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 5965-00-142-9052
NSN 5925-01-376-7569
NSN 5895-01-089-9999
NSN 2925-00-355-5130
NSN 5930-00-965-9294
NSN 4140-00-375-9705
NSN 2925-01-577-9269
NSN 5996-01-043-2105
NSN 6610-01-198-3862
NSN 6110-00-727-6992
NSN 6135-00-299-6918
NSN 5945-00-925-1909