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  2. Factory service manual - Wikipedia

    en.wikipedia.org/wiki/Factory_service_manual

    Factory service manuals (FSM) are the manuals provided by manufacturers which cover the servicing, maintenance, and repair of their products. They are not designed for the general public, however they are created by manufacturers for use at their OEM dealerships.

  3. Hartzell Propeller - Wikipedia

    en.wikipedia.org/wiki/Hartzell_Propeller

    Hartzell stopped producing aircraft to avoid competing with its own propeller customers. [9] In 1926, Hartzell began building propellers for the Aeronca C-2. [10] During World War II the company produced metal propellers for Hamilton-Standard. After the war, Hartzell produced the first composite propellers for the Republic RC-3 Seabee. Hartzell ...

  4. CubCrafters CC19 XCub - Wikipedia

    en.wikipedia.org/wiki/CubCrafters_CC19_XCub

    The standard engine available is the 180 hp (134 kW) Lycoming O-360-C1 (CC363i) four-stroke powerplant, driving a Hartzell Trailblazer composite, constant speed propeller. In July 2019 a 215 hp (160 kW) version powered by a Lycoming IO-390 (CC393i) engine and a Hartzell Pathfinder three-bladed propeller was introduced as the CC19-215. [7]

  5. Utva Lasta - Wikipedia

    en.wikipedia.org/wiki/Utva_Lasta

    The LASTA is equipped with a six-cylinder Lycoming engine AEIO-580-B1A 232 kW (315 HP) of the opposed-cylinder type, and a two-bladed metal propeller Hartzell HC-C2YR-4CF/FC 8475-6, which provides maximum flight velocity (at an altitude of 3000m and a takeoff weight of 1085 kg) of 345 km/h. The empty weight is 888 kg, and the maximum takeoff ...

  6. McCulloch J-2 - Wikipedia

    en.wikipedia.org/wiki/McCulloch_J-2

    A later "Super J-2" variant employed a three-bladed Hartzell controllable-pitch propeller, accompanied by an increase in allowable gross weight. Baggage of up to 95 ...

  7. MX Aircraft MXS - Wikipedia

    en.wikipedia.org/wiki/MX_Aircraft_MXS

    Data from MXS Homepage General characteristics Crew: one pilot Capacity: one (pilot only) Length: 6.51 m (21.35 ft) Wingspan: 7.3 m (24 ft) Height: 1.8 m (6 ft) Empty weight: 572 kg (1,260 lb) Gross weight: 726 kg (1,600 lb) Max takeoff weight: 835 kg (1,840 lb) Fuel capacity: 219.55 litre (58 US gal) (optional long range 295.26 litre (78 US gal)) Powerplant: 1 × Lycoming AEIO-540EXP MT ...

  8. Lycoming O-480 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-480

    All engines have an additional prefix preceding the 480 to indicate the specific configuration of the engine. Although the series is known as the "O-480", there are only geared engines in the series.

  9. SIAI-Marchetti FN.333 Riviera - Wikipedia

    en.wikipedia.org/wiki/SIAI-Marchetti_FN.333_Riviera

    The Nardi FN.333 Riviera, later the SIAI-Marchetti FN.333 Riviera, is an Italian luxury touring amphibious aircraft designed and developed by Fratelli Nardi in the 1950s and produced in small numbers by Savoia-Marchetti during the following decade.