A22L2 Ultra Light (450kg)
Flight performance at maximum take-off weight
| Max speed Vne | 113 kts |
| Stalling speed (flaps down) | 33 kts |
| Max. range (90 fuel, still air) | 590 nm |
| Max. endurance (90 l fuel) | 10 h |
| Rate of climb (ISA, sea level) | >1000 ft/min |
| Engine: Rotax-912 | 100 h.p. |
| Takeoff/landing run (no wind) | 105/135 m |
| Wing span | 9.55 m |
| Length | 6.23 m |
| Height | 2.4 m |
| Wing area | 12.62 m2 |
| Maximum take-off weight | 450 kg |
| Empty weight | 264 kg |
| Loads | +4 / −2 |
Dimensions – subject to specification (wheel/tyre and propellor type)
