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 5996-01-201-8260
NSN 4140-01-477-6401
NSN 6240-01-388-2413
NSN 5910-01-367-6155
NSN 6240-01-331-5246
NSN 6320-00-139-1090
NSN 5895-01-377-8201
NSN 6105-01-446-6527
NSN 6645-00-497-3495
NSN 5930-01-259-0211
NSN 4140-01-227-9726
NSN 5985-00-936-3823