Continuing airworthiness of type design (CAP)

PR.CAP.00001

This procedure describes how the European Union Aviation Safety Agency (EASA) shall internally handle the continuing airworthiness functions related to type design pursuant to Article 22(1)(j) of Regulation (EU) 2018/1139 (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.