This procedure describes how the European Aviation Safety Agency (EASA) shall internally handle the continuing airworthiness functions related to type design pursuant to Article 20(1)(j) of Regulation (EC) No. 216/2008 (Basic Regulation).
It applies to the continuing airworthiness functions related to the type design of aeronautical products, parts and appliances under the Agency´s scope of competences pursuant to the Basic Regulation.