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Aidan Foley Resume


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Aidan Foley Resume

  1. 1. AIDAN FOLEY Tucson, Arizona area 480.227.5391 SUMMARY OF QUALIFICATIONSProject Engineer. Mechanical Design Engineer. Control Account Manager. Checker. Over 15 Years Experience.Aerospace. Defense. Aviation. Former U.S. Marine. Patent Holder. Previous DoD Secret Clearance. MS Office.Unigraphics. UG. Siemens NX 7.5. Teamcenter 8. CATIA V5. ENOVIA. MathCAD. CAREER HIGHLIGHTSProject Engineer, B/E Aerospace, Tucson, Arizona, 2011 - presentLufthansas new-buy Airbus A330s, retrofit A340s, and Boeings 747s new business class luxury passenger suites Addressing 140+ discrepancies, squawks, and management’s top 20 issues as Tiger Team member.Senior Advanced Engineer, Honeywell Aerospace, Glendale, Arizona, 2009 - 2011A2100, MUOS, Star 2, CrIS, and AEHF satellite reaction wheel assemblies Reduced costs by 7/8’s by updating UTA procedure in 4.5 days versus 6 weeks including a 58% increase. Selected as Project Manager to lead 5 satellite reaction wheel projects valued at over $10M.Senior Engineer, Orbital Sciences, Chandler, Arizona, 2006 - 2009FTF, MRT, KEI, and GMD launch vehicles and targets for the Missile Defense Agency Adaptability within 4 functions: Engineering, Control Account Manager, Checking, and Manufacturing. Accountable as KEI CAM for Mechanical Engineering labor budgeted at over $11M. Organized status on over 400 drawings and 200 tasks for upper management review and corrective action. Reduced errors to less than 5% by providing DFM Checking support on over 300 drawings.Design Engineer, ATK, Mesa, Arizona, 2004 - 2005Bushmaster III, M230, M242, and MK44 medium caliber automatic cannons Saved $35K over 4 months by improving on checking compliance through the drawing release cycle. Completed Tooling documentation and transition early in 7 weeks out of a 26 week allotted schedule.Engineering Scientist, Boeing, Mesa, Arizona, 1996 - 2004AH-64D, MELB, and Canard Rotor Wing helicopters Demonstrated versatility across 4 departments: Drive Systems, Rotors, Airframe, and Testing. Tripled rapid deployment capability from 2 to 6 ships by patented main rotor blade nesting. Lowered engine nose gearbox cover install time from 12 hours to 20 minutes by composite redesign effort. Reduced part count from 36 to 4 by high speed machining conversion on primary fuselage bulkhead. Worked within 55% of budget in qualifying Suppliers by designing multiple table-top fatigue tests. EDUCATIONBachelor of Science, Mechanical Engineering, BSME, Suffield University, Twin Falls, IdahoProject Management Professional, PMP, Interface Technical Training, Phoenix, Arizona