| Maximum Static Heaviness/Lightness | | 750/450 lbs. |
| Max. rate of Climb/Descent | | 1600ft/minV |
Two Lycoming IO-360 direct drive, four cylinder, fuel injected, horizontally opposed air cooled engines. The engines are rates t 180 HP at 2700 RPM each at sea level. The propellers are five bladed with constant speed, variable pitch, and fully reversing capability. Propeller diameter is 65 inches.
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