| Specifications |
|---|
| Power plant | 2TRD-LARZAC 04R20 |
| Maximum static thrust, kg | 2x1,440 |
| Engine maximum take-off power, hp | 2x2,20 |
| Wing area, sq.m | 17.67 |
| Takeoff weight, kg | 4,610 |
| Fuel capacity, normal/total, kg | 850/1,680 |
| Thrust-to-weight ratio | 0.625 |
| Takeoff speed, km/h | 180 |
| Maximum ground-level speed, km/h | 850 |
| Max M | 0.85 |
| Service ceiling, m | 15,500 |
| Maximum operational g-load | +8.0 to -3.0 |
| Steady-state turn g-load (H = 4 km, M = 0.7) | 5.5 |
| Max permissible angle of attack, deg | >25 |
| Flight range, km (H = 6 km, M = 0.5) | 1,200 |
| Ferry range, km | 2,400 |
| Landing speed, km/h | 175 |
| Specific maintenance workload, manhours/flying hours | Cw = 2.22 |
| Flying time per flight accident owing to design/production causes, thou h | >150 |
| Average flying time before failure and damage revealed in flight and on ground, h | Ta = 16.5 |
| Probability of trouble-free operation in flying mission | Pfm = 0.9902 |
| Aircraft service life, flying hours | 15,000 |
| Operational life, years | 30 |
