An electronic unit that continously monitors engine speed, temperature, and air flow and adjusts the fuel control, main, turbine engine to compensate for changes. Features may include load sharing capabilities, rotor speed governing, loss-of-load protection and analog or manual backup modes. It may contain automatic start capability or self-diagnostic circuitry.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6320-01-352-5653
NSN 6110-00-312-5414
NSN 5999-00-104-4862
NSN 5975-00-045-1715
NSN 5855-01-208-1471
NSN 2925-00-770-4713
NSN 6620-01-068-4498
NSN 6610-01-140-9608
NSN 5855-01-334-6594
NSN 5996-01-318-9337
NSN 5835-00-106-2120
NSN 6135-01-350-5845