Single-engine pistonutility aircraft
Progress Rysachok
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The Technoavia Rysachok (Ru:Рысачок, English: Trotter) is a general purpose, twin turboprop-powered engined light utility aircraft, designed and built in Russia by Technoavia. Certification was expected by 2012 and by autumn 2011 three flight pre-production examples had been completed and flown. As of 2015 the certification process is stalled and Technoavia has declared that it is no longer involved in the project.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Category
- Single-engine piston
- Country of origin
- Russia
- First flight
- 2010-12-03
Specifications
- Cruise speed
- 135 kt
- Max speed
- 211 kt
- Range
- 1,100 nm
- Service ceiling
- 20,000 ft
- Max takeoff weight
- 12,566 lb
- Empty weight
- 6,107 lb
- Fuel capacity
- 502 US gal
- Powerplant
- Walter M601 F turboprop
- Engines
- 2
- Seats
- 19
- Length
- 40.8 ft
- Wingspan
- 59 ft
- Height
- 17.7 ft
- Number built
- 5
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.