The gea 71 engine/airframe unit is main processor for all engine instrumentation data, including manifold pressure, engine speed (rpm), oil temperature/pressure, electrical system parameters, exhaust gas temperature (egt), cylinder head temperature (cht), fuel and vacuum system parameters, depending upon the aircraft
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 6645-01-286-9872
NSN 5855-01-440-8978
NSN 6610-01-533-7458
NSN 5998-00-001-9703
NSN 2925-00-221-4977
NSN 5835-01-074-7593
NSN 6645-00-519-1026
NSN 6145-01-061-3058
NSN 5835-01-251-7301
NSN 5915-00-099-0347
NSN 6645-01-500-0827
NSN 6150-01-033-4786