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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 ...
Lycoming Engines is a major American manufacturer of aircraft engines. With a factory in Williamsport, Pennsylvania , Lycoming produces a line of horizontally opposed , air-cooled, four, six and eight-cylinder engines including the only FAA -certified aerobatic and helicopter piston engines on the market.
[1] [2] [3] In 1970 a 200 hp (149 kW) fuel injected Lycoming IO-360 engine was fitted and the resulting aircraft was named the Buccaneer. This model replaced both the LA-4 and Seaplane in production and has a higher cruise speed as well as 200 lb (91 kg) increased gross weight.
[2] Velocity SE-RG Retractable landing gear version, 180 completed and flown by December 2011. [2] Rocket Racer The Mark-I X-Racer, a rocketplane design for the Rocket Racing League built on a Velocity SE airframe. It was built by XCOR Aerospace with an XCOR XR-4K14 1,500 lbf (6,700 N) thrust rocket engine fuelled by LOX and kerosene. [4]
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
[1] [2] [5] [6] Engines available as kits from the manufacturer for all models are the Lycoming IO-360 of 180 to 200 hp (134 to 149 kW), Lycoming IO-540 of 260 to 300 hp (194 to 224 kW), Continental IO-550 of 310 to 350 hp (231 to 261 kW) and the Franklin 6A350C1 of 205 to 235 hp (153 to 175 kW).
The type certification for the P.68 Victor, a twin piston engine, high wing monoplane with fixed tricycle landing gear was applied for on 22 January 1969. [2] The Partenavia P.68 was designed as a six-seat light transport and trainer powered by two 200 hp (149 kW) Lycoming IO-360 engines, it made its first flight on 25 May 1970 at Naples. [1]
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