| Flow | S | M | L | |
| 2012 | 2012 | 2012 | ||
| In-Flight-Weight | kg | 60 - 85 | 80 - 105 | 100 - 125 |
| Main-Use | Cross | Cross | Cross | |
| Certifications | ||||
| Naked-Pilot | kg | 43 - 68 | 62 - 87 | 81 - 106 |
| Wing-Load | kg/m² | 2,6 - 3,7 | 3,2 - 4,2 | 3,7 - 4,6 |
| Wing-Weight | kg | 4,5 | 4,9 | 5,3 |
| Area | m² | 23,04 | 25,00 | 27,04 |
| Area proj | m² | 20,52 | 22,27 | 24,09 |
| Span | m | 12,05 | 12,55 | 13,05 |
| Span proj | m | 9,54 | 9,94 | 10,34 |
| Ratio | 6,30 | 6,30 | 6,30 | |
| Ratio proj | 4,68 | 4,68 | 4,68 | |
| Rows | ||||
| Boxes | ||||
| Cells | 50 | 50 | 50 | |
| Closed Cells | ||||
| Lines Ø diam. | ||||
| Lines distance | m | 7,10 | 7,44 | 7,80 |
| Lines total | m | 217 | 235 | 254 |
| Flattening | % | 11 | 11 | 11 |
| Accelerated speed | km/h | 57 | 57 | 57 |
| Basic speed | km/h | 39 | 39 | 39 |
| Minimum speed | ||||
| Best-Sink-Rate | m/s | 1,0 | 1,0 | 1,0 |
| Best-Glide-Ratio | ||||
| GR/Fmax Estimations | p | 10,0 | 10,0 | 10,0 |
| Upper-Surface | ||||
| Under-Surface | ||||
| Lines type | ||||
| Risers | (3A/4B/3C) | (3A/4B/3C) | (3A/4B/3C) | |
| Accelerator | Yes | Yes | Yes | |
| Trims | No | No | No | |
| Ears | Yes | Yes | Yes | |
| B Lines | Yes | Yes | Yes |