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The early Cessna 210 (210 and 210A) had four seats with a Continental IO-470 engine of 260 hp (190 kW). It was essentially a Cessna 182B to which was added a retractable landing gear, swept tail, and a new wing. [2] In 1961, the fuselage and wing were completely redesigned: the fuselage was made wider and deeper, and a third side window was added.
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]
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Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 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
Cessna 210 Centurion four- to six-seat light aircraft; Cessna T303 Crusader six-seat corporate and utility transport; Cessna 310 four- to six-seat light piston twin; Cessna 320 Skyknight four- to six-seat light piston twin; Cessna 336 & 337 Skymaster six-seat light piston twins; Cessna 335 & 340 six-seat twin-engine airliner; Cessna 350 & 400 ...
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]
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
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