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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.
Wings of more than 8 or 9 aspect ratio features other devices to complete the cuff effect, [17] for example stall strips (as used on the Cirrus SR22 and Cessna 400), "Rao slots" (as used on the Questair Venture), vortex generators or segmented droop (as used on a NASA modified Cessna 210). In the case of the high aspect ratio Cessna 210 wing ...
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]
February 26, 1990 KSRQ, Cessna 210, N525CW, Injuries: 1 Serious: The commercial pilot was on initial climb at 200 feet AGL from the Sarasota-Bradenton airport, Sarasota, FL, when the airplane experienced a total loss of engine power. The pilot was on a non scheduled air taxi flight in VFR conditions. No flight plan was filed.
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]
4.3 Performance. 5 See also. 6 References. Toggle the table of contents. Continental O-470. ... Cessna 182 Cessna 185 Cessna 188 Cessna 210 Cessna 310: Produced 1953 ...
R PBN approved (If the letter R is used, the performance based navigation levels that can be met are specified in Item 18 following the indicator PBN/.) S Standard Equipment composed of VHF RTF, VOR and ILS, unless another combination is prescribed by the appropriate ATS authority. T TACAN; U UHF RTF; V VHF RTF; W RVSM approved; X MNPS approved
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.
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