Power Plant
Engine | 2 × Austro Engine AE 330 turbocharged common-rail injected 2.0 liter jet fuel engine with 180 HP and EECU single lever control system |
|---|---|
Propeller | 2 × 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)
* Typical Surveillance Configuration
| Max. cruise speed (14,000 ft MCP ISA) | 326 km/h TAS | 176 kts TAS |
|---|---|---|
| Mission speed / Consumption (ISA, 6,000 ft) at 45 % power at 75 % power | 207 km/h TAS / 34 lt/hr 274 km/h TAS / 56 lt/hr | 112 kts TAS / 9.0 USGal/hr 148 kts TAS / 14.8 USGal/hr |
| Consumption at 35 % power (loiter speed) in total | 28 lt/hr | 7.4 USGal/hr |
| Max. airborne operations time | 9.6 hours | 9.6 hours |
| Typical airborne operations time1) | 6 - 8 hours | 6 - 8 hours |
| Max. range at 50 % power in 14,000 ft | 2,111 km | 1,140 nm |
| Takeoff performance (ISA, MSL, ground roll / take-off distance) | 556 m / 947 m | 1,824 ft / 3,107 ft |
| Landing performance (ISA, MSL, ground roll / landing distance) | 441 m / 779 m | 1,447 ft / 2,556 ft |
| Max. service ceiling | 6,096 m | 20,000 ft |
Dimensions
Mass and Loading
| Crew | 1 or 2 pilots | 1 or 2 operators |
| Typical mission crew | 1 pilot | 1 operator |
| Empty weight | 1,590 kg | 3,505 lbs |
| Useful load | 710 kg | 1,565 lbs |
| Max. take off mass (with STC-62-005) | 2,300 kg (2,360 kg) | 5,071 lbs (5,203 lbs) |
| Max. usable fuel capacity main tank auxiliary tank | 326 l / 261 kg 189 l / 151 kg 137 l / 110 kg | 86 US gal / 576 lbs 50 US gal / 335 lbs 36 US gal / 241 lbs |
Mass & Balance
| Maximum take off mass | 2,300 kg | 5,071 lbs |
| Empty weight | 1,590 kg* | 3,505 lbs* |
| Payload available in TOTAL | 710 kg | 1,566 lbs |
| Typical airplane standard options | 58 kg** | 128 lbs** |
| Crew (2 men) | 160 kg | 353 lbs |
| Fuel (86 US gal/ 326 lt Jetfuel) | 265 kg*** | 576 lbs*** |
| TKS anti-icing fluid (3.9 US gal/ 15 lt) | 16 kg | 35 lbs |
| Payload mission equipment | 215 kg | 474 lbs |
1. With standard mission equippment and 2-man crew.
* Average empty weight, excl. airplane standard options ** TKS anti-icing installation, Auxiliary tanks, DME, WX500 stormscope, Avidyne TAS605 *** Specific fuel weight 0.8 kg/lt
Specifications are based on clean aircraft without sensor or mission equipment. Specifications can differ depending on the specific sensor equipment. The above quoted data are approximately specifications and may change without notice.