# Technoavia SP-95

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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](/source/Aerobatic_aircraft), a production version of the earlier SP-91 Slava.[1] The design is similar to the [Sukhoi Su-26](/source/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](/source/Conventional_landing_gear) with a tail-wheel.[1] It is powered by a [Vedeneyev M14P](/source/Vedeneyev_M14P) radial piston engine.[1]

## 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](/source/Aspect_ratio_(aeronautics)):** 6.03

- **Empty weight:** 800 kg (1,764 lb)

- **Max takeoff weight:** 1,080 kg (2,381 lb)

- **Powerplant:** 1 × [Vedeneyev M14P](/source/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](/source/V_speeds#VNE):** 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](/source/Sukhoi_Su-26)

**Related lists**

- [List of aerobatic aircraft](/source/List_of_aerobatic_aircraft)

## References

Wikimedia Commons has media related to [Technoavia SP-95](https://commons.wikimedia.org/wiki/Category:Technoavia_SP-95).

**Notes**

1. ^ [***a***](#cite_ref-brassey_1-0) [***b***](#cite_ref-brassey_1-1) [***c***](#cite_ref-brassey_1-2) [***d***](#cite_ref-brassey_1-3) [***e***](#cite_ref-brassey_1-4) [***f***](#cite_ref-brassey_1-5) [***g***](#cite_ref-brassey_1-6) [***h***](#cite_ref-brassey_1-7) Taylor 1996, p. 428

**Bibliography**

- Taylor, Michael J. H. (1996). [*Brassey's World Aircraft & Systems Directory 1996/97*](https://archive.org/details/brasseysworldair0000unse). London, England: Brassey's. [ISBN](/source/ISBN_(identifier)) [1 85753 198 1](https://en.wikipedia.org/wiki/Special:BookSources/1_85753_198_1).

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Adapted from the Wikipedia article [Technoavia SP-95](https://en.wikipedia.org/wiki/Technoavia_SP-95) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/Technoavia_SP-95?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.