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Commission Implementing Regulation (EU) 2019/1383 ANNEX II

Commission Implementing Regulation (EU) 2019/1383 ANNEX II

ANNEX IISupplementary provisions

ANNEX II Annex II to Regulation (EU) No 1321/2014 is amended as follows: (1) point 145.A.30 is amended as follows: (a) point (k) is replaced by the following: ‘(k) If the organisation performs airworthiness reviews and issues the corresponding airworthiness review certificate in accordance with point ML.A.903 of Annex Vb (Part-ML), it shall have airworthiness review staff qualified and authorised in accordance with point ML.A.904 of Annex Vb (Part-ML).’; (b) point (l) is deleted; (2) In point 145.A.42, point (3) of point (a) is replaced by the following: ‘(iii) Components categorised as unsalvageable because they have reached their mandatory life limitation or contain a non-repairable defect.’; (3) In point 145.A.42, point (2) of point (c) is replaced by the following: ‘(ii) Unsalvageable components shall not be permitted to re-enter the component supply system, unless mandatory life limitation have been extended or a repair solution has been approved in accordance with Regulation (EU) No 748/2012.’; (4) in point 145.A.50, point (d) is replaced by the following: ‘(d) A certificate of release to service shall be issued after the required maintenance on a component whilst off the aircraft has been carried out. The authorised release certificate ‘EASA Form 1’ referred to in Appendix II of Annex I (Part-M) constitutes the component certificate of release to service except if otherwise specified in point (b) of point M.A.502. When an organisation maintains a component for its own use, an EASA Form 1 may not be necessary depending upon the organisation's internal release procedures defined in the exposition.’; (5) in point 145.A.55, points (b) and (c) are replaced by the following: ‘(b) The organisation shall provide a copy of each certificate of release to service to the aircraft owner/operator, together with a copy of any detailed maintenance record associated with the work carried out and necessary to demonstrate compliance with point M.A.305. (c) The organisation shall retain a copy of all detailed maintenance records and any associated maintenance data for three years from the date on which the aircraft or component to which the work relates was issued with a certificate of release to service. 1. The records under this point shall be stored in a manner that ensures protection from damage, alteration and theft. 2. All computer hardware used to ensure backup shall be stored in a different location from that containing the working data in an environment that ensures they remain in good condition. 3. When an organisation approved under this Annex terminates its operations, all retained maintenance records from the period of three years preceding the termination of operations of the organisation shall be distributed to the last owner or customer of respective aircraft or component or shall be stored in a way specified by the competent authority.’; (6) in point 145.A.70, point 6 of point (a) is replaced by the following: ‘6. a list of certifying staff, support staff and, if applicable, airworthiness review staff, with their scope of approval.’; (7) point 145.A.75 is amended as follows: (a) point (f) is replaced by the following: ‘(f) If specifically approved to do so for aircraft covered by Annex Vb (Part-ML), it may perform airworthiness reviews and issue the corresponding airworthiness review certificate in accordance with the conditions specified in point ML.A.903 of Annex Vb (Part-ML) to this Regulation.’; (b) point (g) is deleted; (8) in point 145.A.95, points (a) and (b) are replaced by the following: ‘(a) A level 1 finding is any finding of significant non-compliance with the requirements of this Annex which lowers the safety standard and seriously endangers flight safety. (b) A level 2 finding is any finding of non-compliance with the requirements of this Annex which may lower the safety standard and may endanger flight safety.’; (9) point 145.B.60 is replaced by the following: ‘ 145.B.60     Exemptions Where a Member State grants an exemption from the requirements of this Annex in accordance with Article 71 of Regulation (EU) 2018/1139, the competent authority shall record the exemption. It shall retain those records for the period provided for in point (3) of point 145.B.55’; (10) Appendix III is replaced by the following: ‘Appendix III Maintenance Organisation Certificate — EASA Form 3-145 Text of image Page 1 of 2 [MEMBER STATE] (*) A Member of the European Union (**) MAINTENANCE ORGANISATION CERTIFICATE Reference: [MEMBER STATE CODE (*)].145.XXXX Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council and to Commission Regulation (EU) No 1321/2014 and subject to the condition specified below, the [COMPETENT AUTHORITY OF THE MEMBER STATE (*)] hereby certifies: [COMPANY NAME AND ADDRESS] as a maintenance organisation in compliance with Section A of Annex II (Part-145) of Regulation (EU) No 1321/2014, approved to maintain products, parts and appliances listed in the attached terms of approval and issue related certificates of release to service using the above references and, when stipulated, to issue airworthiness review certificates after an airworthiness review as specified in point ML.A.903 of Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014 for those aircraft listed in the attached approval schedule. CONDITIONS: 1. This approval is limited to that specified in the scope of work section of the approved maintenance organisation exposition as referred to in Section A of Annex II (Part-145), and 2. This approval requires compliance with the procedures specified in the approved maintenance organisation exposition, and 3. This approval is valid whilst the approved maintenance organisation remains in compliance with Annex II (Part-145) of Regulation (EU) No 1321/2014. 4. Subject to compliance with the foregoing conditions, this approval shall remain valid for an unlimited duration unless the approval has previously been surrendered, superseded, suspended or revoked. Date of original issue: Date of this revision: Revision No: Signed: For the competent authority: [COMPETENT AUTHORITY OF THE MEMBER STATE(*)] EASA Form 3-145 Issue 4 (*) Or EASA if EASA is the competent authority. (**) Delete for non-EU Member States or EASA. Text of image Page 2 of 2 MAINTENANCE ORGANISATION TERMS OF APPROVAL Reference: [MEMBER STATE CODE (*)].145.[XXXX] Organisation: [COMPANY NAME AND ADDRESS] These terms of approval are limited to those products, parts and appliances and to the activities specified in the scope of work section of the approved maintenance organisation exposition, Maintenance Organisation Exposition reference: Date of original issue: Date of last revision approved: Revision No: Signed: For the competent authority: [COMPETENT AUTHORITY OF THE MEMBER STATE (*)] EASA Form 3-145 Issue 4 (*) Or EASA if EASA is the competent authority. (**) Delete as appropriate if the organisation is not approved. (***) Complete with the appropriate rating and limitation. (****) Complete with appropriate limitation and state whether the issue of airworthiness review certificates is authorised or not. CLASS RATING LIMITATION BASE LINE AIRCRAFT (**) (***) (***) [YES/NO] (**) [YES/NO] (**) (***) (***) [YES/NO] (**) [YES/NO] (**) (***) (***) [YES/NO] (**) [YES/NO] (**) (***) (***) [YES/NO] (**) [YES/NO] (**) ENGINES (**) (***) (***) (***) (***) COMPONENTS OTHER THAN COMPLETE ENGINES OR APUs (**) (***) (***) (***) (***) (***) (***) (***) (***) (***) (***) (***) (***) SPECIALISED SERVICES (**) (***) (***) (***) (***) ’

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Other provisions in Commission Implementing Regulation (EU) 2019/1383

Compiled from an official source version. Later amendments or repeals may not be reflected; the official text prevails. · Read the official text ↗ · Data as of 2026-07-04

CitationANNEX II of Commission Implementing Regulation (EU) 2019/1383 (LawPlayer, data as of 2026-07-04)

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