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
Rate at 0m 16 m/sec
Fuel kg
Cost (approx) 190,000USD

Su-29, P.O.Sukhoj

32k photo by O.T.Kieboom, Farnborough-1996

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.





  • Su-29 aerobatic plane (Russian)
  • SUKHOI Su-29
  • Russian Aerobatic Team
  • Sukhoj ejection seat
  • Aerobatic Movies
  • Civilian/Aerobats
  • Bob's Airplane Gallery
  • Sukhoj Aircraft at AAHZ'S AVIATION PAGE
  • Su-29/31 sales to South Korea
  • John Piggott, pilot of the Su-29;
  • Bob Davis Dacy airshow
  • Sukoi Su-29 - flying copy!
  • Asian Aerospace'98
  • Profile of Patric Williams
  • Aerobatic Images
  • Irkutsk Aeroclub ROSTO

  • Created December 10, 1996
    Modified February 10, 1999
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