| Specifications |
| Max. speed - at 11,000 m |
850 km/h |
| - at 5,000 m |
755 km/h |
| - at sea level |
720 km/h |
| Max. range (without auxiliary fuel tanks) |
1000 km |
| Max. range (with auxiliary fuel tanks) |
1750 km |
| Service ceiling |
11 500 m |
| Max. climb (with armament) |
22 m/s |
| Flight endurance (with auxiliary fuel tanks) |
3 h 50 min |
| Flight endurance (without auxiliary fuel tanks) |
2 h 30 min |
| Engine |
ZMBD Progress (Ivchenko) AI-25TL |
| Thrust |
16,87 kN |
| Armament load |
kg |
| Max. takeoff weight |
4700 kg |
| Opt. takeoff weight |
4525 kg |
| Empty weight |
3540 kg |
| Wingspan (including fuel tanks) |
9,46 m |
| Capacity of auxiliary fuel tanks |
2x420 l |
| Length |
12,13 m |
| Height |
4,77 m |
| Wing area |
18,8 m2 |
| Max. permitted g |
-4/+8g |
| Armament |
23 mm GSh-23 two barrelled cannon and various combination of bombs |
