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  2. 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.

  3. Category:Continental aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Continental...

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  4. Continental O-240 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-240

    The 130 hp (97 kW) O-240 was a new engine design derived from the six-cylinder Continental O-360 and introduced in 1971. It is generally similar in overall dimensions to the Continental O-200, but with a higher 8.5:1 compression ratio, designed to run on 100/130 avgas. The O-240 delivers 30% more power than the O-200 while it weighs only 12% more.

  5. Continental O-300 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-300

    The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines. The GO-300 engine suffered reliability problems as a result of pilots mishandling the engine and operating it at too low an engine rpm. This caused the Cessna Skylark to develop a poor reputation for engine reliability ...

  6. File:Continental O-200-A C150H left 3-quarter above.JPG

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  8. Continental O-280 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-280

    The Continental C115, C125 and C140 aircraft engines were manufactured by Continental Motors in the 1940s, all sharing the US military designation O-280.These engines feature a flat-6 configuration and produce 115 hp (86 kW) 125 hp (93 kW) or 140 hp (104 kW) respectively.

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