EN
L 205/38
Official Journal of the European Union
5.8.2022
2. that the test and measuring equipment used for the test were adequate for the test and appropriately calibrated.
(d) The flight testing for the purpose of obtaining a type certificate shall be conducted in accordance with the methods for such flight testing specified by the Agency.
The applicant for a type certificate shall make all the flight tests necessary to determine compliance with the applicable type-certification basis.
The flight tests shall include a period of operation in a final configuration of a sufficient duration to ensure that there will be no safety issues when the aircraft first enters service. (e) An applicant for a type certificate shall allow the Agency to: 1. review any data and information related to the demonstration of compliance; 2. witness or carry out any test or inspection conducted for the purpose of the demonstration of compliance; 3. conduct a physical inspection of the first article of that product in the final configuration to verify the compliance of the design with the type-certification basis and the applicable environmental protection requirements and any other investigation determined in accordance with point 21L.B.46. (f) Upon the completion of the compliance demonstration, the applicant shall declare to the Agency that: 1. they have demonstrated compliance with the type-certification basis and the applicable environmental protection requirements as established and notified to the applicant by the Agency in accordance with points 21L.B.43 and 21L.B.45, according to the compliance demonstration plan; and 2. no feature or characteristic has been identified that may make the product unsafe or environmentally incompatible for the uses for which certification is requested.
21L.A.26
Type design
The applicant for a type certificate shall define the product type design to enable its unique and unambiguous identification, consisting of: (a) drawings and specifications and a listing of those drawings and specifications that are necessary to define the configuration and the design features of the product; (b) information on the materials and processes used; (c) information on the methods of manufacture and assembly; (d) any airworthiness limitations; (e) the environmental compatibility requirements; and (f) any other data allowing by comparison the determination of the airworthiness, and, if relevant, the environmental compatibility of later products of the same type.
21L.A.27
Requirements for the issuance of a type certificate
In order to be issued with a type certificate, the applicant shall: (a) demonstrate their design capability in accordance with point 21L.A.23; (b) demonstrate the compliance of the design in accordance with point 21L.A.25; (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 (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; (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.