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http://en.wikipedia.org/wiki/Technoavia_SM92_Finist  |
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
- 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 in July 2009.
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