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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.
In the 1930s, Lycoming made a number of attempts to develop successful high-power aircraft engines. The 1 200 hp (895 kW) O-1230 was Lycoming's attempt to produce an engine based on the United States Army Air Corps hyper engine concept, and used a variety of features to produce nearly 1 hp/in 3 (46 kW/L) of engine displacement.
200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1A but with impulse coupling magnetos. [4] IO-360-A1B6 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the A1B but with a crankshaft that has one 6.3 order and one 8th order counterweights.
The Lycoming O-290 is a dual ignition, four-cylinder, air-cooled, horizontally opposed aircraft engine.It was first run in 1939, and entered production three years later. A common variant of the type is the O-290-G, a single ignition model which was designed to drive a generator as part of a ground power unit.
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines. Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
Lancair 200 Model first flown in 1984, powered by a 100 hp (75 kW) Continental O-200 engine. Overall length is 19.75 ft (6.02 m). [3] Lancair 235 Model introduced in 1985, powered by a 100 to 115 hp (75 to 86 kW) Lycoming O-235 engine. Overall length is 20.00 ft (6.10 m), slightly longer than the 200, due to the engine and mount dimensions. [3] [2]
CP-323 – CP-320 with 140–160 hp O-320 Lycoming engine CP-323A – CP-323 with bubble canopy; CP-324 – Emeraude Club with JPX 2100 engine; CP-328A; CP-1310 – Super Emeraude by Scintex with Continental O-200 (23 built) CP-1315 – Super Emeraude with Potez 4E engine (17 built) CP-1320 – Saphir the Super Emeraude with cabin and wings ...
Data from Brassey's World Aircraft & Systems Directory. General characteristics Crew: 2 Length: 24 ft 10 in (7.55 m) Wingspan: 34 ft 9 in (10.69 m) Height: 7 ft 9 in (2.36 m) Wing area: 136 sq ft (12.6 m 2) Airfoil: NACA 23015/23013 (root/tip) Empty weight: 1,750 lb (794 kg) Max takeoff weight: 2,550 lb (1,157 kg) Powerplant: 1 × Textron Lycoming AEIO-540-D 6-cylinder horizontally-opposed ...
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