Whole Plan Recovery: Installed GRS wholeplane ballastic parachute.
Fuselage: Carbon tube space frame, CFRP-Kevlar-hybrid safety cell and seat, seat position and tilt angle fully ground adjustable, sliding canopy, Oratex cover.
Wing: CFRP spars and ribs, sandwich torsion box, combined flaps and ailerons (flaperons), tie-down-cutouts optional, Oratex cover.
Empennage: CFRP structure, rudder aerodynamically balanced, elevator aerodynamically and mass balanced.
Landing Gear: Two cantilevered main wheels 400-4 with spring and damper units, aerodynamic aluminum profile struts, drum brakes with separate actuation, steerable tail wheel with elastomeric spring/damper.
Controls: Flaperon and elevator control by pushrods, adjustable control stick, rudder control by steel cables, rudder pedals adjustable.
Propulsion: 3-cylinder radial engine Verner Scarlett, including electric start, generator, 2-blade ground adjustable CFRP-prop, aluminum-spinner, 5 gallon fuel tank.
Avionics/Electronics: GFRP panel with altimeter, airspeed indicator, bank indicator, compass, oil pressure, oil temperature, tachometer, 12V and USB sockets, aircraft grade wiring, automatic circuit breakers, LiFePo-battery.