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The Van's Aircraft RV-8 homebuilt aircraft is often fitted with a 200 hp IO-360 engine. The largest engine that is normally fitted to the Thorp T-18 homebuilt aircraft is the 200 hp IO-360 engine. IO-360-A1A 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1.
The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2. [4] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by 3 ⁄ 16 inch (4.8 mm), developing 210 hp (160 kW).
Powered by a Lycoming 0-360-A1P of 180 hp (134 kW) [5] The A-1B can be modified to accept a Lycoming IO-360-A1D6 engine of 200 hp (149 kW) and an MT MTV-15-B/205-58 propeller under an STC. [6] Husky A-1B-160 Pup Certified on 18 August 2003 without flaps and 21 October 2005 with flaps. Powered by a Lycoming 0-320-D2A, 160 hp (119 kW
S.205 F/R-18: Avco Lycoming O-360 S.205 F/R-20: Avco Lycoming IO-360-A1A S.205 F/R-22: Franklin 6A-350C1 S.206 6-seat version, never realized S.208 5-seat version with a 260 hp engine and a retractable undercarriage S.208M military version for the Italian Air Force S.208AG agricultural version, also used as an aviation-ambulance. S.210 twin ...
Production version with a Lycoming O-360 A1A 180 hp (134 kW), type certified 26 July 1960. This differed from the Colonial C-2 in having four foot greater span, revised nose, doors, higher gross weight and reinforcement of the wing and wing-to-fuselage carry-through structure. [2] [3] LA-4A Shorter bow from the Colonial C-2, only two built.
Lycoming Engines is a major American manufacturer of aircraft engines. With a factory in Williamsport, Pennsylvania , Lycoming produces a line of horizontally opposed , air-cooled, four, six and eight-cylinder engines including the only FAA -certified aerobatic and helicopter piston engines on the market.
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.
A curved vertical stabilizer dorsal fairing is the most noticeable change. It also included a fifth seat, wider chord flaps, and an increased gross weight of 100 pounds. The 1961 Model B95A featured fuel injected Lycoming IO-360-B1A engines.