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 5935-01-431-7503
NSN 5950-00-518-2162
NSN 6145-00-437-8960
NSN 5945-01-194-7541
NSN 6130-01-516-4519
NSN 6220-01-524-0285
NSN 5910-01-237-3725
NSN 5935-01-223-9060
NSN 6110-01-467-9074
NSN 5960-01-243-0007
NSN 6105-01-248-0195
NSN 5935-01-578-2356