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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).
The Cessna 177B Cardinal uses a Lycoming O-360-A1F6D of 180 hp (130 kW). O-360-A1F6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1F6 except that it is equipped with one Bendix D4LN-2021 impulse coupling dual magneto instead of incorporating two single magneto. [1] [2] O-360-A1G
Lycoming O-360 powered production variant. SB7L-360A-2 Lycoming IO-390 210 hp variant [7] SB7L-360A-3 ROAMES Short for Remote Observation Automated Modelling Economic Simulation. Two Lycoming IO-390-A1B6 powered variants built for Ergon Energy featuring upgraded avionics, Garmin G500 EFIS cockpit. The aircraft is capable of fully automated ...
In January 2009 the base price of the IO-390-EXP version was USD$32,650.00. [ 7 ] In November 2009 Lycoming announced that it had obtained an FAA Supplemental Type Certificate to replace the originally fitted Lycoming O-360 engines in the Mooney M20E, M20F and M20J with a new or remanufactured IO-390-A3A6 engine. [ 8 ]
The 200 was quickly replaced by the Lancair 235, equipped with the slightly more powerful Lycoming O-235. Re-engined versions quickly followed; the Lancair 320 with the 150 hp Lycoming O-320, and the Lancair 360 with the 180 hp Lycoming O-360. A new tail was introduced for the later models in order to address stability problems at low speeds ...
Recognizing that the aircraft was underpowered, Cessna introduced the 177A in 1969. The revision featured a 180 hp (135 kW) four-cylinder Lycoming O-360, moving the design's price and role somewhere between that of the 172 and 182. [2] The additional power improved cruise speed by 11 knots (20 km/h). [1] [8] Cessna 177B Cardinal
Replacing the prototype's truss tailboom with a simple aluminum tube as the tailboom, the 269A came with the option for several models of Lycoming O-360 engines: the carbureted O-360-C2D, restricted to 165 hp (123 kW) in the 269A, or the carbureted HO-360-B1A/B1B or fuel-injected HIO-360-B1A/B1B, all rated for 180 hp (134 kW) in the 269A.
The design goals were to produce a simple four-seat aircraft capable of flying cross country flights with full seats. [2] The CH 640 is a four-seat, low-wing touring aircraft with tricycle landing gear and a single engine in tractor configuration. It has a standard empty weight of 1,147 lb (520 kg), a gross weight of 2,200 lb (998 kg) and an ...