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 5910-01-642-0467
NSN 6145-01-310-9379
NSN 2925-01-364-7926
NSN 4140-01-415-0941
NSN 6150-01-322-1167
NSN 2925-01-510-2221
NSN 5905-01-493-3381
NSN 6145-00-153-2818
NSN 5910-00-071-8122
NSN 5960-01-489-1510
NSN 5990-01-004-6343
NSN 6145-01-318-6720