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Sablatnig C.I

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Title: Sablatnig C.I  
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Language: English
Subject: Franz Schneider
Publisher: World Heritage Encyclopedia

Sablatnig C.I

Sablatnig C.I
Role reconnaissance two-seater
National origin Germany
Manufacturer Sablatnig
Produced 1917
Number built ~2

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 (variant specified)

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


  • Maximum speed: 120 km/h (75 mph; 65 kn)
  • Time to altitude: 9 min to 3,281 ft (1,000 m)
  • Guns: 1 x Parabellum machine-gun
  • Bombs: 6 x 110 lb (50 kg) bombs



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