Continental O-170

The Continental O-170 engine is the collective military designation for a family of small aircraft engines, known under the company designation of A50, A65, A75 and A80. The line was designed and built by Continental Motors commencing in the 1940s. It was employed as the powerplant for civil and military light aircraft.

The horizontally opposed, four-cylinder engines in this family are all identical in appearance, bore, stroke, dry weight, and piston displacement. All feature a bottom-mounted updraft carburetor fuel delivery system. The higher power variants differ only in compression ratio and maximum allowable rpm, plus minor modifications. The lower power versions are fully convertible to the higher rated versions.

;A65-1:

;A65-2:

;A65-3:

;A65-4:

;A65-5:

;A65-6:

;A65-7:

;A65-8:

;A65-8F:

:A65-9:

;A65-12:

;A75

:, Compression ratio 6.3:1, max rpm 2,600, fuel consumption at cruise 4.8 US gph. The exhaust valves have stellite faces and the connecting rods have a hole drilled in the rod cap to improve lubrication. The pistons have three rings and smaller piston pins.

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