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As a contract mechanical and stress engineer, I worked for Boeing for twelve years and during this period was involved in all stages of developing new wide-body aircraft, from concept studies through first flight and subsequent in-service repairs.
Boeing 787 Dreamliner
I have worked on all aircraft variants of this family (787-8, 787-9 and 787-10) and on most primary and secondary structural elements (regular fuselage sections, door cutouts, floors, bulkheads, cargo barriers, etc.) as well as aircraft systems (ECS, ICS, PECS, waste water, landing gear, nacelle, etc.).
The work included FEM and hand stress analysis of composite parts, honeycomb panels, titanium and aluminum alloy components, combined splices, preparation of stress templates, and development of SCN documentation in accordance with FAA requirements and Boeing standards.
During the last two years, I worked in Customer Support and was responsible for repairs of fuselage structures after significant in-service damage not covered by the SRM.
Boeing 777-9
Responsible for the structural integrity of the Section 46 door cutout reinforcement.
The work included static and fatigue analysis of aluminum components, joints and splices.
I also led a team of engineers throughout all project stages and coordinated with stakeholders from structures, systems, payloads and other disciplines to implement required design changes.
Boeing 737-800BCF
Passenger-to-Freighter (P2F) conversion program. Performed static and fatigue analysis of keel beam structures.
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