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The Continental C90 and O-200 are a family of air-cooled, horizontally opposed, four-cylinder, direct-drive aircraft engines of 201 in 3 (3.29 L) displacement, producing between 90 and 100 horsepower (67 and 75 kW).
The O-200 powered a very important airplane design milestone: the Cessna 150. By the 1960s turbocharging and fuel injection arrived in general aviation and the company's IO-520 series came to dominate the market. [citation needed] In 1965, Ryan Aeronautical acquired a 50% stake in Continental Motors. [10] In 1969, Teledyne Incorporated acquired ...
200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1A but with impulse coupling magnetos. [4] IO-360-A1B6 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1B but with a crankshaft that has one 6.3 order and one 8th order counterweights.
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The most widely produced variant of the Bo 208 is the Bo 208C, which used a Continental O-200-A flat-four-cylinder air-cooled piston engine giving 75 kW (100 HP). A number of O-200 engines installed on Juniors were licence-built by Rolls-Royce in England. A 1966 Bölkow Bo 208C Junior, G-BSME (596), at Rotterdam Airport, The Netherlands
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.
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Continental O-300 engine installation in a Cessna 172. The C-145 was developed from the 125 hp (93 kW) C-125 engine. Both powerplants share the same crankcase, although the C-145 produces an additional 20 hp (15 kW) through a longer piston stroke, higher compression ratio of 7.0:1 and different carburetor jetting.