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  2. Aircraft engine controls - Wikipedia

    en.wikipedia.org/wiki/Aircraft_engine_controls

    For an aircraft equipped with a constant speed propeller, this is the most direct indication of the engine's operating power. A fully open throttle would show a manifold pressure roughly equal to the ambient air pressure, i.e. full power; note that the maximum therefore changes with altitude unless the engine is equipped with a turbocharger or ...

  3. FADEC - Wikipedia

    en.wikipedia.org/wiki/FADEC

    A full authority digital engine (or electronics) control (FADEC) is a system consisting of a digital computer, called an "electronic engine controller" (EEC) or "engine control unit" (ECU), and its related accessories that control all aspects of aircraft engine performance.

  4. Lycoming O-290 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-290

    The Lycoming O-290 is a dual-ignition, four-cylinder, air-cooled, horizontally opposed aircraft engine.It was first run in 1939, and entered production three years later. A common variant of the type is the O-290-G, a single-ignition model which was designed to drive a generator as part of a ground power unit.

  5. Ground support equipment - Wikipedia

    en.wikipedia.org/wiki/Ground_support_equipment

    Ground power unit that needs towing. A ground power unit (GPU) is a vehicle capable of supplying power to aircraft parked on the ground. [2] Ground power units may also be built into the jetway, making it even easier to supply electrical power to aircraft.

  6. MIL-STD-704 - Wikipedia

    en.wikipedia.org/wiki/MIL-STD-704

    MIL-STD-704 Aircraft Electrical Power Characteristics is a United States Military Standard that defines a standardized power interface between a military aircraft and its equipment and carriage stores, covering such topics as voltage, frequency, phase, power factor, ripple, maximum current, electrical noise and abnormal conditions (overvoltage and undervoltage), for both AC and DC systems.

  7. Auxiliary power unit - Wikipedia

    en.wikipedia.org/wiki/Auxiliary_power_unit

    The first German jet engines built during the Second World War used a mechanical APU starting system designed by the German engineer Norbert Riedel.It consisted of a 10 horsepower (7.5 kW) two-stroke flat engine, which for the Junkers Jumo 004 design was hidden in the engine nose cone, essentially functioning as a pioneering example of an auxiliary power unit for starting a jet engine.

  8. List of aviation, avionics, aerospace and aeronautical ...

    en.wikipedia.org/wiki/List_of_aviation,_avionics...

    Ground Power Unit: Aerospace Ground Equipment GPWS ground proximity warning system: Avionics G/S glideslope: Avionics GS groundspeed: GSE ground support equipment: Aerospace ground equipment GSPT Gross shop processing time GSPU Glider snatch pick-up: GUMPS: Gas, Undercarriage, Mixture, Propeller, Seat belts/Switches Mental checklist before landing

  9. Honeywell auxiliary power unit - Wikipedia

    en.wikipedia.org/wiki/Honeywell_auxiliary_power_unit

    A Honeywell GTCP36-150(CX) auxiliary power unit mounted in the tail of a Cessna Model 750 Citation X. Honeywell auxiliary power units are a series of gas turbine auxiliary power units (APU) made by Honeywell Aerospace. Honeywell started manufacturing APUs in the early 1950s and since then they can be found on many aircraft. [1]