Technoavia SP-95

SP-95
The SP-91 was also marketed outside Russia as the Interavia I-3 (Интеравиа И-3)
General information
Type	Aerobatic monoplane
National origin	Russia
Manufacturer	Technoavia

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 m² (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)

See also

Related development

• Sukhoi Su-26

Related lists

• List of aerobatic aircraft

References

Notes

Bibliography

• Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory 1996/97. London, England: Brassey's. ISBN 1 85753 198 1.