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| Ref # |  | JS202449 |
| Year of birth | | 1968 |
Permanent/Home Location/Address |
| City or Town | | Kherson |
| Country | | UKRAINE |
Current Location/Address |
| Country | | UKRAINE |
Languages |
| Primary Language | | Fluency |
| English | | Read, write and speak fluently |
Nationalities |
| Main Nationality | | UKRAINE |
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Experience Classification |
| Job Function | | Years Experience |
| Aerospace Engineer | | 17 |
| CAD/CAM Engineer | | 17 |
| Design Engineer | | 17 |
| Engineering Manager | | 14 |
| Project Engineer | | 17 |
| Industry | | Years Experience |
| Aerospace and Aviation | | 17 |
| Engineering | | 17 |
| Manufacturing | | 17 |
Qualifications |
| Highest Qualifications | | Masters |
| Qualification | Subject | Establishment/Country | Year |
| Masters or Higher | aircraft construction | Ukraine | 1993 |
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Computer Skills and Software Used |
Several CAD/CAM systems including CATIA V5, NX6, SolidWorks, FEMAP, MSC PATRAN/NASTRAN, ANSYS etc.
MS Office products including MS Project. |
Work Locations |
| Are you willing to move or relocate? | |
Yes - I will travel domestically
Yes - I will relocate domestically
Yes - I will travel internationally
Yes - I will relocate internationally | |
Availability |
| Start Immediately? | | Available Now |
Ideal Next Job |
Aicraft structures design, modification, analysis.
Composite structures design and analsys. |
Required Salary & Conditions |
| min USD 5,000 a month |
Employment History |
| Total Years of Work Experience: | | 19 |
| Commenced Full Time Work: | | 1993 |
| Name | | Advanced Design Alliance |
| Job Title: | | Structural Engineer |
| Duration | | From : 2006 To: |
Summary |
Aircraft design, development and certification.
Composite structures design and manufacturing process development.
Loads definition, structural design and analysis.
Compliance verification.
Project management. |
Work Experience |
2006 – Present
Advanced Design Alliance, A Private Company, Kherson, UKRAINE
Project Engineer
Advanced Composite 5-seater
Preliminary design, structural design and analysis.
Adam A500 composite flap structural analysis
FE- modeling, linear and non-linear static analysis, optimization.
Engine Powered Glider
Design, development and certification of an engine powered glider.
Responsibilities: configuration layout; aerodynamics analysis; stability evaluation; structural analysis; communication to DULV certification authority in Germany; loads definition; load tests; prototype manufacturing; compliance verification.
Lancair Legacy.
Building of an aircraft from the kit in favor of a private customer: airplane configuration, communication between the customer and Lancair Performance Aircraft (the kit manufacturer), resolving issue of running Continental IO-550-N engine on 95 octane auto gas due to shortage of 100LL (avgas) in Ukraine, and organization of actual building of the airplane.
A winglet for a propjet
Design of a winglet for Epic Aircraft: develop a 3D model of the winglet based on aerodynamic analysis output and actual wing geometry.
2002 – 2006
Flight Design GmbH , Stuttgart, Germany
Engineering subdivision EUA, Kherson, UKRAINE
Director of Engineering
Flight Design MC-01
Project responsibilities: preliminary design; loads definition per CS-VLA requirements; structural design and FE analysis; prototype manufacturing.
Flight Design CT modifications CT2K, CTSW, CTSW2006.
Project responsibilities:
• structural analysis, drawings and drawing changes approval throughout product life cycle;
• certification per as follows:
- US Light Sport Aircraft (LSA, F2245, F2279, F2295 ASTM Specifications);
- German LTF-UL;
- Canadian Design Standards for Advanced Ultra Light Aeroplanes;
- Swiss certification per LTF-UL including compliance of manufacturing and manufacturing quality systems;
• typical certification responsibilities included: communication to the authorities; setting up certification plan; checking and pre-approval of load calculation reports; load tests supervision; flight test program development; Maintenance Manual, Pilot Operating Handbook, QA Manual review and development; checking and pre-approval of compliance documentation.
• support of marketing and sales for feasibility studies;
• non-conformance reports resolution and approval;
• support of customer service regarding specific repairs and installations.
Other projects:
• Setting up preconditions for certification as a Design Organization per EASA Part 21 by means of development and implementation of appropriate procedures including:
- Change Review Board concept development and implementation;
- Engineering Procedures Manual development and implementation;
• Quality Management System per ISO9001 and AS/EN9100 standards development and implementation.
2001 – 2002
Lancair Certified Aircraft, Bend, OR, US – now Cessna
Design Engineer
Familiarization with certified aircraft production.
Columbia 350 (FAR Part 23 certified aircraft) projects: air conditioning system installation; horizontal stabilizer installation; toe-in and camber issue investigation; door surface modeling; main landing gear attachment modification.
1993 – 2001
Flight Design GmbH , Stuttgart, Germany
Manufacturing and Engineering subdivision OWC, Kherson, UKRAINE
CF-45 five seater, preliminary design.
Project responsibilities included: statistics evaluation; arrangement for 5 people and new Rotax 936 engine; airplane lofting including 3-D surface model.
Rigid Wing (hang-glider) full-cycle development up to serial manufacturing (40 pieces a month).
Project responsibilities: loads and stress calculation based on a given concept and sketches; load tests and certification documentation; tooling development; setting up and running serial manufacturing with about 70 people.
Flight Design CT
• power plant design for Rotax 912 and Hirth F30 engines;
• engine mount stress analysis;
• engine compartment lofting;
• power plant prototyping;
• tooling development;
• flap and ailerons hinges design and stress analysis;
• aircraft prototyping. |
Last Updated on 08-Jan-12
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