Develops, integrates and documents structural and interior payload system requirements to establish the system design
Develops, maintains and modifies structural and interior payload system and component designs, using 3-D Computer Aided Design tools and/or other design methods, to provide product definition to other engineering groups, production operations, suppliers and external customers throughout the product lifecycle.
Performs, integrates analytical and test results to validate and verify systems and components meet requirements and specifications.
Bachelor of Science degree in Engineering (with a focus on Mechanical, Civil, Aerospace Aeronautical or Material Sciences)
Strong understanding and demonstrated experience with FAA Title 14 Part 25 and/or EASA equivalent.