| B-Bus | ||
| 2013 | ||
| In-Flight-Weight | kg | 120 - 210 |
| Main-Use | Tandem | |
| Certifications | ||
| Naked-Pilot | kg | 90 - 180 |
| Wing-Load | kg/m² | 2,9 - 5,0 |
| Wing-Weight | kg | 8,9 |
| Area | m² | 41,60 |
| Area proj | m² | 36,09 |
| Span | m | 14,70 |
| Span proj | m | 11,90 |
| Ratio | 5,20 | |
| Ratio proj | 3,90 | |
| Rows | 4 | |
| Boxes | 39 | |
| Cells | 52 | |
| Closed Cells | 6 | |
| Lines Ø diam. | 2,4 mm; 1,8 mm; 1,4 mm; 1,0 mm | |
| Lines distance | m | 9,70 |
| Lines total | ||
| Flattening | % | 13 |
| Accelerated speed | km/h | 50 |
| Basic speed | km/h | 37 |
| Minimum speed | ||
| Best-Sink-Rate | m/s | 1,2 |
| Best-Glide-Ratio | ||
| GR/Fmax Estimations | p | 8,4 |
| Upper-Surface | S9017-E25 38 g/m² | |
| Under-Surface | S9017-E25 38 g/m² | |
| Lines type | Dyneema; Aramide | |
| Risers | 4(3A/4B/3C/2D) | |
| Accelerator | No | |
| Trims | cm | 9 |
| Ears | Yes | |
| B Lines | Yes |