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Advanced Technology Innovation Corp. · Posted Nov 3, 2026
Required Skills and Experience Bachelor's degree in Engineering from an accredited institution. 8+ years of experience in the aerospace industry with strong design emphasis. An equivalent combination of education, experience, and other projects may be considered. Knowledge of aircraft structural design and familiarity with industry standards for the manufacture, repair, and assembly of components. Prior work experience designing aircraft/spacecraft primary and secondary structures. Prior work experience designing vehicle systems integration accommodation. Significant experience using CAD software and composite workbenches to design aircraft/spacecraft structures and components. Experience with GD&T per ASME Y14.5, functional tolerancing, drawing creation, assembly tolerance stack-up analysis. Experience with Product Lifecycle Management tools (PLM software), requirements management tools, and configuration management. Proficiency in MS Office, technical writing skills, the ability to communicate and present technical material to various stakeholders. A high degree of autonomy, ability to work quickly and prioritize tasks in a fast-paced environment as part of a team or individually. Strong time management and organizational skills. Demonstrate willingness to adjust thinking and behavior. Ability to communicate effectively with peers and leadership in a manner that is timely, respectful, and open to other ideas. Preferred Skills and Experience Degree in Mechanical Engineering, Aerospace Engineering or similar from an accredited institution. Experience with CATIA V5 and/or CATIA 3DX. Experience with CATIA V5 CPD (Composite Part Design) and/or FiberSIM. Experience designing sheet metal parts Experience designing with aerospace fastener systems Knowledge of composite aircraft structural design and familiarity with industry standards for the manufacture, repair, and assembly of components. Prior work experience designing bonded composite structures. Experience with the design of flight vehicles or vehicle systems to a set of requirements or standards such as CFR 14, Part 400, Part 23 and 25, military or NASA. Familiarity with MRB tasks associated with dispositioning non-conformant metallic and composite components resulting from manufacturing, assembly, or field operations.