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  2. Cessna 150 - Wikipedia

    en.wikipedia.org/wiki/Cessna_150

    The Cessna 150 is a two-seat tricycle gear general aviation airplane that was designed for flight training, touring and personal use. [2] In 1977, it was succeeded in production by the Cessna 152, a minor modification to the original design. The Cessna 150 is the fifth most produced aircraft ever, with 23,839 produced. [3]

  3. Continental O-200 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-200

    The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939. [7] [8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special, [9] Aeronca 7AC, [3] and Luscombe 8A. [10] The engine was developed from the earlier O-190 by increasing the stroke 1 ⁄ 4 inch.

  4. List of Cessna models - Wikipedia

    en.wikipedia.org/wiki/List_of_Cessna_models

    Prototype single piston engine monoplane utility airplane Cessna 150: 1957 23,839 Single piston engine monoplane utility airplane Cessna 152: 7,584 Single piston engine monoplane utility airplane Cessna 160: 1962 1 Prototype single piston engine monoplane utility airplane Cessna 162 Skycatcher: 2006 275 Single piston engine monoplane utility ...

  5. Flight envelope - Wikipedia

    en.wikipedia.org/wiki/Flight_envelope

    For instance a Cessna 150 at 2,500-foot (760 m) altitude and 90-mile-per-hour (140 km/h) speed needs about 60 horsepower (45 kW) to fly straight and level. The C150 is normally equipped with a 100-horsepower (75 kW) engine, so in this particular case the plane has 40 horsepower (30 kW) of extra power.

  6. Lycoming O-320 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-320

    150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Provisions for a controllable-pitch propeller and 25-degree spark advance. [2] O-320-A1B 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as A1A but with straight riser in oil sump and -32 carburetor. [4] O-320-A2A

  7. Thrust-to-weight ratio - Wikipedia

    en.wikipedia.org/wiki/Thrust-to-weight_ratio

    where is propulsive efficiency (typically 0.65 for wooden propellers, 0.75 metal fixed pitch and up to 0.85 for constant-speed propellers), hp is the engine's shaft horsepower, and is true airspeed in feet per second, weight is in lbs.

  8. Lycoming O-235 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-235

    A Lycoming O-235-C2C engine mounted in an American Aviation AA-1 Yankee light aircraft. Type Certified piston aero-engine: National origin: United States: Manufacturer Lycoming Engines: First run 1941 Major applications: Cessna 152 Piper Tomahawk Grumman American AA-1 Beechcraft Skipper: Produced 1942–present Developed from: Lycoming O-233 ...

  9. Cessna - Wikipedia

    en.wikipedia.org/wiki/Cessna

    Cessna's first business jet, the Cessna Citation I, performed its maiden flight on September 15, 1969. [20] Cessna produced its 100,000th single-engine airplane in 1975. [21] In 1985, Cessna ceased to be an independent company. It was purchased by General Dynamics Corporation and became a wholly owned subsidiary.