I am an experienced electronic engineer design professional capable of implementing all phases of product development from conception through proposal, design, debug, qualification test, delivery installation and integration on both military and commercial avionics systems. My strengths include documentation and attention to details. I have experience taking customer specifications and developing advanced products to meet and exceed customer requirements.

Customer interface and systems responsibility as well as documentation, testing and integration.Advanced Products product line: • Guided the design and development of two different test equipment systems for Comac-C919 and directed and managed an outsource engineering firms work product. • Coordinated documentation deliverables for Boeing.767-2C Inerting Controller. • Headed the reuse and modification of a previously certified unit for P-42/Gulfstream 650 Hydraulic Quantity Indicator. • Organized a parts obsolescence redesign of the F-15 Enhanced Engine Monitor Display.Controllers product line: • Executed an obsolescence redesign of the F-18 Aerial Refueling Pod control system. • Generated system design and requirements of an Internal R&D project to control a Hydrogen Fuel Cell and associated support equipment in cooperation with Airbus. • Orchestrated all aspects of the design through FAA certification and customer interface of the electronics portion of a foam based fire detection and suppression system for cargo aircraft. • Designed, built and qualified a Ground Crew Refuel Controller for the Airbus A350. • Headed the design, qualification and Highly Accelerated Life Testing (HALT) of a three motor Brushless DC controller for steering a smart munition. • Generated system design, mechanical packaging and requirements of a Brushless DC Motor controller for an electronics heat rejection system.

Implement designs and follow through to completion and delivery, equipment to perform verification of the signals in space for in-route (VOR/DME) and terminal (ILS/GS) aircraft navigation aids. • Designed, built, tested, installed and flight tested JCAB (Japanese FAA) #2, JCAB SAAB and Thailand Automatic Flight Inspection Systems. • Designed, built and qualified a Ground Crew Refuel Controller for the Airbus A380. • Designed, built and tested a prototype low cost flight inspection system called fLite Checker. • Designed, built and authored User and Installation manuals for the Differential GPS/DATALINK Interface Unit. • Designed, built and wrote Maintenance Manuals and Test Procedures for a TV Positioning System camera Test Set.

Implement and document the designs, perform the testing and interface with the customers for contracted programs. • Designed, built and qualified a Ground Crew Refuel Controller for the Airbus A340. • Designed, built and qualified a Ground Crew Refuel Controller and Cockpit Fuel Quantity Display for the McDonald Douglas MD-80/90 and Boeing 717.

Implement and document the designs, and perform the testing for contracted programs. • Designed test equipment and authored Acceptance Test Procedures for: • the MD-80/90 and Boeing 717 Fuel Quantity Gauging System production testing. • the MD-11 Fuel Quantity Gauging System, for production testing and for SwissAir. • the AMG-136 Tacit Rainbow Fuel Pump Controller. • the Multiplex Junction Probe Portable Tester. • Repackaged and qualified the MD-11 cockpit BITE display and the Ground Crew Refuel Controller into a single unit for McDonald Douglas’s C-17 Globemaster. • Designed, built and qualified the Manual Fuel Control Panel for the B-2 Spirit cockpit. • Designed built and qualified the cockpit BITE display and the Ground Crew Refuel Controller for McDonald Douglas MD-11. • Designed and built a dichroic LCD Fuel quantity display for the Grumman A6.

USH-26 Serpentine Tape Drive Controller (Z80)Processor based implementation of a tape cartridge system controller which allowed data to be recorded in both the forward and reverse directions on alternating tracks.

ILASS switch controllerMicroprocessor based controller for the switching system of a very large test station. This controller received commands via a IEEE-488 interface and programmed all signal paths from stimulus and response sources to units under test. Continuous testing of programmed paths to preclude incorrect connections to UUT's was a major responsibility of this controller.Generated a single custom integrated circuit to replace a circuit card which utilized obsolete technology. This was a feasibility project to determine the usefulness of designing Semi-Custom Integrated circuits to replace functions rather than redesigning assemblies using medium scale integrated circuits.