| Engine |
Twin TAE Centurion 2.0 Turbo Diesel |
| Horsepower |
270 hp total |
| Propellers |
MT 3-blade composite constant speed, full-feathering |
| Airworthiness category |
Normal |
| Length |
28 ft 1 in |
| Height |
8 ft 2in |
| Wing Span |
44 ft |
| Maximum takeoff weight |
3,935 lbs |
| Useful load |
1,174 lbs |
| Fuel capacity, usable standard |
50 US gal |
| Fuel capacity, usable extended |
72 US gal |
| Fuel |
Jet A-1 |
| Takeoff distance, ground roll* |
1,130 ft |
| Takeoff distance, 50-foot obstacle |
1,730 ft |
| Landing distance, ground roll |
1,069 ft |
| Landing distance, 50-foot obstacle |
1,877 ft |
| Rate of climb, sea level* |
1,280 ft/min |
| Maximum operating altitude |
18,000 ft |
| Maximum SE ceiling (standard day) |
10,000 ft |
| Cruise speed at 80% |
168 kts/12.5 gal/hr total |
| Economy at 60% |
151 ktas/8.8 gal/hr total |
| Stall speed, full flaps gear down |
56 kias |
| Stall speed, clean |
62 kias |
| Maximum landing gear operating speed |
194 kts |
| Maximum demonstrated crosswind |
20 kts |
| Range, at 80% extended fuel |
917 nm |
| Range, at 60% extended fuel |
1,129 nm |