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  2. Continental O-300 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-300

    The GO-300 employs a reduction gearbox, so that the engine turns at 3200 rpm to produce a propeller rpm of 2400. The GO-300 produces 175 hp (130 kW) whereas the ungeared O-300 produces 145 hp (108 kW). [1] The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines.

  3. Category:Continental aircraft engines - Wikipedia

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

    Download as PDF; Printable version; In other projects Wikimedia Commons; ... Continental O-300; Continental O-470; Continental IO-520; Continental O-526; R ...

  4. Continental Aerospace Technologies - Wikipedia

    en.wikipedia.org/wiki/Continental_Aerospace...

    Restored Continental AV1790-5B tank engine at the American Armored Foundation Tank Museum in Danville, Virginia. TD-300 Diesel Engine. In 1929, the company introduced its first aircraft engine, [3] a seven-cylinder radial designated as the A-70, with a displacement of 543.91 cu in (8.91L) that produced 170 hp (127 kW).

  5. Continental O-470 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-470

    The Continental O-470 engine is a family of carbureted and fuel-injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed especially for use in light aircraft by Continental Motors. Engines designated "IO" are fuel-injected.

  6. Continental IO-550 - Wikipedia

    en.wikipedia.org/wiki/Continental_IO-550

    The Continental IO-550 engine is a large family of 9 liter fuel injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in light aircraft by Teledyne Continental Motors. The first IO-550 was delivered in 1983 and the type remains in production.

  7. Continental IO-360 - Wikipedia

    en.wikipedia.org/wiki/Continental_IO-360

    Rolls-Royce Continental IO-360-D Licence production in the United Kingdom by Rolls-Royce IO-360-DB 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper. [4] IO-360-E

  8. Cessna 350 Corvalis - Wikipedia

    en.wikipedia.org/wiki/Cessna_350_Corvalis

    It was certified on March 30, 2003 as the Model LC42-550FG (for Lancair Certified, Model 42, Continental 550 engine, Fixed Gear) and marketed as the Columbia 350. [4] Like the 300, the 350 is powered by a Teledyne Continental IO-550-N powerplant producing 310 horsepower (230 kW) at 2700 rpm. The 350 has the same takeoff and landing weights as ...

  9. Continental IO-520 - Wikipedia

    en.wikipedia.org/wiki/Continental_IO-520

    The Continental IO-520 is a six-cylinder, horizontally opposed aircraft engine produced by Teledyne Continental Motors. First run in 1963 as a development of the IO-346 , it has been produced in versions incorporating fuel injection ( IO-520 ), turbo-charging ( TSIO-520 ), and gearing ( GTSIO-520 ).