Engineer will perform stress and fatigue analysis to support design and write certification reports for a new aircraft program. Analysis may include primary airframe structure, secondary airframe structure, systems stress analysis, and fatigue and damage tolerance analysis. Performs stress and fatigue analysis, approves drawings for structural integrity and compliance to the FAR’s in a timely manner. Documents stress analyses in yellow sheet report system for each drawing. As required, documents analyses in formal reports for FAA approval. May review and approve supplier drawings, stress reports and test reports. May plan and support structural tests as required. Coordinates with the design groups, manufacturing, FEM group, test group and damage tolerance group and others as required.
Education and Experience
Bachelors degree in Aerospace, Mechanical, or Civil Engineering required. Minimum of 5 years stress analysis experience of primary airframe structure, systems, and/or fatigue and damage tolerance analysis. Composites structures experience a plus. Must have worked on aircraft structures.
12+ months — possible extension and possible FTE opportunity.
Requirements
What you'll need
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