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The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939. [7] [8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special, [9] Aeronca 7AC, [3] and Luscombe 8A. [10] The engine was developed from the earlier O-190 by increasing the stroke 1 ⁄ 4 inch.
Download as PDF; Printable version; ... Pages in category "Continental aircraft engines" ... Continental O-200; Continental O-240;
Data from Jane's All the World's Aircraft 1958-59 General characteristics Crew: 1 Capacity: 1 passenger or student pilot Length: 6.5 m (21 ft 4 in) Wingspan: 8.22 m (27 ft 0 in) Height: 2.07 m (6 ft 9 in) Wing area: 12.7 m 2 (137 sq ft) Airfoil: NACA 23013.5 Empty weight: 345 kg (761 lb) Gross weight: 600 kg (1,323 lb) Fuel capacity: 116 L (30.6 US gal; 25.5 imp gal) in two tanks Powerplant: 1 ...
The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines. The GO-300 engine suffered reliability problems as a result of pilots mishandling the engine and operating it at too low an engine rpm. This caused the Cessna Skylark to develop a poor reputation for engine reliability ...
The Continental C115, C125 and C140 aircraft engines were manufactured by Continental Motors in the 1940s, all sharing the US military designation O-280.These engines feature a flat-6 configuration and produce 115 hp (86 kW) 125 hp (93 kW) or 140 hp (104 kW) respectively.
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Data from Plane and Pilot General characteristics Crew: one Capacity: one passenger Empty weight: 860 lb (390 kg) Gross weight: 1,500 lb (680 kg) Fuel capacity: 18 U.S. gallons (68 L; 15 imp gal) Powerplant: 1 × Continental C-85 four-cylinder horizontally opposed aircraft engine, 85 hp (63 kW) Propellers: 2-bladed metal Performance Maximum speed: 120 mph (190 km/h, 100 kn) Cruise speed: 110 ...