Denver, Colorado, United States
I ensure the parts used on the structure of the aircraft are designed efficiently by performing a multitude of structural checks. I need to take into account the loading conditions, material properties, temperature and program requirements to effectively complete the task. A completed job will show that the structure passes all possible failure modes with positive margins of safety by submitting a report called a strength check note. • Produced baseline analysis strength check notes on the 737 MAX fan cowl hinge fittings, T-Clips, • Extracted loads by identifying finite elements using Patran that correspond to relevant structure for analysis. • Performed analysis by creating common structures workstation templates for ease of use on future load revisions and geometry changes to existing fan cowl structure. • Recommended corrective action for design changes to hinge fittings, cross engine debris shield brackets, and T-Clip structure. • Generated 10 non-conformance report analyses on the 737 MAX Inlet.
• Stress analyst for the 787 Dreamliner • Completed Structural Repair Manual for wing leading edge and elevator skin of the empennage • Analysis included feasible repair options with viable materials, configurations, and locations • Created templates for repair analyses using Common Structures Workstation (CSW)