• Source: 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



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

Kata Kunci Pencarian:

• Sablatnig C.I
• Sablatnig
• Sablatnig N.I
• Albatros C.I
• AEG C.I
• List of World War I Central Powers aircraft
• List of military aircraft of Germany by manufacturer
• Fokker C.I
• Sablatnig C.II
• List of aircraft (Sa)