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 5910-01-337-0284
NSN 5998-00-205-8803
NSN 5965-01-532-0628
NSN 6105-01-027-9568
NSN 5920-01-276-6208
NSN 6620-01-336-1473
NSN 2925-00-757-7028
NSN 6105-01-294-6502
NSN 5855-01-258-6180
NSN 4140-01-441-1661
NSN 5950-01-441-3110
NSN 6685-01-316-7227