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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