Aeroprakt-32
Drawing on years of experience, the A-32 was designed as a further development of the successful A-22LS with improved aerodynamic and ergonomic properties. The engine of the A-32 is the reliable Rotax-912 ULS 100 hp. The equally powerful Rotax-912 iS injection engine is an option. There are two configurations available for controlling the aircraft; a central Y-stick or double yokes. The ergonomic cockpit design allows easy access to the luggage compartment with convenient compartments for storage. 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 ULSPower: 100 HP/73.5 kW at 5800 RPM
- VNE speed not to be exceeded: 240 km/h
- Max. horizontal speed: 215 km/h
- Cruising speed at 4650 RPM: 175 km/h
- VA max. maneuver speed: 151 km/h
- VFE max. flap speed: 147 km/h
- VS1 stall speed, flaps retracted: 60 km/h
- VS0 stall speed full flaps: 50 km/h
- Fuel consumption at 175 km/h (4650 RPM): 13 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, 3700 RPM (with normal landing gear): 1300 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: 120 m
- Landing run at MTOW & ISA: 158 m
- Take off distance over a 15 m obstacle (MTOW & ISA): 319 m
- Landing distance over a 15 m m obstacle (MTOW & ISA): 404 m
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