| Technical data | |
|---|---|
| Type | Su-31M |
| Function | Aerobatic |
| Year | 197? |
| Crew | 1 |
| Engines | 1*400/360hp Vedeneyev M-14PF |
| Length | 6.83m |
| Wingspan | 7.80m |
| Wing area | 11.80m2 |
| Height | 2.4m |
| Empty weight | 670kg |
| Loaded weight | 968kg |
| Wing Load (kg/m2) | 82.0 |
| Power load (kg/hp) | 2.67 |
| Speed | 407km/h |
| Stall Speed | 98km/h |
| Roll rate | 420°/sec |
| Service g-Limits | +12/-10 |
| Ultimate g-Limits | +23/-23 |
| Landing Speed | 114km/h |
| Landing Roll | ?m |
| Takeoff Roll | ?m |
| Turn time | ?sec |
| Ferry Range | 1200km |
| Flight Endurance | 40+min |
| Ceiling | 4000m |
| Climb | |
| Rate at 0m | 24m/sec |
| 1000m | min |
| Payload | |
| Fuel | 280+?l |
| Cost | ?USD |
Su-31M aerobatic by Sukhoj OKB
 |
Sukhoi has delivered (Dec 1997?) its' first Su-31M sport aerobatic trainer, equipped with the new SKS-94 super light ejection seat. The $35000 ejection system is designed by Advanced Sukhoi Technology and Zvezda, Russian main manufacturer of military ejection seats. aircraft also received new canopy, in-wing fuel tanks and auxiliary underbelly tank.
The World Championship heritage of the Sukhoi Aircraft is also displayed by the SUKHOI SOLO. The "monstrously powerful" Sukhoi Su-31X provides by far the highest power to weight ratio of any propeller driven aircraft, hanging from the propeller it will roll vertically several times- a real helicopter.
| Predecessors | Modifications | |
|---|---|---|
 Su-31 |
? | |
