A-32
Using our long-term design experience, the A32 was designed as a development of the successful A-22LS model with improved aerodynamic and ergonomic characteristics. Classic LSA with a pulling propeller. Powerplant is Rotax-912 ULS 100 hp. Two versions of a control system – the central stick and control yokes. Ergonomic cockpit design performs easy access to the luggage compartment and convenient compartments for storage. Individual dashboard design, possibility of installing of equipment from leading manufacturers – Dynon, Garmin, Kanardia. Combines easy operation with the comfort of a car.
Technical Data & Performance
- Engine Rotax 912 ULS
- Power 100 HP / 73,5 kW at 5800 RPM
- VNE never exceed speed 240 km/h
- Max. horizontal speed 215 km/h
- Cruise speed at 4650 RPM 175 km/h
- VA max. maneuvering speed 151 km/h
- VFE max. flap extended 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 fuel capacity (optional tanks) 90 l (114 l)
- Range with 2×45 l tanks, 30 min. reserve at 1000 ft, ISA conditions, 3700 RPM (with wheels 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 rund at MTOW & ISA 158 m
- Take off distance over a 15 m obstacle (MTOW & ISA) 319 m
- Landing distance from 15 m obstacle (MTOW & ISA) 404 m
Önceki
Sonraki
