Contract to Goodrich, Phoenix, AZ-- Provided electrical engineering (EE) support to resolve EMI performance issues on the Readiness Indicator for the Emergency Evacuation System Slide on the Airbus A380 aircraft- Successfully completed EMI Qualification test of new configuration Readiness Indicator; expedited completion of documents to transition updated design into production- Completed A380 EE Slide Lighting Qual, Gas Generator Lightning Qual, Carbon Fiber Composite Direct Effects Lightning testing compliance and re-design/fabrication of lightning test equipment- Supported an Enhanced Readiness Indicator development effort

- Successfully used EVMS, Cost and Schedule Performance Index on S-92, F35, F-15 Programs- Successful in securing fast track approval of various data items on the Sikorsky 92 Rate Sensor, MFDS and F-15 Singapore programs; managed personnel, cost, risk mitigation and customer relations.Principal Electrical / Systems Engineer (SE) on F-15 Singapore and USAF Displays, 10/2007 – 04/2008- Completed Qualification Performance Testing and Test Report on the F-15 Singapore 6x6 Color DisplayTechnical Project Engineering Lead on Sikorsky S-92 and CMHP Programs, 10/2005 – 04/2008- Led Sikorsky S-92 Angular Rate Sensor Program through complete development life cycle- Responded to accelerated customer delivery request, achieved 100% on-time delivery, 2.5 year tenure- Gained significant improvement in customer satisfaction, increasing sales order by 50%- Implemented innovative PWB procurement strategy, reducing cycle time by 75%- Instrumental in achiving DO-160E and TSO Compliance- Transitioned S-92 to full rate production, as text book case, ahead of schedule and under budget- Introduced processes, schedule and cost improvements, which improved the bottom line- Technical leader of development effort of Rockwell’s EyeHUD™ HMD system for Sikorsky CMHPPrincipal Systems Engineer on the F35 Joint Strike Fighter (JSF) MFDS and HMD, 06/2002 – 09/2005- Provided SE support on the F35 JSF Helmet Mounted Display (HMD) System- Generated Power Variation Test Document for F35 JSF 8x20 Multifunction Display Systems (MFDS)- Researched and procured Programmable Power Analysis System as capital equipment for the MFDS- Performed the analysis and generated the Aircraft Performance Compliance Document for the MFDS- Supported DO-178B and SE of MFDS Computer Processor; used Power-PC processor, 1394B Fiber Optics, Ethernet, FPGA, CPLD, Bridge Chip, PCI, embedded software- Provided SE of the Optics and video path’s LED and lamp source for the MFDS

Non-DoD- Managed DO-160D Qualification of Modular Avionics Units for 7 OEMs; met DO-178B and DO-254 requirements, Met Safety Of Flight, Performance, Environmental and EMI compliance requirements- Managed simultaneous Qualification efforts on 5 of 7 OEMs from planning, test and report approvals- Implemented design changes to transition from red label to silver label to production black label

- Provided hands-on hardware technical support for various avionics systems for a 400+ aircraft fleet- Provided hardware, software and troubleshooting using various Automatic Test Equipment systems- Led technical effort, retrofitted EICAS, various Flat Panel Display Units (DU) and A320 Fuel System- Negotiated improved retrofit program agreement with supplier, within 2 months, after a 3 year stalemate, resulting in a 3 to 1 year schedule reduction and $2.5 million in savings- Assisted Warranty Repair Managers in recovering $350+ million in warranty repair claims in 5 years