Aeroprakt-22LS
The A-22LS is a robust two-seater high-decker with fixed landing gear. The engine is either a Rotax-912 ULS or Rotax-912 iS injection engine, both with 100 hp. In terms of control, you can choose from a central Y-stick or double yokes. There is a wide range of additional options available to order, such as a metal luggage compartment with a side door. You can arrange the panel as you wish with avionics from leading manufacturers such as Dynon, Garmin and Kanardia.
Technical data and performance
- Engine: Rotax 912 ULS
- Power: 100 HP/73.5 kW at 5800 RPM
- VNE speed not to be exceeded: 230 km/h
- Max. horizontal speed: 183 km/h
- Cruising speed at 4650 RPM: 150 km/h
- VA max. maneuver speed: 168 km/h
- VFE max. flap speed: 147 km/h
- VS1 stall speed, flaps retracted: 77 km/h
- VS0 stall speed full flaps: 60 km/h
- Fuel consumption at 150 km/h (4650 RPM): 15 l/h
- Total tank capacity (optional tanks): 90 l (114 l)
- Range with 2×45 l tanks, 30 min. reserve at 1000 ft, ISA conditions, 4000 RPM (with normal landing gear): 980 km
- Crosswind limit: 7 m/s
- Max. load factors: 4/-2
- Maximum weight: 600 kg
- Empty weight: 290–345 kg
- Take off run at MTOW & ISA: 105 m
- Landing run at MTOW & ISA: 185 m
- Take off distance over a 15 m obstacle (MTOW & ISA): 335 m
- Landing distance over a 15 m m obstacle (MTOW & ISA): 440 m
Curious about the Aeroprakt-22LS? Contact us, we are happy to help you! Also view the Aeroprakt-32
