Single-engine pistongeneral aviation aircraft
Praga E-210
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The Praga E-210 was a four-seat, twin-engined touring aircraft built in Czechoslovakia in the late 1930s. It had an unusual pusher configuration . Its tail unit and undercarriage were modified significantly before World War II and after the war a more powerful version designated E-211 was flown.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- ČKD-Praga
- Category
- Single-engine piston
- First flight
- 1936-01-01
Specifications
- Cruise speed
- 110 kt
- Max speed
- 120 kt
- Range
- 320 nm
- Service ceiling
- 14,800 ft
- Max takeoff weight
- 2,756 lb
- Empty weight
- 1,609 lb
- Powerplant
- Walter Minor 4
- Engines
- 2
- Seats
- 4
- Length
- 27.9 ft
- Wingspan
- 41 ft
- Height
- 6.8 ft
- Number built
- 3
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.