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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...

    Pages in category "Continental aircraft engines" The following 24 pages are in this category, out of 24 total. ... Continental O-200; Continental O-240; Continental O ...

  4. 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 ...

  5. Continental Motors Company - Wikipedia

    en.wikipedia.org/wiki/Continental_Motors_Company

    In 1905, Continental Motors was born with the introduction of a four-cylinder, four stroke cycle L-head engine operated by a single camshaft. In August 1929, the Continental Motors Company formed the Continental Aircraft Engine Company as a subsidiary to develop and produce its aircraft engines. [1] A Continental engine in a 1948 Divco delivery ...

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

    en.wikipedia.org/wiki/File:Continental_O-200-A_C...

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  8. Jodel D.11 - Wikipedia

    en.wikipedia.org/wiki/Jodel_D.11

    Data from Jane's All the World's Aircraft 1958-59 General characteristics Crew: 1 Capacity: 1 passenger or student pilot Length: 6.5 m (21 ft 4 in) Wingspan: 8.22 m (27 ft 0 in) Height: 2.07 m (6 ft 9 in) Wing area: 12.7 m 2 (137 sq ft) Airfoil: NACA 23013.5 Empty weight: 345 kg (761 lb) Gross weight: 600 kg (1,323 lb) Fuel capacity: 116 L (30.6 US gal; 25.5 imp gal) in two tanks Powerplant: 1 ...

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