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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).
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 ...
Only two Jupiters were built. The first, designated 360-4 and initially registered as F-WLKE had two 200 hp (150 kW) Lycoming IO-360-A1A engines driving two-bladed propellers and was configured as a 4-5 seater. [5] The second prototype was of a more powerful and slightly larger variant designated the model 360-6; it first flew on 25 May 1965. [6]
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
In 1958 the M20A joined the lineup with a larger 180 hp (130 kW) Lycoming O-360-A1A engine, and by 1959, this was the only model offered, with a total sales that year of 231 units. This was the first year the company made a profit.
Scaled up S-1 with tandem two-seat fuselage and powered by a 200 hp (149 kW) Lycoming AEIO-360-B4A piston engine. [15] S-2A Aerotek-built S-2A with a 200 hp (149 kW) Lycoming AEIO-360-A1A or -A1E piston engine, constant speed propeller, later builds have a longer landing gear and a 2-inch-wider (51 mm) front cockpit; 259 built. [15] [19] S-2B
One, sold by the current owner of the Sedan design, replaces many of the components ahead of the firewall with updated versions, including a Lycoming O-360-A1A engine of 180 horsepower (130 kW), a constant speed propeller, a new engine mount, and a fiberglass cowling. A second modification from the design holder allows the removal of the oil ...
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