I pulled the spec (below) on a Lycoming 0-360J2A, horizontal helicopter engine...R22
Q- what are the prop flange bushings? something to worry about?
Q-can I put a std. Aluminum propeller on this crankshaft?
Q-why is the engine rated 145 hp at 2400 to 2700+RPM?
Q-what caused the de-rating, camshaft?
thanks
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O-360-J2A Similar to the O-360-C1C except has O-320-B2C prop flange bushings, light weight cylinders and lower power rating.
O-360-C1C Similar to O-360-C1A except has Bendix 200 series magnetos.
O-360-C1A Similar to O-360-A1A except has crankcase machined for conical rubber mount bushings in place of dynafocal mountings.
O-360-A1A Basic Model. Four cylinder, horizontally opposed, air cooled, direct drive engine with provisions for supplying oil through propeller shaft for a single acting controllable pitch propeller.
O-360-B2C Similar to O-360-B2A except has heavier IO-360-A crankshaft and rods.
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