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Technoavia SM92 Finist

By Wikipedia,
the free encyclopedia,

http://en.wikipedia.org/wiki/Technoavia_SM92_Finist


Turbo-Finist SMG (reg. no HA-YDF). Periodically used for skydiving
Turbo-Finist SMG (reg. no HA-YDF). Periodically used for skydiving

Technoavia SM92 Finist is a utility aircraft with a STOL capability designed by the Russian company Technoavia. Maiden flight on December 29, 1993. Built by Smolensk aviation plant.

Variants

  • SM92 Finist
  • SM-92T Turbo-Finist
  • SMG-92 Turbine Finist

Operators

 Russia

Specifications

General characteristics

  • Crew: 1 pilot, 6-8 passengers or 600 kg of cargo
  • Wing area: 20.4 m²
  • Wing span 14.60 m
  • Length 9.13 m
  • MTOW: 2350 kg
  • Normal Take-off weight: 2200 kg
  • Empty weight: 1500 kg
  • Powerplant: 360 hp
    • Engine type: 1 PD M-14P
  • Fuel capacity 380 litres

Performance

  • Cruising speed: 200—220 km/h
  • Maximum speed: 280 km/h
  • Range: 1300 km
  • Service ceiling: 3000 m

External links




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Published - July 2009














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