This position conducts stress analyses on designs of experimental, prototype, or production aircraft mission equipment, and related components to evaluate the ability to withstand stresses imposed during flight or ground operations imposed by static, dynamic, or thermal loads, due to operational or test conditions. The role is responsible for entire projects with significant scope and complexity, contributing to the department or business unit by applying advanced knowledge of one or more functional areas. This includes analyzing, researching, and developing structural engineering specifications for various materials, analyzing damage tolerance, durability, design allowables, and structural modeling. The Engineer II will study preliminary specifications and design requirements to determine strength and bending characteristics of parts, assemblies, and total airframe, consult with design personnel regarding analysis results and necessary modifications, and formulate mathematical models or devise other computer analysis methods to assist in stress analysis.
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Job Type
Full-time
Career Level
Mid Level
Number of Employees
11-50 employees