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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).
[2] [4] IO-360-B1C 177 hp (132 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the HIO-360-B1B externally but with a crankcase machined for No. 1 Dynafocal mounts. [2] [4] IO-360-B1D 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the B1B but with an AN fuel pump ...
[2] [3] LA-4S Seaplane Version without wheeled landing gear, produced 1969-72 under STC SA781EA approved 8 July 1969 and amended 28 November 1969, issued to Revo, Inc. [2] [3] LA-4T Turbocharged version with 180 hp (134 kW) Lycoming O-360 A1D engine and Rayjay turbocharger. Not produced. [2] LA-4-200 Buccaneer Lycoming IO-360 A1B 200 hp (149 kW ...
Initial production version with a 200hp (149kW) Lycoming IO-360 engine. HR.100/210 Safari Production version with a 210hp (157kW) engine, 113 built of both 200B Royal and 210 Safari variants. HR.100/235TR Experimental HR.100 with an enlarged tail and retractable landing gear and a 235hp Lycoming O-540-B engine, one built. HR.100/250TR
The DA40 was initially marketed as the DA40-180, powered by a fuel injected Textron Lycoming IO-360 M1A engine. [3] [4] The DA40-XL has a constant speed propeller and is powered by a 180 hp (130 kW) Lycoming IO-360-M1A fuel injected engine. It has a maximum cruise speed of 147 kn (272 km/h; 169 mph), burning 9.2 gallons of Avgas per hour.
The G-200's acceptable installed power range is 150 to 220 hp (112 to 164 kW) and the standard engine used is the 200 hp (149 kW) Lycoming IO-360 powerplant. [ 2 ] [ 4 ] The G-200 has an empty weight of 750 lb (340 kg) and a gross weight of 1,150 lb (520 kg), giving a useful load of 400 lb (180 kg).
The Lancair 360 is a two-seat aircraft marketed in kit form. It is a low-wing monoplane of conventional configuration with retractable tricycle undercarriage. The Lancair Legacy was chosen to replace the Lancair 360 in 1999. [1] Lancair 360 MKII A Lancair 360 at Peachtree-Dekalb Regional Airport.
Height: 6 ft 2 in (1.88 m) Wing area: 81.3 sq ft (7.55 m 2) Empty weight: 1,368 lb (621 kg) Gross weight: 2,200 lb (998 kg) Fuel capacity: 61.4 US gallons (232 litres) Powerplant: 1 × Lycoming IO-360 A1B four cylinder, horizontally opposed, four stroke aircraft engine, 200 hp (150 kW) Propellers: 3-bladed Hoffmann VP with wood blades; Performance