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The successful candidate will perform the following duties:
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Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as an integrated team
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Structural analysis includes calculation of loads, Static analysis, Fatigue analysis, Damage-Tolerance analysis, and Vibration analysis
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Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method
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Generate documentation to report analysis and, test results to supportcertification/qualification
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Support Gated Reviews to validate the quality and completeness of work packages
Full Time