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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 plane was built from plans that cost $145. [4] Variants. Some versions were built using 125 hp (93 kW) Lycoming O-235 and ... 1 × Continental O-200-A air ...
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 ...
The aircraft was intended to be offered with a variety of new or rebuilt engines. Rebuilt engines were to be available to reduce the purchase price. Design powerplants included the Continental A65-8 of 65 hp (48 kW), Continental C90-14F of 90 hp (67 kW), Continental O-200 A of 100 hp (75 kW) and a Lycoming O-235 C1 of 108 hp (81 kW).
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.
Data from Company website, AeroCrafter & Kitplanes General characteristics Crew: one Capacity: one passenger and 630 lb (285 kg) useful load Length: 17 ft 6 in (5.33 m) Wingspan: 22 ft 0 in (6.71 m) Height: 6 ft 0 in (1.83 m) Wing area: 176 sq ft (16.37 m 2) Empty weight: 600 lb (272 kg) Max takeoff weight: 1,230 lb (557 kg) Powerplant: 1 × Continental O-200 Four cylinder, four-stroke piston ...
Data from Jane's All the World's Aircraft 1982–83 General characteristics Crew: 1 pilot Capacity: 1 passenger Length: 18 ft 0 in (5.49 m) Wingspan: 25 ft 0 in (7.62 m) Height: 8 ft 0 in (2.44 m) Wing area: 105.0 sq ft (9.75 m 2) Empty weight: 733 lb (332 kg) Max takeoff weight: 1,270 lb (576 kg) Fuel capacity: 23 US gal (19 imp gal; 87 L) Powerplant: 1 × Continental O-200 -A air-cooled flat ...
In 1967 the aircraft were modified by adding a Continental O-200 engine, V-Belt RPM reduction system, four-bladed Fahlin fixed pitch wooden propeller, and associated airframe upgrades. After demonstrating quiet flight, [ 1 ] the aircraft were again modified to military QT-2PC configuration, known only as Tail Numbers "1" and "2", with avionics ...
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