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 6130-01-299-3375
NSN 6685-01-514-0431
NSN 5990-01-658-9964
NSN 6220-00-823-6688
NSN 5985-00-878-0823
NSN 5920-01-385-5707
NSN 6105-00-407-1232
NSN 6150-01-632-2907
NSN 5975-00-692-9435
NSN 5935-01-009-4051
NSN 6650-01-599-9253
NSN 5960-01-445-3622