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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).
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]
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.
Maximum gross weight is 1,890 lb (857 kg). Powered by a Lycoming 0-360-A1P of 180 hp (134 kW) [5] Aviat A-1C Husky Husky A-1B Certified on 28 January 1998. 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]
Same as IO-360-A except for reduced compression ratio and rated power. The crankshaft has two 6th order dampers. [4] IO-360-C 210 hp (157 kW) at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for accessory drive provisions. The crankshaft has two 6th order ...
The current engine is a Lycoming IO-360-A1B6, giving the Fury a max speed of 222 mph. The aircraft will carry two adults with up to 100 pounds of baggage and has a range of 1000 miles. The aircraft will carry two adults with up to 100 pounds of baggage and has a range of 1000 miles.