Search results
Results from the WOW.Com Content Network
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] 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] This rocket-powered aircraft flew several demonstration flights at the 2008 EAA AirVenture Oshkosh ...
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
[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 ...
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 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.)
Prototype with a 120 kW (160 hp) Lycoming O-320 engine FA-200-160 Initial version, powered by 120 kW Lycoming O-320 engine and fixed-pitch propeller. FA-200-180 More powerful development - 130 kW (180 hp) Lycoming IO-360 engine and constant speed propeller. FA-200-180AO Powered by 130 kW Lycoming IO-320 engine and fitted with fixed-pitch propeller.