enow.com Web Search

Search results

1. Results from the WOW.Com Content Network

2. Lycoming O-360 - Wikipedia

   en.wikipedia.org/wiki/Lycoming_O-360

   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).

3. Lake Buccaneer - Wikipedia

   en.wikipedia.org/wiki/Lake_Buccaneer

   [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.

4. Velocity SE - Wikipedia

   en.wikipedia.org/wiki/Velocity_SE

   [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]

5. List of Lycoming O-360 variants - Wikipedia

   en.wikipedia.org/wiki/List_of_Lycoming_O-360...

   [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 ...

6. Giles G-200 - Wikipedia

   en.wikipedia.org/wiki/Giles_G-200

   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).

7. Partenavia P.68 - Wikipedia

   en.wikipedia.org/wiki/Partenavia_P.68

   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]

8. Fuji FA-200 Aero Subaru - Wikipedia

   en.wikipedia.org/wiki/Fuji_FA-200_Aero_Subaru

   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.

9. SIAI-Marchetti S.205 - Wikipedia

   en.wikipedia.org/wiki/SIAI-Marchetti_S.205

   S.205 F/R-18: Avco Lycoming O-360 S.205 F/R-20: Avco Lycoming IO-360-A1A S.205 F/R-22: Franklin 6A-350C1 S.206 6-seat version, never realized S.208 5-seat version with a 260 hp engine and a retractable undercarriage S.208M military version for the Italian Air Force S.208AG agricultural version, also used as an aviation-ambulance. S.210 twin ...