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 6320-00-521-9248
NSN 6685-01-137-5710
NSN 5835-01-242-9806
NSN 6105-00-613-8638
NSN 5920-01-347-5852
NSN 5965-00-594-3115
NSN 6685-00-978-8608
NSN 2925-01-633-4048
NSN 6685-01-585-8073
NSN 5835-01-013-9321
NSN 5990-01-282-4617
NSN 6130-01-516-1752