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Data from Janes' All The World's Aircraft 1982-83 General characteristics Crew: One Capacity: Five passengers Length: 28 ft 2 in (8.59 m) Wingspan: 36 ft 9 in (11.20 m) Height: 9 ft 8 in (2.95 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,303 lb (1,045 kg) Gross weight: 4,000 lb (1,814 kg) Fuel capacity: 87 US gal (72 imp gal; 330 L) (usable capacity) Powerplant: 1 × Continental Motors ...
Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1 Single piston engine monoplane racer Cessna CR-3: 1933 1 Single piston engine monoplane racer Cessna CW-6: 1928 Single piston engine monoplane utility airplane Cessna C-34 Airmaster ...
The first engine in this series was the E165, a 471 cubic inch (7.7 L) engine producing 165 hp (123 kW), and was the first of the Continental's "E" series engines. Later versions were given the company designation of E185 (185 hp (138 kW) continuous) and E225 (225 hp (168 kW)).
The IO-520 series engines normally produce 285 to 310 horsepower (210 to 230 kW) and are used in numerous aircraft such as certain models of the Bellanca Viking 300 and Super Viking, the Beech Bonanza and Baron, and Cessna 185- 206-, 210-, 310-, and 400-series aircraft. The IO-520 remained in production in 2019. [1]
The SMA SR305-230 is an air/oil-cooled, horizontally opposed, four-cylinder, four-stroke, diesel piston aircraft engine producing 170 kW (227 hp). The engine is manufactured by SMA Engines, and is currently the only product of this French company. The engine is offered as a conversion package for the Cessna 182.
Work on a potential replacement for the Cessna 195 began in 1949. The resulting in the Model X210 was similar to the 195, sharing the latter's basic design and conventional landing gear configuration, but was powered by a 240 hp (179 kW) Continental O-470 flat-six engine mounted on a redesigned forward fuselage. [2]
The Continental R-670 (factory designation W670) was a seven-cylinder four-stroke radial aircraft engine produced by Continental displacing 668 cubic inches (11 litres) and a dry weight of 465 lb (211 kg). Horsepower varied from 210 to 240 at 2,200 rpm. The engine was the successor to Continental's first radial engine, the 170 hp Continental A ...
The controversial Continental GO-300 engine from the civil 175 was never used in the T-41; the T-41B through D instead used the Continental IO-360. Cessna never offered a civil model directly analogous to these aircraft, but Cessna licensee Reims Aviation in France sold similar IO-360-powered models as the R172 Rocket and Hawk XP. [10] T-41A