Specifications

Specification

Aircraft Dimensions

Fuselage Height 4.4 mt – 14.4 ft
Fuselage Length 11.8 mt – 39.7 ft
Wingspan 14 mt – 46 ft
Cabin Height (seat to cover) 1.36 mt – 4.46 ft
Cabin Width 1.48 mt – 4.85 ft
Max Seating capacity 2+9
Fuel tank capacity 800 lt – 212 US Gal

Powerplant

Engine Manufacturer Lycoming TEO-540-C1A
Engine Power 2 x 375 HP
Time Before Overhaul 2000 hrs
Propeller 2 x 3 blades constant speed
Fuel Consumption 30 US Gal/h
Fuel Type 100/130, 100LL and 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
Baggage allowance

Performance

Vmax 444.48 km/h – 240 kts (8000 ft)
Cruise Speed 75% 333.36 km/h – 180 kts (75%, 5000 ft)
Stall Speed (Flaps Down Power Off) 111 km/h – 60 kts
Pratical ceiling
Take off run 350 mt – 1148 ft
Take off distance 600 mt – 1968.5 ft
Landing Run 250 mt – 820 ft
Landing Distance 500 mt – 1640 ft
Rate of climb 7,62 m/s – 1500 ft/min
Range 1.137 nm 6.3 hrs
Flight Rule Commuter