Power Plant
| Engine | 2x Austro Engine AE330 turbocharged common-rail injected 2.0 liter jet fuel engine with 180 HP and EECU single lever control system |
|---|---|
| Propeller | 2x MT propeller MTV-6-R-C-F/CF 194-80 3-blade constant speed propeller |
| Fuel grades | Jet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8 |
Performance (MTOM, ISA)
| Max. speed (14,000 ft, MCP) | 356 km/h TAS | 192 kts TAS |
|---|---|---|
| Cruise Speed at 85 % (12,000 ft) | 333 km/h TAS | 180 kts TAS |
| Stalling speed, landing configuration | 126 km/h | 68 kts CAS |
| Max. rate of climb (MSL) | 5.2 m/s | 1,028 ft/min |
| Max. range (incl. auxiliary tank) (FL160, 50% PWR) incl. climb, no reserves | 2,385 km | 1,288 nm |
| Fuel consumption at 60% (12,000 ft) in total | 44.7 l/h | 11.8 US gal/h |
| Take-off performance (MSL, ground roll / take-off obstacle) | 480 m / 883 m | 1,574 ft / 2,730 ft |
| Landing performance (MSL, ground roll / landing distance) | 441 m / 779 m | 1,446 ft / 2,555 ft |
| Certified service ceiling | 6,096 m | 20,000 ft |
| Single engine service ceiling (MTOM, ISA, rate of climb: 50 ft/min.) | 3,354 m | 11,000 ft |
| Single engine absolute ceiling (MTOM, ISA, rate of climb: 0 ft/min.) | 4,116 m | 13,500 ft |
| Max. demonstrated crosswind | 46 km/h | 25 kts |
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