Performs structural stress analysis for aircraft interior components and systems using hand calculations and finite element methods. Evaluates metallic and composite structures for static and durability performance, determines margins of safety, documents certification results, supports gated reviews, and guides structural design and configuration development. The role also involves trade studies, regulatory compliance with FAA and EASA requirements, and collaboration across engineering teams.

Performs structural stress analysis of aircraft seats and other interior components using classical calculations and finite element methods. Develops certification documentation, reviews supplier test plans and reports, evaluates metallic and composite structures, and determines structural integrity and margins of safety. Supports gated reviews, design configuration, trade studies, and regulatory compliance with FAA and EASA requirements while collaborating across engineering teams.