A-22LS
Two-seat aircraft, high-wing airplane with non-retractable gear legs and nose support. The aircraft is designed to perform visual flights in simple weather conditions. Powerplant is Rotax-912 ULS / Rotax-912 iS with 100 hp. Two versions of a control system – the central stick and control yokes. A wide range of additional options is available to order – floats installation, including amphibious , a towing clutch, a metal luggage compartment with a side door. Individual dashboard design, possibility of installing of equipment from leading manufacturers – Dynon, Garmin, Kanardia. Reliable, safe and time-tested aircraft.
Technical Data & Performance
- Engine Rotax 912 ULS
- Power 100 HP / 73,5 kW at 5800 RPM
- VNE never exceed speed 230 km/h
- Max. horizontal speed 183 km/h
- Cruise speed at 4650 RPM 150 km/h
- VA max. maneuvering speed 168 km/h
- VFE max. flap extended 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 fuel capacity (optional tanks) 90 l (114 l)
- Range with 2×45 l tanks, 30 min. reserve at 1000 ft, ISA conditions, 4000 RPM (with wheels 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 rund at MTOW & ISA 185 m
- Take off distance over a 15 m obstacle (MTOW & ISA) 335 m
- Landing distance from 15 m obstacle (MTOW & ISA) 440 m
Önceki
Sonraki
