| Technical data | |
|---|---|
| Type | Su-29 |
| Function | Aerobatic trainer |
| Year | 1992? |
| Crew | 2 |
| Engines | 1*360hp M-14P |
| Length | m |
| Wingspan | m |
| Wing area | m2 |
| Empty weight | 735kg |
| Loaded weight | 862kg |
| Maximum takeoff weight | 1200kg |
| Wing Load (kg/m2) | |
| Power load (kg/hp) | 2.39 |
| Maximum Speed (horizontal) | 325km/h |
| Maximum allowed | 450km/h |
| Landing Speed | 120km/h |
| Landing Roll | m sec |
| Takeoff Roll | m sec |
| Turn time | sec |
| Roll rate | 6rad/sec |
| g-Limits | +12/-10 |
| Ferry Range | 1200km |
| Flight Endurance | hmin |
| Ceiling | m |
| Climb | |
| Rate at 0m | 16 m/sec |
| Payload | |
| Fuel | kg |
| Cost (approx) | 190,000USD |
Su-29, P.O.Sukhoj
 |
Two-seater, designated for aerobatic training, competitions and airshows. Aircraft is based on Su-26M single-seater and utilizes most of technology of the predecessor. Thanks to wider use of composite materials, aircraft performance with one pilot is similar to this of a single-seater predecessor.
First production batch (1992, about 30 planes) was sold to customers all over the World. In 1993 production started at Dubna machine assembly factory. In 1994 aircraft was certified in Russia (???).
Su-29 may be custom equipped with "Bekker" or "Bendix King" navigation equipment, as well as GPS.
At the 1996 World Aerobatic Championships in Oklahoma City, the Russian Sukhoi Design Bureau demonstrated an ejection seat for Su-29 two place unlimited competition aerobatic aircraft.
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