Light aircraft managment system project

Light Aircraft Engine Management System

The engine management system for light aircraft was designed specifically for experimental ultra-light planes. Despite its compact size, this device provides essential readings for Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), Engine RPM, Fuel Flow and Level, and a HOPS meter.  The display features a large, sunlight-readable LCD with adjustable backlight controls.  After installation within an enclosure, the device fits into a standard 3 1/8” hole in the aircraft panel