ANNEX IISupplementary provisions
ANNEX II Annex I (Part 21) to Regulation (EU) No 748/2012 is corrected as follows: (1) point 21.A.15 is corrected as follows: (a) the first paragraph of point (b) is replaced by the following: ‘(b) An application for a type-certificate or restricted type-certificate shall include, as a minimum, preliminary descriptive data of the product, the intended use of the product and the kind of operations for which certification is requested. In addition, it shall include, or be supplemented after the initial application by, a certification programme for the demonstration of compliance in accordance with point 21.A.20, consisting of:’; (b) point (d) is replaced by the following: ‘(d) An application for a type-certificate or restricted type-certificate for an aircraft shall include, or be supplemented after the initial application by, an application supplement for approval of the operational suitability data.’; (2) point 21.A.93 is corrected as follows: (a) the first paragraph of point (b) is replaced by the following: ‘(b) An application shall include, or be supplemented after the initial application by, a certification programme for the demonstration of compliance in accordance with point 21.A.20, consisting of:’; (b) point (2) of point (c) is replaced by the following: ‘2. apply for an extension of the time period provided for in the first sentence of point (c) for the original application and propose a new date for the issuance of the approval. In that case, the applicant shall comply with the type-certification basis, operational suitability data certification basis and environmental protection requirements, as established by the Agency in accordance with point 21.A.101 and notified in accordance with point 21.B.105, for a date to be selected by the applicant. However, that date shall not precede the new date proposed by the applicant for the issuance of the approval by more than five years for an application for a change to type-certificate or restricted type-certificate for a large aeroplane or a large rotorcraft, and by more than three years for an application for a change to any other type-certificate or restricted type certificate.’; (3) in point 21.A.174, point (ii) of point (b)(3) is replaced by the following: ‘(ii) a non-member State: — a statement by the competent authority of the State where the aircraft is, or was, registered, reflecting the airworthiness status of the aircraft on its register at the time of transfer; — a weight and balance report with a loading schedule; — the flight manual when such a manual is required by the airworthiness code for the aircraft; — historical records to establish the production, modification and maintenance standard of the aircraft, including all limitations associated with a restricted certificate of airworthiness issued in accordance with point 21.B.327; — a recommendation for the issuance of a certificate of airworthiness or restricted certificate of airworthiness and for an airworthiness review certificate pursuant to an airworthiness review in accordance with Annex I (Part-M) to Regulation (EU) No 1321/2014 ( *1 ) or an airworthiness review certificate in accordance with Annex Vb (Part-ML) to Regulation (EU) No 1321/2014. — the date on which the first certificate of airworthiness was issued and, if the standards of Volume III of Annex 16 to the Chicago Convetnion apply, the CO 2 metric value data.; ( *1 ) Commission Regulation (EU) No 1321/2014 of 26 November 2014 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks ( OJ L 362, 17.12.2014, p. 1 ).’;" (4) in point 21.A.181, point (1) of point (a) is replaced by the following: ‘1. compliance with the applicable type-design and continued airworthiness requirements; and’; (5) in point 21.A.211, point (1) of point (a) is replaced by the following: ‘1. compliance with the applicable type-design, environmental protection and continued airworthiness requirements; and’; (6) in point 21.A.431B, point (2) of point (a) is replaced by the following: ‘(2) that follow design data included in certification specifications issued by the Agency, containing acceptable methods, techniques and practices for carrying out and identifying standard repairs, including the associated instructions for continued airworthiness; and’; (7) in point 21.A.432C, the first paragraph of point (b) is replaced by the following: ‘(b) An application for a major repair design approval shall include, or be supplemented after the initial application by, a certification programme containing:’; (8) in point 21.A.711, point (d) is replaced by the following: ‘(d) An approved organisation may issue a permit to fly (EASA Form 20b, see Appendix IV) under the privilege granted in accordance with point M.A.711 of Annex I (Part-M) of Regulation (EU) No 1321/2014 or point CAMO.A.125 of Annex Vc (Part-CAMO) of Regulation (EU) No 1321/2014 or point CAO.A.095 of Annex Vd (Part-CAO) of Regulation (EU) No 1321/2014, when the flight conditions referred to in point 21.A.708 of this Annex have been approved in accordance with point 21.A.710 of this Annex;’; (9) in point 21.B.325, point (c) is replaced by the following: ‘(c) For aircraft originating from a non-member State, in addition to the appropriate airworthiness certificate referred to in point (a) or (b), the competent authority of the Member State of registry shall issue: 1. for new or used aircraft subject to Annex I (Part-M) to Commission Regulation (EU) No 1321/2014, an initial airworthiness review certificate (EASA Form 15a, Appendix II); 2. for new aircraft subject to Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014, an initial airworthiness review certificate (EASA Form 15c, Appendix II); 3. for used aircraft subject to Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014, an initial airworthiness review certificate (EASA Form 15c, Appendix II), when the competent authority has performed the airworthiness review.’ (10) in Appendix II, EASA 15c – Airworthiness review certificate is replaced by the following: ‘ Airworthiness Review Certificate – EASA Form 15c NOTE: persons and organisations performing the airworthiness review in combination with the 100-h/annual inspection may use the reverse side of this form in order to issue the CRS referred to in point ML.A.801 corresponding to the 100-h/annual inspection. AIRWORTHINESS REVIEW CERTIFICATE (ARC) (for aircraft complying with Part-ML) ARC reference: ……….. Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council: [NAME OF THE COMPETENT AUTHORITY] (**) hereby certifies that: ☐…..it has performed an airworthiness review in accordance with Regulation (EU) No 1321/2014 on the following aircraft: [or] ☐.….the following new aircraft: Aircraft manufacturer:………………………………….Manufacturer’s designation:…………………………… Aircraft registration:……………………………………Aircraft serial number:…………………………………. (and that this aircraft) is considered airworthy at the time of the review. Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of review (*): ……………………………………………………………….. Signed: ............................................................................Authorisation No (if applicable): ………………………. [OR] [NAME OF APPROVED ORGANISATION, ADDRESS and APPROVAL REFERENCE] (**) [or] [FULL NAME OF THE CERTIFYING STAFF AND PART-66 LICENCE NUMBER (OR NATIONAL EQUIVALENT)] (**) hereby certifies that it has performed an airworthiness review in accordance with Regulation (EU) No 1321/2014 on the following aircraft: Aircraft manufacturer:………………………………….Manufacturer’s designation:…………………………… Aircraft registration:……………………………………Aircraft serial number:…………………………………. and that this aircraft is considered airworthy at the time of the review. Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of review (*): ……………………………………………………………….. Signed: ............................................................................Authorisation No (if applicable): ………………………. =================================================================================== 1st extension: The aircraft complies with the conditions of ML.A.901(c) of Annex Vb (Part-ML) Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of issue (*): …………………………………………………… ……………… Signed: ............................................................................Authorisation No: ……………………… Company name: .............................................................Approval reference: ……………………………………... =================================================================================== 2nd extension: The aircraft complies with the conditions of ML.A.901(c) of Annex Vb (Part-ML) Date of issue: ..................................................................Date of expiry: ………………………………………….. Airframe flight hours (FH) at date of issue (*): …………………………………………………… ……………… Signed: ............................................................................Authorisation No: ……………………… Company name: .............................................................Approval reference: ……………………………………... (*) Except for balloons and airships (**) The issuer of the Form can tailor it to his need by deleting the name, the certifying statement, the reference to the subject aircraft and the issuance details that are not relevant for his use. EASA Form 15c, Issue 4’. ( *1 ) Commission Regulation (EU) No 1321/2014 of 26 November 2014 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks ( OJ L 362, 17.12.2014, p. 1 ).’;’