21L.A.27 Requirements for the issuance of a type certificate

• Regulation (EU) 2022/1358 found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)

21L.A.27 Requirements for the issuance of a type certificate Regulation (EU) 2022/1358 In order to be issued with a type certificate, the applicant shall: (a)     demonstrate their design capability in accordance with point [21L.A.23](#_DxCrossRefBm1649097313); (b)     demonstrate the compliance of the design in accordance with point [21L.A.25](#_DxCrossRefBm1649097803); (c)      demonstrate, for aircraft type certificates, that the engine or propeller, or both, if installed on the aircraft, have either: 1.       a type certificate issued or determined in accordance with [Annex I](#_DxCrossRefBm1649096844) (Part 21) or issued in accordance with this Annex; or 2.       been included within the application for the aircraft type certificate and the applicant has ensured the compliance of the engine and propeller during the compliance demonstration in point [21L.A.25](#_DxCrossRefBm1649097803); (d)     demonstrate that there are no unresolved issues from the physical inspection of the first article of that product in the final configuration or any other investigation carried out by the Agency in accordance with points (c) and (d) of point [21L.B.46](#_DxCrossRefBm1649097807). #### 21L.A.27 Requirements for the issuance of a type certificate *Regulation (EU) 2022/1358* In order to be issued with a type certificate, the applicant shall: (a) demonstrate their design capability in accordance with point [21L.A.23](#_DxCrossRefBm485230805); (b) demonstrate the compliance of the design in accordance with point [21L.A.25](#_DxCrossRefBm485231299); (c) demonstrate, for aircraft type certificates, that the engine or propeller, or both, if installed on the aircraft, have either: 1. a type certificate issued or determined in accordance with [Annex I](#_DxCrossRefBm485230334) (Part 21) or issued in accordance with this Annex; or 2. been included within the application for the aircraft type certificate and the applicant has ensured the compliance of the engine and propeller during the compliance demonstration in point [21L.A.25](#_DxCrossRefBm485231299); (d) demonstrate that there are no unresolved issues from the physical inspection of the first article of that product in the final configuration or any other investigation carried out by the Agency in accordance with points (c) and (d) of point [21L.B.46](#_DxCrossRefBm485231303).