INTRODUCTION Subpart J regulatory approval provides for the Design of Aircraft and Components Design Organisation Approval (DOA). The responsibilities associated with the management of a Design Organisation are numerous and varied with a constant flow of challenges. The primary function of the DOA holder is to assume full responsibility for all designed product (Initial Airworthiness)…

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Introduction The course focuses on the relationship between EASA Driven Airworthiness Regulatory obligations and the methods whereby Industry is able to show compliance. Using EASA regulatory compliance as the baseline with appropriate consideration of both the Federal Airworthiness Authority (FAA) and International Civil Aviation Organisation (ICAO) EASA Airworthiness regulation within the commercial environment is deeply…

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Introduction – Certification requirements for civil [commercial] aircraft are derived from ICAO Annex 8 Airworthiness of Aircraft together with ICAO Airworthiness Manual, Part V State of Design and State of Manufacture. Each ICAO contracting state is obligated to establish its own legal framework. Within the European Community this activity is undertaken by EASA essentially harmonised…

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Introduction – The role of the CAMO is wide reaching with an obligation to ensure the ongoing status of the Continuing Airworthiness of the Operators Fleet. Having a detailed awareness related to the Management of Repairs and Supplemental Type Certificates (STC’s) is an important element of the full role of Continuing Airworthiness. The course focuses…

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INTRODUCTION Subpart J regulatory approval provides for the Design of Aircraft and Components Design Organisation Approval (DOA) and Subpart G provides for a Production Organization approval (POA). The primary function of the DOA holder is to assume full responsibility for all designed product (Initial Airworthiness) including the need to support Continued Airworthiness of the designed…

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INTRODUCTION Subpart J regulatory approval provides for the Design of Aircraft and Components Design Organisation Approval (DOA) and Subpart G provides for a Production Organization approval (POA). The primary function of the DOA holder is to assume full responsibility for all designed product (Initial Airworthiness) including the need to support Continued Airworthiness of the designed…

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