Principal Stress Engineer

Responsibilities

• Support the production concessions of aircraft structure and are responsible for the creation of quality solutions in a timely manner from a design point of view
• Perform stress analysis for both metallic and non‑metallic parts
• Work in close collaboration with design colleagues to provide solutions
• Use classical hand calculations and computer techniques to develop efficient solutions to satisfy airworthiness requirements
• Ensure safety, efficiency, and regulatory compliance while adhering to the terms of the concession
• Autonomously perform unusually complex stress calculations for metallic, composite, and hybrid structures
• Assess design solutions for manufacturing non‑conformities, airframe repairs, and modifications to the aircraft definition
• Ensure appropriate Airbus methods, processes and procedures are followed
• Liaise with and support stakeholders such as Design, Manufacturing, Quality, and other Airbus departments

• Bachelor of Science (BS) Degree in Engineering (Aero, Civil, Mechanical) with a strong curriculum emphasis on structural design and analysis and mechanics of materials
• 13 years total experience in stress analysis with airframe structures
• Experience in airframe design (metallic & composites)
• F&D T, SRM, MRB, FAR/JAR/CS/Part 25, Certification
• CATIA, NASTRAN, and PATRAN
• In‑depth knowledge of technical principles of engineering
• Applied knowledge of technical documentation, techniques and procedures
• Strong computer background including MS Office (Outlook, Excel, Word, PowerPoint) and Google Suite (Docs, Sheets, Slides, Gmail)
• Authorized to work in the US
• Working knowledge of all Airbus Structures