| Falcon 2009 | 24 | 26 | 27 | 29 | |
| 2009 | 2009 | 2009 | 2009 | ||
| In-Flight-Weight | kg | 70 - 90 | 80 - 100 | 90 - 110 | 100 - 125 |
| Main-Use | Leisure | Leisure | Leisure | Leisure | |
| Certifications | ; | ; | ; | ; | |
| Naked-Pilot | kg | 63 | 72 | 81 | 93 |
| Wing-Load | kg/m² | 3,3 | 3,5 | 3,6 | 3,9 |
| Wing-Weight | kg | 5,8 | 6,0 | 6,4 | 6,8 |
| Area | m² | 24,49 | 26,08 | 27,59 | 28,99 |
| Area proj | m² | 21,96 | 23,39 | 24,74 | 25,99 |
| Span | m | 11,31 | 11,67 | 12,00 | 12,30 |
| Span proj | m | 9,61 | 9,92 | 10,21 | 10,47 |
| Ratio | 5,22 | 5,22 | 5,22 | 5,22 | |
| Ratio proj | 4,21 | 4,21 | 4,21 | 4,21 | |
| Rows | 4 | 4 | 4 | 4 | |
| Boxes | 25 | 25 | 25 | 25 | |
| Cells | 52 | 52 | 52 | 52 | |
| Closed Cells | 14 | 14 | 14 | 14 | |
| Lines Ø diam. | 1,7 mm; 1,1 mm | 1,7 mm; 1,1 mm | 1,7 mm; 1,1 mm | 1,7 mm; 1,1 mm | |
| Lines distance | m | 6,27 | 6,47 | 7,44 | |
| Lines total | |||||
| Flattening | % | 10 | 10 | 10 | 10 |
| Accelerated speed | km/h | 50 | 50 | 50 | 50 |
| Basic speed | km/h | 38 | 38 | 38 | 38 |
| Minimum speed | km/h | 23 | 23 | 23 | 23 |
| Best-Sink-Rate | m/s | 1,1 | 1,1 | 1,1 | 1,1 |
| Best-Glide-Ratio | |||||
| GR/Fmax Estimations | |||||
| Upper-Surface | Skali-0904 42 g/m² | Skali-0904 42 g/m² | Skali-0904 42 g/m² | Skali-0904 42 g/m² | |
| Under-Surface | Skali-0904 42 g/m² | Skali-0904 42 g/m² | Skali-0904 42 g/m² | Skali-0904 42 g/m² | |
| Lines type | Aramid; Dyneema | Aramid; Dyneema | Aramid; Dyneema | Aramid; Dyneema | |
| Risers | 5(2A+1A'/3B/4C/2D) | 5(2A+1A'/3B/4C/2D) | 5(2A+1A'/3B/4C/2D) | 5(2A+1A'/3B/4C/2D) | |
| Accelerator | cm | 14 | 14 | 14 | 14 |
| Trims | No | No | No | No | |
| Ears | Yes | Yes | Yes | Yes | |
| B Lines | Yes | Yes | Yes | Yes |