SR-10 dual-pilot light jet trainer
| length | 9.59 meters |
| wing span | 8.4 m |
| swept wings | -10° |
| normal empty weight kg 2000 | |
| normal take-off mass | 2400 kg |
| Max. take-off weight | 3100 kg / 2.7 tons |
| Power plant, Type | turbofan, AL-55 |
| number / power x., kgf | 1 x 1750 |
| Cruising speed H = 6000 m, km / h | 520 |
| Maximum maneuvering speed, km / h | 700 |
| Maximum speed of horizontal flight, km / h | 900 |
| Maximum number of flight | M 0.85 |
| Max. speed | 800 km/h 900 km/h (Mach 0.85) up to 600 mph; Mach 0.78 |
| Service ceiling, m | 6000 |
| separation speed, km / h | 190 |
| Landing speed, km / h | 185 |
| Landing speed, km / h | 180 |
| Practical ceiling, m | 11000 |
| Maximum range, km | 1500 |
| Practical range, km | 1200 km or 1,000 miles |
| Maximum rate of climb at sea level, | m/s 60 |
| Minimum radius steady bend, m | 290 |
| Maximum angular velocity of rotation of the roll, | rad / s 7 |
| operating overload range | + 10 -8 |
| Max. operational overload damage. | + 8 / -6 |
| Crew | 2 people. |
| Location crew | tandem |
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