ConFIGURATION

Two-seat, tandem arrangement, low-wing aerobatic monoplane with

conventional (taildragger) landing gear.

AIRframe

Fuselage Assembly, 4130 Steel

Carbon Fiber Wing Assembly with integral Tank

Carbon / Glass Hybrid Composite Empennage Structure

Fiberglass Landing Gear Spring

Choice of Steerable, lightweight Tailwheel or Soft Tailwheel

Two-seat Bubble Canopy

SYSTEMS

Electric Stall Warning System

Pitot Static System Drain

40 Amp Alternator

12 V Battery

Trickle Charger Socket

Strobe / Navigation Lights at Wing Tips

Alternate Static Port

Glider Air Tow System

External Power Receptacle AN2552-compatible

POWERPLANT AND PROPELLER

Lycoming AEIO-360 A1E, 200 hp 4-cylinder Engine

Gomolzig, 4 in 1 Exhaust System

Muehlbauer, MTV 12-B-C / C183-17e, 3-blade Propeller

Electric Starter

Two Fuel Pumps (1 engine-driven, 1 electric)

Lycoming-recommended Cold Weather Kit

COCKPIT

Fixed Composite Front Seat, Contour Molded

Adjustable Composite Rear Seat, Contour Molded

Forward Rudder Pedals with differential Toe Brakes

Manually Adjustable Rear Rudder Pedals with differential Toe Brakes

Front and Rear Seat Hooker Safety Harness with Ratchet

2 Front and 2 Rear Bezel-operated Air Vents

Leather Seat Upholstery front and rear

Rear Airframe Lexane Tray

EQUIPMENT

Polyurethane Wing Walk Protection

Polyurethane Elevator Protection

Left-hand and Right-hand Sighting Devices 45°/ 90°

FRONT PANEL INSTRUMENTATION

Airspeed Indicator

Altimeter

Metric Airspeed and Altimeter

Slip and Skid Indicator upright and/or inverted flight