O-360, HO-360, IO-360, AIO-360, HIO-360 & TIO-360 Operator's Manual Document Part No. 60297-12 & 60297-12-5
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Continenta Motors Maintenance Manuals. O200 Series Engines Library Contents; X30012 : M-0: X30010: X30011 : A65, A75, C75, C85, C90 and O-200 series Engine Operator's Manual
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the 360 series is a family of air cooled, naturally aspirated, horizontally opposed, 6-cylinder, gasoline, fuel injected, spark ignition, four-stroke, direct drive, right (cw) rotating, aircraft engine with manual engine controls for fixed wing aircraft. certified fuels. 100/100ll avgas minimum and alternative fuels.
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TO FACTORY OR NOT TO FACTORY…THAT IS THE QUESTION. If you’re comparing to factory, consider this… you can get a 3 year, 100% warranty with a Western Skyways Gold Seal engine, but the factory only offers a 1 year warranty.You decide.
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The published Maintenance Manuals, Overhaul Manuals, Operator Manuals and Installation and Operation Manuals for Gasoline Engines are listed the Diesel Engines and here for our Experimental Engine Documentation Electronic copies of Continental Aerospace Technologies technical publications are available for download from the website by subscription To subscribe to the library, you will need …
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Maintenance Manual O-360 and IO-360 Series Engines iv © March 2006 Superior Air Parts Inc. General Information THIS PAGE INTENTIONALLY LEFT BLANK Maintenance Manual O-360 and IO-360 Series Engines v © March 2006 Superior Air Parts Inc. General Information SAFETY ADVISORY
O/IO-360 Series Technical Data Summary Operational Limits Units O-360 IO-360 Max Continuous Speed RPM 2700 Max Continuous Manifold Pressure In-Hg 29.5 Cylinder Head Temperature: Maximum °F 500° Maximum Recommended °F 430° Oil: Maximum Temperature (at engine inlet) °F 240° Minimum Pressure (at idle) psig 20 Minimum Pressure (normal) psig 55
WARNING: OPERATION OF A DEFECTIVE ENGINE WITHOUT A PRELIMINARY EXAMINATION CAN CAUSE FURTHER DAMAGE TO A DISABLED COMPONENT AND POSSIBLE INJURY TO PERSONNEL. MAKE SURE THOROUGH INSPECTION AND TROUBLESHOOTING PROCEDURES ARE ACCOMPLISHED.
Engine rated power at sea level standard day inlet conditions (29.92 in Hg, 59°F, 0 water vapor) with maximum allowable cylinder head and oil temperatures with full rich (maximum) fuel flow. 2. Typical engine weight including all accessories. 3. See Maintenance Manual M-0 for details and applicability.
O-360 & IO-360 SERIES ENGINES INSTALLATION & OPERATION MANUAL 621 South Royal Lane, Suite 100 / Coppell, TX 75019 / 800-277-5168 www.superior-air-parts.com P/N SVIOM01 Revision B, February, 2007 FAA Approved
INSTALLATION & OPERATION MANUAL 621 South Royal Lane, Suite 100 / Coppell, TX 75019 / 800-277-5168 www.superior-air-parts.com P/N SVIOM01 Revision B, February, 2007 FAA Approved Installation & Operation Manual O-360 and IO-360 Series Engines © February 2007 Superior Air Parts Inc.
For a similarly named and broadly similar engine by another manufacturer, see Lycoming O-360. The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010.
The engine is available in both naturally aspirated, fuel injected IO-360 models and turbocharged TSIO-360 versions. It is also available in both left and right hand rotation versions for use on twin-engined aircraft. There was no carbureted version of this engine, which would have been designation O-360, therefore the base model is the IO-360.