A-22LS
Two-seat, high-wing aircraft with non-retractable landing gear and steerable nose wheel. The aircraft is designed to fly VFR. The engine is Rotax-912 ULS or Rotax-912 iS with 100 hp. Two versions of the control system – a central stick or two control yokes. A wide range of additional options is available to order – floats installation, including amphibious , a towing hitch, a metal luggage compartment with a side door. Individual dashboard design, possibility of installing equipment of leading manufacturers – Dynon, Garmin, Kanardia. Reliable, safe and time-tested aircraft.
Technical Data & Performance
| Engine | Rotax 912 ULS / Rotax-912 iS |
| Power | 100 HP / 73,5 kW at 5800 RPM |
| VNE never exceed speed | 124 kts |
| Top level speed | 99 kts |
| Cruise speed at 4650 RPM | 81 kts |
| VA max. maneuvering speed | 91 kts |
| VFE max. flap extended speed | 79 kts |
| VS1 stall speed, flaps retracted | 42 kts |
| VS0 stall speed full flaps | 32 kts |
| Fuel consumption at 81 kts (at 4650 RPM) | 4.0 US gph |
| Total fuel capacity (optional tanks) | 24 (30) US gal |
| Range with 2×24 US gal. tanks, 30 min. reserve at 1000 ft, ISA conditions, 4000 RPM (with wheels landing gear) | 529 nm |
| Crosswind limit | 14 kts |
| Max. load factors | 4 / -2 |
| Maximum weight | 1323 lb |
| Empty weight | 639 – 761 lb |
| Take off run at MTOW & ISA | 344 ft |
| Landing run at MTOW & ISA | 607 ft |
| Take off distance over a 50 ft obstacle (MTOW & ISA) | 1099 ft |
| Landing distance from 50 ft obstacle (MTOW & ISA) | 1444 ft |
