Specifications
| Wing span | 8.44m | 27ft 10in |
| Wing area | 9.8 m2 | 105½ sq ft |
| Aspect ratio | 7.42 |
| Length | 6.19m | 20ft 4in |
| Height | 2.30m | 7ft 6in |
| Cockpit width | 1.12m | 44in |
| Empty weight | 330 kg | 727 lbs |
| Max AUW | 560 kg | 1235 lbs |
| Max luggage | 27 kg | 60 lbs |
| Max payload | 230 kg | 508 lbs |
| Payload (full fuel) | 172 kg | 380 lbs |
| Fuel capacity (useable) | 77 ltrs | 20.3 gal |
| Cruise speed (75%, 18 lt/hr) | 120 kts | 138 mph |
| Cruise speed (55%, 14 lt/hr) | 105 kts | 121 mph |
| Never exceed speed | 164 kts | 188 mph |
| Max rough air speed | 118 kts | 136 mph |
| Stall speed - clean | 44 kts | 50 mph |
| Stall speed - full flap | 39 kts | 45 mph |
| Take-off run | 150m | 490ft |
| Take-off distance (50ft obst) | 287m | 940ft |
| Landing run | 119m | 390ft |
| Landing distance (50ft obst) | 350m | 1150ft |
| Range (75%, no reserves) | 490 nm | 560 sm |
| Range (55%, no reserves) | 570 nm | 660 sm |
| Rate of climb | 247 m/min | 810 ft/min |
| Glide ratio | 1:16 |
| Engine | Rotax 912ULS 100hp with slipper clutch |
| Exhaust system | Stainless steel purpose designed exhaust system |
| Brakes | Hydraulic, adjustable, toe operated disc brakes |
| Flaps | Two position split flaps (15° and 30°) |
| Propeller | Three blade in-flight adjustable pitch propeller (Woodcomp SR3000) |
| Harness | Four position Schroth harness |
| BRS | A Ballistic Rescue System is a popular option |