Aircraft Dimensions

Fuselage height 4.4 m – 14.4 ft
Fuselage length 11.8 m – 39.7 ft
Wingspan 14 m – 46 ft
Cabin height (seat to cover) 1.36 m – 4.46 ft
Cabin width 1.48 m – 4.85 ft
Max seating capacity 11 including crew
Fuel tank capacity 800 lt – 212 US Gal

Powerplant

Engine manufacturer Lycoming TEO-540-C1A
Engine power 2 x 375 HP
Time Between Overhaul 2000 hrs
Propellers 2 x 3 blades, constant speed
Fuel consumption 30 US gal/h
Fuel type 100 / 130, 100LL, UL100

Design Weight & Loading

Maximum take-off weight 3600 kg – 7936.64 lb
Std. empty weight 2250 kg – 4960 lb
Useful load 1350 kg – 2976 lb
   

Performance

Vmax 444.48 km/h – 240 kt (8000 ft)
Cruise speed @ 75% power 333.36 km/h – 180 kt 
Stall speed (flaps down, power off)  111     km/h – 60 kts
Pratical ceiling  
Take-off run 350 m – 1148 ft
Take-off distance 600 m – 1968.5 ft
Landing run 250 m – 820 ft
Landing distance 500 m – 1640 ft
Rate of climb 7.62 m/s – 1500 ft/min
Range 1,137 nm  / 6.3 hrs