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  2. Power transfer unit - Wikipedia

    en.wikipedia.org/wiki/Power_transfer_unit

    Large transport category aircraft with hydraulically powered flight controls and utilities typically have multiple, independent hydraulic systems powered by a combination of engine-driven and electrically driven hydraulic pumps. Multiple hydraulic systems are typically needed for redundancy, where for instance if one system fails or loses ...

  3. Ram air turbine - Wikipedia

    en.wikipedia.org/wiki/Ram_air_turbine

    A ram air turbine (RAT) is a small wind turbine that is connected to a hydraulic pump, or electrical generator, installed in an aircraft and used as a power source. The RAT generates power from the airstream by ram pressure due to the speed of the aircraft. It may be called an air driven generator (ADG) on some aircraft. [1]

  4. Learjet 25 - Wikipedia

    en.wikipedia.org/wiki/Learjet_25

    The landing gear, brake, flap and spoiler systems are hydraulically operated. On aircraft 25-061 through 25-180 the engine driven hydraulic pumps supply fluid under a pressure of 1,500 psi (10.3 MPa). System pressure is maintained at 1,250 to 1,500 psi (8.6 to 10.3 MPa) by a pressure regulator.

  5. Cessna Skymaster - Wikipedia

    en.wikipedia.org/wiki/Cessna_Skymaster

    Introduced for the 1973 model year with a recontoured nose cap, flush wingtip lights, low-drag front exhaust stack and wing strut fairings, a flush-mounted pitot port on the left wing strut, a split airstair door replacing the cabin and baggage doors, aileron gap seals, and a hydraulic powerpack replacing the engine-driven pump. Power was ...

  6. Cessna 170 - Wikipedia

    en.wikipedia.org/wiki/Cessna_170

    Better results were obtained by departing from the Arado jet pump method and using an engine-driven generator to power electric motors driving axial fans to move the internal air. [5] This concept was adopted on the Model 319 but substituted an engine-driven hydraulic pump to drive hydraulic-powered axial fans.

  7. Lycoming O-435 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-435

    Geared engine model which incorporates a dual generator and vacuum pump drive. It produces 260 hp (194 kW) at 3400 rpm for takeoff, with a compression ratio of 7.3:1, a dry weight of 430 lb (195 kg) and fitted with a Marvel MA-4-5 or PS-5BD carburetor. Type certified on February 8, 1955. [1] GO-435-C2B2

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