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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 Cessna 177B Cardinal uses a Lycoming O-360-A1F6D of 180 hp (130 kW). O-360-A1F6D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the A1F6 except that it is equipped with one Bendix D4LN-2021 impulse coupling dual magneto instead of incorporating two single magneto. [1] [2] O-360-A1G
In the 1930s, Lycoming made a number of attempts to develop successful high-power aircraft engines. The 1 200 hp (895 kW) O-1230 was Lycoming's attempt to produce an engine based on the United States Army Air Corps hyper engine concept, and used a variety of features to produce nearly 1 hp/in 3 (46 kW/L) of engine displacement.
Replacing the prototype's truss tailboom with a simple aluminum tube as the tailboom, the 269A came with the option for several models of Lycoming O-360 engines: the carbureted O-360-C2D, restricted to 165 hp (123 kW) in the 269A, or the carbureted HO-360-B1A/B1B or fuel-injected HIO-360-B1A/B1B, all rated for 180 hp (134 kW) in the 269A.
List of Lycoming O-360 variants; Lycoming O-435; Lycoming O-480; Lycoming O-540; Lycoming O-1230; R. Lycoming R-680; Lycoming XR-7755; T. Lycoming T53; Honeywell T55;
Data from Aviat website General characteristics Crew: one Capacity: one passenger Length: 22 ft 7 in (6.88 m) Wingspan: 35 ft 6 in (10.82 m) Wing area: 183 sq ft (17.0 m 2) Empty weight: 1,275 lb (578 kg) on wheels Gross weight: 2,200 lb (998 kg) on wheels and floats Fuel capacity: 50 US gallons (190 litres) Powerplant: 1 × Lycoming O-360-A1P four cylinder, four stroke piston aircraft engine ...
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 ...
The Auster D.6 was a four-seat British light aircraft, a development of the Auster Autocar with a horizontally opposed engine. It was available with a choice of two engines, a 160 hp Lycoming O-320 or 180 hp Lycoming O-360.
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