Lycoming O-145-B2
The Lycoming Model O-145 engines are four cylinder, horizontally opposed, air-cooled aircraft engines. The A, B, and C series are identical in design with only such changes in construction as to permit the different horsepower ratings. The O-145 is direct drive while the GO-145 has a reduction gearing ratio of 27 to 17. The piston displacement for all models is 144.5 cubic inches. The A series is rated at 50-55 HP at 2300 RPM, the B series at 65 HP at 2550 RPM, and C series at 75 HP at 3100 RPM. The G series is 75 HP at 3200 RPM with a propeller RPM of 2015. The number following the letter denotes the equipment on the engine. 1 is single ignition, 2 is dual ignition, and 3 is dual ignition with generator and starter drives.
Ready to dissamble
Magnetos off
Carburetor and oil sump removed
Top cover and accessory case removed
Cylinder heads removed
Loose valve seat is the reason it wasn’t running right
All the parts cleaned and ready to go back together
Camshaft and crankshaft in place
Crankcase halves bolted together
Bottom side showing the camshaft
Crank and cam gears installed
Back case in stalled
Pistons and connecting rods going together
All the pistons are in and waiting for the top cover
Ready to install cylinder heads
Cylinder head parts
First head installed
All the cylinder heads are on
Valves adjusted, covers and spark plugs installed
Magnetos installed
In the aeroplane and test run