POWERLINK

Electronic computer-based systems for regulating ignition and fuel injection of piston aircraft engines, namely, digital speed and fuel flow rate-control computers, manifold temperature sensors, cylinder head temperature sensors, exhaust gas temperature sensors, manifold pressure sensors, fuel pressure sensors, engine speed sensors, fuel injector solenoids, microprocessor circuit boards, electronic control units, throttle position switches, high voltage coils, electrical wiring, electrical connectors, fuel pump relays, engine data download ports, and interferences and monitors for displaying engine data collected by the computer-based systems