title: Technoavia SP-95
text: # Technoavia SP-95
  
  The Technoavia SP-95 is a Russian aerobatic aircraft, a production version of the earlier SP-91 Slava. The design is similar to the Sukhoi Su-26 family as it was designed by the same designer. It is an aerobatic competition aircraft and can be changed from single-seat to two-seat configuration. The SP-95 is a metal construction low-wing cantilever monoplane with a conventional landing gear with a tail-wheel. It is powered by a Vedeneyev M14P radial piston engine.
  
  ## Variants
  
  ### SP-91 Slava
  
      Prototype aerobatic competition aircraft powered by an AOOT M-14P engine, five built. Also marketed outside Russia as the Interavia I-3.
  
  ### SP-95
  
      Production variant of the SP-91.
  
  ## Specifications (SP-95)
  
  Data from
  
  General characteristics
  
  * Crew: one or two
  * Length: 7.00 m (23 ft 0 in)
  * Wingspan: 8.40 m (27 ft 7 in)
  * Wing area: 11.7 $m^2$ (126 sq ft)
  * Aspect ratio: 6.03
  * Empty weight: 800 kg (1,764 lb)
  * Max takeoff weight: 1,080 kg (2,381 lb)
  * Powerplant: 1 × Vedeneyev M14P Nine-cylinder radial engine, 270 kW (360 hp)
  * Propellers: 3-bladed
  
  Performance
  
  * Maximum speed: 300 km/h (190 mph, 160 kn)
  * Stall speed: 105 km/h (65 mph, 57 kn)
  * Never exceed speed: 450 km/h (280 mph, 240 kn)
  * Range: 1,300 km (810 mi, 700 nmi) with full fuel
  * g limits: +11, - 9 (single-seat) or +12, -10 (two-seat)
  * Rate of climb: 17.0 m/s (3,350 ft/min)
  