The aircraft is a four-place, low-wing, single-engine airplane, equipped with tricycle landing gear.
This airplane is certificated in the normal and utility category. See the airplane’s P.O.H. for approved maneuvers. The airplane is approved for day and night VFR operations when equipped in accordance with F.A.R. 91 or F.A.R 135.
The airplane is powered by a horizontally opposed, four cylinder, direct drive, normally aspirated, air cooled, carburetor equipped engine. The engine is a Lycoming Model O-360-A4K and is rated at 180 horsepower.
The fuel system consists of two tanks with a total capacity of 52.6 gallons, of which 51 gallons is usable, two sump tanks, independent fuel gauges, and a fuel selector valve. An auxiliary electric fuel pump supplements engine-driven pump.
The electrical system uses a 24-volt, 70-amp alternator and a battery.