Lycoming O-290


The Lycoming O-290 is a dual ignition, four-cylinder, air-cooled, horizontally opposed aircraft engine. It was first run in 1939, and entered production three years later.
A common variant of the type is the O-290-G, a single ignition model which was designed to drive a generator as part of a ground power unit.

Variants

Civil models

;O-290
;O-290-A
;O-290-AP
;O-290-B
;O-290-C
;O-290-CP
;O-290-D
;O-290-D2
;O-290-D2A
;O-290-D2B
;O-290-D2C
;O-290-G

Military models

;O-290-1
;O-290-3
;O-290-11

Applications

Specifications (O-290-D2A)