Continental O-360

__NOTOC__The Continental O-360 is a family of air-cooled, six cylinder aircraft engines which have been manufactured by Continental Motors in the United States of America, now part of the Teledyne corporation, since 1962. [ [http://users.adelphia.net/~aeroengine/Continental2.html Continental, Teledyne Continental Motors, TCM (US);Rolls-Royce (UK); Honda (Japan)Part 2: O-315 through OL-1430] ] It is available in in both normally aspirated, fuel injected (designated IO-360) and turbocharged (designated TSIO-360) versions, and is available with both left and right hand rotation. Taylor 1976, p.792-793] It has been used as the powerplant of a number of aircraft, including the Piper Seneca and Cessna Skymaster.

Engine Specifications

pistonspecs

type=6 cylinder turbocharged horizontally opposed piston engine
bore=4.44 in (11.3 mm)
stroke=3.875 in (9.85 mm)
displacement=360 in³ ( L)
length=57.5 in (146 mm)
diameter=
width=33 in (84 mm)
height=28 in (71 mm)
weight=327.5 lb (149 kg)
valvetrain=
supercharger=
turbocharger=
fuelsystem=
fueltype=
oilsystem=
coolingsystem=
power=220 hp (164 kW) at 2600 rpm
specpower=
compression=7.5:1
fuelcon=
specfuelcon=
oilcon=
power/weight=

References

Notes

Bibliography

*Taylor, J.W.R. (ed.). "Jane's All the World's Aircraft 1976-77". London: Jane's, 1976. ISBN 0 354 00538 3.

External links

* [http://www.tcmlink.com/EngSpecSheetDocs/LTSIO360RB.pdf Engine specification sheet]