Artem Komisarenko

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Activity as Head of Office of Airworthiness of EASA DO 21J.416

Position of Design Engineer and Compliance Verification Engineer in EASA certified Design Organization 21J.416.

Activity as head of Office of Airworthiness 21J.416.

Performing of tasks as nominated DE and CVE, HoA within EASA approved Flight Design DO; Performing of tasks and activity coordination as Office of Airworthiness and depytu HoA under Authority of EASA, FAA, etc; Perorming of tasks related to COSM of FD Products; Interface function between Design and Production Organization (especially with sections in Ukraine).

Deputy of Head of Airworthiness for Flight Design Design Organization (Part 21, Subpart J). EASA nominated as Design Engineer, Compliance Verification Engineer for disciplines: Structures, Loads, Flight Mechanics, Aerodynamics, Flight Test, Aeroelasticity, Flammability, COSM (Continued Safety Operational Monitoring). Design development and certification support for CT, CT Supralight, MC, C4 aircraft models according to the requirements of ASTM F2245, ASTM F2316, LTF-UL 2003, CS-LSA, CS-VLA, Part 23, etc.

Management and development of Project teams (CT, MC, C4). Planning and coordination of general projects activity. Performance of activity as Head of Design in the range of Design Organization according requirements of EASA Part 21. Coordination of DO activity with subcontractors and members of DO. Performance of planned trainings of DO members and subcontractors.

Creation and development of engineer team for design of new model of four-seat aircraft C4. Development of conceptional design of aircraft. Performance of basic general flight loads analysis, load analysis of units. Development of aircraft design variants according specified certification basis. Management of project engineers team, support of team activity, professional training of team members.

Design of parts and units of CT and MC aircraft models, load analysis and loads stress calculations, development of 3D models and design drawings, certification tests performance, development of technological production jigs and technological documentation.

General aeronautical engineering, Aerodynamics and Flight dynamics, Aircraft units design, Aircraft systems design, Strength of aircraft components and systems.