Speed
| Utility | Normal | |
| Vne (MAX. BRS DEPLOY) | 315 KMH | 315 KMH |
| Va (maneuver IAS) | 270 KMH | 220 KMH |
| Vno (max. cruise speed) | 226 KMH | 223 KMH |
| Vfe (max. IAS w. Flaps extended) | 185 KMH | 185 KMH |
| Vs (min. IAS w. Flaps retracted) | 100 KMH | 102 KMH |
| Vs1 (min. IAS w. Flaps T/O) | 96 KMH | 99 KMH |
| Vs0 (min. IAS in landing conf.) | 89 KMH | 91 KMH |
| Vbg (best gliding, flaps retracted), ratio 7.51 | 139 KMH | 142 KMH |
| Max Speed to enter steep Aerobatic | 160 KMH | ----- |
Take-Off Performance
| Utility | Normal | |
| T/O Roll | 185 m | 200 m |
| VR | 90 KMH | 92 KMH |
| T/O Distance | 380 m | 410 m |
| V2 | 114 KMH | 116 KMH |
Height: 0 m MCA
Engine: Take-Off performance
Flap: T/O
Runway: dry concrete
Wind Limits
| Side Wind | 10 MPS | 19 kt |
Engine Performance
| RPM | Boost | |
| Max 1 sec | 3025 RPM | 1.02 kgf/сm2 |
| Max 30 sec | 2860 RPM | 0.85 kgf/сm2 |
| Max Take-Off | 2750 RPM | 0.965 kgf/сm2 |
| Max Cont. | 2680 RPM | 1.02 kgf/сm2 |
Oil Tank
| Max Oil fill | 12L |
| Oil fill for Aerobatic | 9L |
| Min Oil fill | 7L |
G-Factor
| Utility | +5 | -3.2 |
| Normal | +3.8 | -1.5 |
Intentional spin with extended flaps PROHIBITED
Min Pressure of main spar: 1.5 kgf/cm2
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