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 6320-01-089-9086
NSN 5915-01-208-4774
NSN 5990-01-490-4341
NSN 6620-01-197-7662
NSN 6240-01-153-2861
NSN 5915-01-140-3783
NSN 5935-01-501-4912
NSN 6650-01-495-8031
NSN 5835-00-185-4919
NSN 6645-00-916-5615
NSN 6610-00-711-2551
NSN 6620-00-860-1626