The Technoavia SP-95 is a Russian aerobatic aircraft, a production version of the earlier SP-91 Slava.[1] The design is similar to the Sukhoi Su-26 family as it was designed by the same designer.[1] It is an aerobatic competition aircraft and can be changed from single-seat to two-seat configuration.[1] The SP-95 is a metal construction low-wing cantilever monoplane with a conventional landing gear with a tail-wheel.[1] It is powered by a Vedeneyev M14P radial piston engine.[1]

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

Variants

SP-91 Slava

Prototype aerobatic competition aircraft powered by an AOOT M-14P engine, five built.[1] Also marketed outside Russia as the Interavia I-3.

SP-95

Production variant of the SP-91.[1]

Specifications (SP-95)

Data from [1]

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

Wikimedia Commons has media related to Technoavia SP-95.

Notes

Bibliography

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