Structural analysis of aircraft modifications, including design support, and preparation of technical documentation necessary to ensure airworthiness Determination of stress levels in primary and secondary aircraft structure, systems, and equipment resulting from applied and induced loads, as well as the comparison of these stresses with material properties to predict failure and structural instabilities given due consideration to applicable failure theories
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Job Type
Full-time
Career Level
Entry Level
Number of Employees
5,001-10,000 employees