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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 ...
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 ...
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 ]
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
The RV-4 is a new design based upon the concepts proven in the RV-3 and is not merely a stretched RV-3. The RV-4 airframe will accept a range of engines up to 180 hp (134 kW), including the Lycoming O-360. The RV-4 has a new wing, with increased wingspan and wing area over the RV-3. The RV-4 is designed for sport aerobatics.
Later production Seminoles were built with Lycoming O-360-A1H6 engines. [5] The PA-44-180T Turbo Seminole version was certified on November 29, 1979. It features two turbocharged 180 hp (135 kW) Lycoming TO-360-E1A6D engines, which offer a significant improvement in performance at high density altitude. The Turbo Seminole had its takeoff gross ...