Sablatnig C.I

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.

== Specifications == General characteristics

Length: 8.7 m (28 ft 7 in) Wingspan: 16.0 m (52 ft 6 in) Empty weight: 1,050 kg (2,315 lb) Gross weight: 1,540 kg (3,395 lb) Powerplant: 1 × Argus As III , 130 kW (180 hp) Propellers: 2-bladed Performance

Maximum speed: 120 km/h (75 mph, 65 kn) Time to altitude: 9 min to 3,281 ft (1,000 m) Armament

Guns: 1 x Parabellum machine-gun Bombs: 6 x 110 lb (50 kg) bombs

Notes

== References == Gray, Peter & Thetford, Owen (1987) [1970]. German Aircraft of the First World War (2nd ed.). London: Putnam. ISBN 0-85177-809-7.

External links

https://1000aircraftphotos.com/Contributions/McBrideBill/9356.htm