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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.
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
The Continental O-470 engine is a family of carbureted and fuel-injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed especially for use in light aircraft by 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]
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]
On February 7, 2009, Estes Industries stopped producing Cox engines and sold all of their remaining inventory – mainly spare parts – to several private buyers from Canada and the US. One of the new owners of the remaining Cox engine and parts inventory has launched a website [1] with an online store. After the bankruptcy of Hobbico in 2019 ...
M1 ATC RTF SATCOM (INMARSAT) M2 ATC RTF (MTSAT) M3 ATC RTF (Iridium) N No COM/NAV equipment for the route carried or is unserviceable. O VOR; P1-P9 Reserved for RCP; Q (Not allocated) 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/.)
Hush kits can adversely affect the range and performance of the aircraft they are fitted to because of the extra weight. It also reduces engine performance and aerodynamic efficiency. For example, the hush kit fitted to the Gulfstream II adds 106 kilograms (234 lb) to the total airplane weight of 65,500 lb (29,700 kg), causing around a 1.6% ...
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