| Gts | 16 | 19 | 22 | |
| 2014 | 2014 | 2014 | ||
| In-Flight-Weight | kg | 50 - 110 | 60 - 130 | 70 - 140 |
| Main-Use | Paramotor | Paramotor | Paramotor | |
| Certifications | ||||
| Naked-Pilot | kg | 33 - 93 | 43 - 113 | 53 - 123 |
| Wing-Load | kg/m² | 3,1 - 6,9 | 3,2 - 6,8 | 3,2 - 6,4 |
| Wing-Weight | ||||
| Area | m² | 16,00 | 19,00 | 22,00 |
| Area proj | ||||
| Span | ||||
| Span proj | ||||
| Ratio | ||||
| Ratio proj | ||||
| Rows | ||||
| Boxes | ||||
| Cells | 54 | 54 | 54 | |
| Closed Cells | 10 | 10 | 10 | |
| Lines Ø diam. | ||||
| Lines distance | ||||
| Lines total | ||||
| Flattening | ||||
| Accelerated speed | 67 km/h; 58 km/h | 67 km/h; 58 km/h | 67 km/h; 58 km/h | |
| Basic speed | km/h | 40 | 40 | 40 |
| Minimum speed | km/h | 25 | 25 | 25 |
| Best-Sink-Rate | ||||
| Best-Glide-Ratio | ||||
| GR/Fmax Estimations | ||||
| Upper-Surface | ||||
| Under-Surface | ||||
| Lines type | ||||
| Risers | ||||
| Accelerator | ||||
| Trims | ||||
| Ears | ||||
| B Lines |