25
MAY
2018

Continuing airworthiness of type design (CAP)

PR.CAP.00001

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.

 

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