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 6220-00-234-8257
NSN 5975-01-089-9862
NSN 6220-01-618-7446
NSN 6240-01-203-7325
NSN 5920-01-644-0973
NSN 6135-01-048-0910
NSN 6650-01-116-4650
NSN 5999-01-142-0480
NSN 5895-01-091-2646
NSN 2925-01-432-6520
NSN 6645-00-108-6479
NSN 5965-00-937-6482