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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 ...
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]
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]
Centurion 1.7 installation in a Diamond DA42 Centurion 1.7 (TAE 125-01) The first product introduced by Thielert, a 1689 cm³ (103 in³) engine producing 135 PS (99 kW) is an inline-four engine based on the Mercedes-Benz OM668 from Mercedes-Benz A-Class A 170 CDI (W168) with 80 mm bore and 84 mm stroke.
4.3 Performance. 5 See also. ... Download as PDF; Printable version; ... Cessna 182 Cessna 185 Cessna 188 Cessna 210 Cessna 310: Produced 1953–1986
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 Space Bug engine set the scene for all the Cox engines that followed, and went into full production in 1952. This engine was so popular that it caused problems for other model engine manufacturers. In 1953 Cox produced their first ready to fly (RTF) airplane, the TD1, which was powered by the Space Bug engine.