Crew: 1 or 2

Capacity: 11 seats / 1,414 kg (3,117 lb) useful load including fuel

Length: 11.8 m (38 ft 9 in)

Wingspan: 14 m (45 ft 11 in) ; 16.6 m (54 ft) on STOL variant

Height: 4.4 m (14 ft 5 in)

Wing area: 25.4[35] m2 (273 sq ft)

Aspect ratio: 7.7

Empty weight: 2,386 kg (5,260 lb) ; 2,416 kg (5,326 lb) on STOL variant

Max takeoff weight: 3,680 kg (8,113 lb)

Fuel capacity: 750 L (200 US gal) usable fuel

Powerplant: 2 × Lycoming TEO-540C1A 6-cylinder air-cooled horizontally-opposed turbocharged piston engines, 280 kW (375 hp) each

Powerplant: 2 × Continental GTSIO-520-S 6-cylinder horizontally-opposed turbocharged, geared piston engines, 280 kW (375 hp) each

Propellers: 3 or 4-bladed MT-Propeller, 1.95 m (6 ft 5 in) diameter constant-speed fully-feathering propeller

Performance

Maximum speed: 359 km/h (223 mph, 194 kn) at 10,000 ft (3,000 m)

Cruise speed: 319 km/h (198 mph, 172 kn) at 75% power at 10,000 ft (3,000 m)

Stall speed: 120 km/h (75 mph, 65 kn) full flaps; 122 km/h (76 mph; 66 kn) full flaps on STOL variant

Never exceed speed: 400 km/h (250 mph, 220 kn)

Range: 1,760 km (1,090 mi, 950 nmi)

Service ceiling: 5,900 m (19,500 ft) restricted to four passengers over 4,000 m (13,000 ft) [35]

Rate of climb: 5.8 m/s (1,140 ft/min) ; 6.53 m/s (1,285 ft/min) on STOL variant

Wing loading: 145 kg/m2 (30 lb/sq ft)

Power/mass: 6.6 kg/kW (10.8 lb/hp)

Takeoff run: 564 m (1,850 ft); 445 m (1,460 ft) on STOL variant

Takeoff distance: 791 m (2,595 ft); 682 m (2,238 ft) on STOL variant

Landing run: 365 m (1,198 ft); 290 m (950 ft) on STOL variant

Landing distance: 743 m (2,438 ft); 590 m (1,940 ft) on STOL variant

Fuel Consumption: 117 L/h (31 US gal/h)