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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 Piper PA-44 Seminole is fitted with one LO-360-E1A6D or one LO-360-A1H6 on the right wing along with one O-360-E1A6D or O-360-A1H6 on the left wing to eliminate the critical engine on this twin. LO-360-A1G6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1.
Standard engines available are the 180 hp (134 kW) Lycoming O-360-C4P or O-360-C1G and the 180 hp (134 kW) Superior O-360-A3A2 four-stroke powerplants. [1] [3] The aircraft can be flown on wheels, tundra tires, skis or amphibious floats. Belly pods are available to increase cargo and fuel capacity. [1]
The base engine is a Lycoming O-360 180 hp (134 kW) engine, but alternative examples have been built using the Lycoming IO-540, Ranger, Ford V-8 and V-6, Continental, Jacobs, and even Pratt & Whitney R-985 engines. [2]
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 ]
The Aiglon is an all-metal low-wing monoplane with a fixed tricycle landing gear and powered by a nose-mounted 180 hp (134 kW) Lycoming O-360-A3AD or a Lycoming O-360-A3A engine. It was based on the early HR100 but had a lighter airframe and new fin and rudder.
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
Data from www.socata.org SOCATA TB user group and TB21 POH General characteristics Crew: 1 Capacity: 4 passengers Length: 7.75 m (25 ft 5 in) Wingspan: 9.85 m (32 ft 4 in) Height: 2.85 m (9 ft 4 in) Airfoil: RA 16 3C3 Empty weight: 911 kg (2,008 lb) EFIS and MTV 9 propeller Max takeoff weight: 1,400 kg (3,086 lb) Fuel capacity: 336 Liters (88.8 U.S. Gallons) Powerplant: 1 × LYCOMING TIO-540 ...