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Same as the IO-360-A1B but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1B6 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1B6 but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1C
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).
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 IO-390 was developed from the similar IO-360 engine, by using cylinders from the IO-580 [citation needed] to increase the O-360's cylinder bore. (Although the IO-390 cylinder assembly [ 4 ] is not the same part number as the IO-580, [ 5 ] the cylinder barrels of both have a 5.318 bore and 4.375 stroke dimension.)
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.
The MFI-15 Safari and MFI-17 Supporter were created from Saab's adaptation of the MFI-9 Junior for basic training for civil and military operators. In 1968 Saab began work on its MFI-15, based on the MFI-9 but with some design changes. Foremost of the changes in the Saab built MFI-15 prototype was the 120 kW (160shp) Lycoming IO-320 piston ...
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
[21] [22] Many light aircraft are powered by versions of these engines, with power ratings in the 100–360 hp (75–270 kW) range. Engines in this series also include the O-235 four-, O-580 six- and O-720 eight-cylinder engines, and the advanced turbocharged and fuel-injected 450 hp (340 kW) TIGO-541 variant of the venerable (carbureted) O-540.