VS (stall speed): 27 kts | 31 mph | 50 kph
VC (cruise speed): 70 kts | 81 mph | 130 kph
VNE (never exceed speed) : 92 kts | 106 mph | 170 kph
Climb ratio: 1000 ft/min | 5 m/s
Takeoff distance over 50ft (15m) obstacle: 160 ft | 50 m
Landing distance over 50ft (15m) obstacle: 130 ft | 40 m
MEW (manufacturers empty weight): 200 kg | 441 lbs
MTOW (maximum takeoff weight): 450 kg | 992 lbs
Engine: Rotax 503
Fuel consumption: 14 liter by h.
The TwinStar series of two place airplane was introduced in 1984. First came the completely open TwinStar; later the TwinStar was enclosed and named the
TwinStar Mark II.
The TwinStar Mark II featured side by side seating, was enclosed, and had an exceptional climb rate for a two seat aircraft.
Both aircraft are powered by the 503 Rotax engine.