Specifications & Performance
| Model | A-22LS |
| Engine | Rotax 912 ULS |
| Power | 100 hp / 73.5 kW at 5800 RPM |
| VNE never-exceed speed | 210 km/h |
| VA manoeuvring speed | 150 km/h |
| VFE maximum flap extended speed | 115 km/h |
| VS1 stall speed, clean configuration | 70 km/h |
| VS0 stall speed in landing configuration | 60 km/h |
| Cruise speed at 4500 RPM | 150 km/h |
| Maximum speed in level flight | 190 km/h |
| Demonstrated crosswind component | 7 m/s |
| Limit load factors | +4 / -2 |
| Take-off run at MTOW & ISA | 105 m |
| Landing roll at MTOW & ISA | 135 m |
| Take-off distance over 15 m obstacle (MTOW & ISA) |
215 m |
| Landing distance from 15 m obstacle (MTOW & ISA) | 350 m |
Certification in Germany
A22-LS (MTOM 600 kg)
DULV - Kennblatt 991-22 1 (Rotax 912 ULS), beinhaltet F-Schlepp bis 700 kg Abflugmasse!
- Details (German) https://www.dulv.de/kennblatt/Dreiachs/991-221.pdf