Czech airplane
Letov Š-14
The Letov Š-14 was a single-seat, single-engine aircraft, designed and built in Czechoslovakia in the early 1920s. Originally intended as a biplane fighter, it was later modified into a monoplane and entered as a contestant in a speed competition.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Letov
- Country of origin
- Czechoslovakia
- First flight
- 1924-01-01
Specifications
- Cruise speed
- 129 kt
- Max speed
- 129 kt
- Range
- 267 nm
- Service ceiling
- 16,405 ft
- Max takeoff weight
- 1,975 lb
- Empty weight
- 1,464 lb
- Powerplant
- Hispano-Suiza 8Fb V8 water-cooled
- Engines
- 1
- Seats
- 1
- Length
- 21.1 ft
- Wingspan
- 26.6 ft
- Number built
- 1
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.