STC Applications can be of two types: An application from an EU organization for the EASA approval of a new STC. This requires that the applicant has Design Organisation Approval (DOA) or, at least, Alternative Procedures (AP to DOA). An application from a non-EU organization for the EASA validation of a non-EU STC. The application…
Introduction The principal source regulation concerning aircraft airworthiness in EASA Certification Framework is found in ICAO international standard of Annex 8 which defines “airworthy” – in respect of an aircraft, engine, propeller or part thereof – as “The status of an aircraft, engine, propeller or part when it conforms to its approved design and is…
Today, the two main aircraft certification systems are FAR 25 regulations and CS 25 regulations (Essentially Harmonised Regulatory Codes however each authority has the right to require specific conditions. Certification Introduction Certification is a regulatory obligation, with all aircraft, their engines and propellers certifiable. The “Type Certificate” – issued to signify the airworthiness of an…
Review the Following Details of ageing aircraft system requirements with any specified sampling programmes, (if applicable) Details of specific structural maintenance programmes, (if applicable), including but not limited to: a. Damage Tolerance and Supplemental Structural Inspection Programmes (SSID) SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAMME (SSIP) Increased utilisation, longer operational lives, and the high safety demands imposed on…
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