| Engine: | Pratt & Whitney PT6A-64 turbine with 1,570 shp., flat-rated to 700 shp. |
| Propeller: | Hartzell, metal, four-blade, constant-speed, full-feathering, reversible, 91 in. diameter. |
| Maximum ramp weight: | 6,614 lbs. |
| Useful load: | 2,367 lbs. |
| Maximum useable fuel: | 281.62 gals. or 1,886.85 lbs. |
| Payload with full tanks: | 480 lbs. |
| Certified ceiling: | 30,000 ft. The cabin will be at 8,850 ft., since the maximum pressure differential is 6.2 psi. |
| Maximum cruising speed: | 300 kts. with a fuel flow of 55 gph. |
| Seating: | six seats, with an optional seventh seat. |