|Weights and dimensions||D2||Most 2 seaters|
|Wing area (sq m)||15,5||11|
|Cabin width (m)||1,46||1,1|
|Empty weight prototype (kg)||275|
|Max. take-off weight (kg)||600|
all at ISA, sea level, with MTOW
|Engine power (HP):||100||80-130|
|Cruise speed @75%P (km/h)||240||160-250|
|Max level speed, full throttle, 5000 rpm (km/h)||260|
|Stall speed (km/h)||85|
|Best climb (at 120 km/h, gear up, MTOW) (fpm)||850|
|Best climb at 500 kg (2 adults, 4 hr fuel) (fpm)||1300||600-1000|
|Best glide angle (at 150 km/h, gear up)||1:10|
|Take off over 50′ obstacle (m)||500|
|Take off run (m)||350|
|Landing distance over 50′ obstacle (m)||450|
|Tank content (ltrs)||140||70|
|Endurance, 30 min reserve (hrs)||8||4|
|Range, no wind, 30 min reserve (km)||1800||700|
The cabin has an even floor.
The wings are foldable.
Engine Rotax 912 ULS,
uses 18 l/hr mogas at cruise speed, 16 l/hr at 220 km/h.
Propeller on prototype Woodcomp VAR-2, variable pitch.
Construction, main structure aluminum 2024, ribs of hard foam.
Landing gear steering monowheel type with rubber compression spring,
tailwheel with shock cord suspension,
tipwheels with metal spring suspension.