complying with Annex I (Part 21) to Regulation (EU) No 748/2012; (c) contained in the requirements referred to in point 21.A.90B or 21.A.431B of Annex I (Part 21) to Regulation (EU) No 748/2012; (d) contained in the requirements referred to in point 21L.A.62, 21L.A.102, 21L.A.202 or 21L.A.222 of Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012; (e) declared by a declarant of a declaration of design compliance complying with Annex Ib (Part 21 Light) to Regulation (EU) No 748/2012.’;
(3)
point (e)3 in point M.A.305 is replaced by the following: ‘3. data specific to certain components: (i)
an in-service history record for each life-limited part based on which the current status of compliance with airworthiness limitations is determined;