Editing CASA C-212 Aviocar (section)

===300 Series===
Standard production version from 1987 on. Engines were [[Honeywell]] TPE331-10R-513C, also rated at {{convert|900|shp|abbr=on}} continuous (925 shp maximum). The propellers were changed from four-bladed Hartzell composite blade propellers to four-bladed Dowty-Rotol all-metal propellers. [[Wingtip device|Winglets]] and a larger vertical stabilizer area provided improved performance, and the addition of a nose baggage compartment gave the nose a more streamlined look than the 200 series. Various systems were incrementally upgraded, including the addition of an integrated autopilot system.
;C-212-M series 300 (300M series): Military version.
;C-212 series 300 airliner: 26 seat regional airliner.
;C-212 series 300 utility: 23 seat civil utility version.
;C-212 series 300P: Civil utility version with [[Pratt & Whitney Canada|Pratt & Whitney Canada PT6A-65]] engines.