type of aircraft
Sablatnig C.I
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The Sablatnig C.I was a conventional C-type reconnaissance two-seater aircraft developed and built by Sablatnig in Berlin, Germany in 1917. It was a two-bay biplane of conventional design, with staggered wings, two open cockpits in tandem, and fixed, tailskid undercarriage. The C.I was developed into the Sablatnig N.I in 1918.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Sablatnig
- Country of origin
- German Reich
- First flight
- 1917-01-01
Specifications
- Max speed
- 65 kt
- Service ceiling
- 3,281 ft
- Max takeoff weight
- 3,395 lb
- Empty weight
- 2,315 lb
- Powerplant
- Argus As III
- Engines
- 1
- Seats
- 2
- Length
- 28 ft
- Wingspan
- 52 ft
- Number built
- 2
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.