Oda Unit Member, Structures F&Dt
L-3 is a global provider of mission-critical technologies to military and commercial customers. The Platform Integration Division provides innovative solutions for major structural modifications and systems integration to military and commercial aircraft.-- ODA Unit Member, Structures, Fatigue and Damage Tolerance. (January 2015 - October 2016); Auth 14CFR 23 & 25; A3, A4, A12, B3, B4, C3, C4, D3, D4, E3, E4, I10 and Repair & Alterations P3 & P9-- Lead, Fatigue & Damage… Show more L-3 is a global provider of mission-critical technologies to military and commercial customers. The Platform Integration Division provides innovative solutions for major structural modifications and systems integration to military and commercial aircraft.-- ODA Unit Member, Structures, Fatigue and Damage Tolerance. (January 2015 - October 2016); Auth 14CFR 23 & 25; A3, A4, A12, B3, B4, C3, C4, D3, D4, E3, E4, I10 and Repair & Alterations P3 & P9-- Lead, Fatigue & Damage Tolerance Analysis. (February 2013 – October 2016) Lead fatigue and damage tolerance engineer for all structural modifications made to Dassault Falcon 2000S, Lockheed EC-130 E & H, AT-802L and Cessna U-35o Review and approval of all engineering drawings; verify M&P specs and approve processing sequence.o Meet the requirements of FAR 25.571, including Instructions for Continued Airworthiness under FAR 25.1529 and App. H to Part 25; and, Subpart E of Part 26 to obtain STC.o Developed inertial load (ny, nz) spectra for supported masseso Supervised 5 technical staff and provided mentoring to three of themo Review and approve reports for ODA; generate compliance reportso Developed flight loads fatigue spectra for fuselage and wing structureo Specified the analysis methodology to be usedo Computed SSF using estimated SCF; devised approximations for SIF for DT analyseso Initiated and supervised the modification of the joint analysis program-- Fatigue & Damage Tolerance Analyst. (June 2012 – January 2013). Analysis of fatigue critical structural elements of the Sikorsky MH-60M U.S. Army Helicopter.o Computed damage fraction of elements under flight by flight spectrum using actual flight test loads.o Developed fastener loads in complex riveted and bolted joints.o Computed SSF using estimated SCFso Extraction of local stresses from NASTRAN FEMo Prepared final fatigue analysis report. Show less
