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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. Engines designated "IO" are fuel-injected.
Download QR code; Print/export Download as PDF; Printable version; In other projects ... Continental O-470; Continental IO-520; Continental O-526; R. Continental R ...
The Cessna 188 borrowed heavily from the Cessna 180, the initial version using the same tail cone and fin structure as well as the same Continental O-470-R 230 hp (170 kW) powerplant. The 188's airframe is predominantly built from 2024-T3 aluminum, with the chemical hopper constructed from fiberglass. The fuselage is of semi-monocoque ...
Restored Continental AV1790-5B tank engine at the American Armored Foundation Tank Museum in Danville, Virginia. TD-300 Diesel Engine. In 1929, the company introduced its first aircraft engine, [3] a seven-cylinder radial designated as the A-70, with a displacement of 543.91 cu in (8.91L) that produced 170 hp (127 kW).
Continental O-470-13A air-cooled aircraft engine. A flat-six engine, also known as a horizontally opposed-six, is a six-cylinder piston engine with three cylinders on each side of a central crankshaft. The most common type of flat-six engine is the boxer-six engine, where each pair of opposed cylinders moves inwards and outwards at the same ...
The 1954 model year introduced a 225 hp (168 kW) O-470-J engine and interior refinements. 1956 introduced a 230 hp (172 kW) O-470-K engine with a new air intake duct. Certified on 23 December 1952. 641 (1953), 620 (1954), 891 (1955), and 512 (1956) built. [5] [6] A 1957 Cessna on display at Hullavington Airfield, England. 180A
twin engine conversion Camair 480, 2 Continental O-470-B, 240 hp each. Camair 480C, 2 Continental IO-470- 260 hp each. 25+- built. X-16 Bi-Navion One twin-engined (130hp Lycomings) prototype designed and built by Dauby Equipment Company in 1952, production by Riley and later by Temco. [18] Temco Riley 55
Data from 1956 Observers Book of Aircraft General characteristics Crew: one Capacity: four passengers Length: 27 ft 0 in (8.23 m) Wingspan: 35 ft 0 in (10.67 m) Height: 10 ft 6 in (3.20 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,850 lb (1,293 kg) Gross weight: 4,600 lb (2,087 kg) Fuel capacity: 100 US gal (83 imp gal; 380 L) Powerplant: 2 × Continental O-470-B horizontally opposed ...