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

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

External links

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

Aircraft produced by Sablatnig

SF-1 SF-2 SF-3 SF-4 SF-5 SF-6 SF-7 SF-8 B.I C.I C.II C.III N.I P.I P.III

Idflieg C-, CL-, CS-, and CLS-class aircraft designations

C- and CL-	AEG C.I C.II C.III C.IV C.V C.VI C.VII C.VIII AGO C.I C.II C.III C.IV C.VII C.VII Albatros C.I C.II C.III C.IV C.V C.VI C.VII C.VIII C.IX C.X C.XI C.XII C.XIII C.XIV C.XV Aviatik C.I C.II C.III C.V C.VI C.VIII C.IX BFW CL.I CL.II CL.III CL.IV DFW C.I C.II C.III C.IV C.V C.VI Fokker C.I Friedrichshafen C.I Germania C.I C.II C.IV Halberstadt C.I CL.II C.III CL.IV C.V C.VII C.VIII C.IX CLS.X Hannover C.I CL.II CL.III CL.IV CL.V Junkers CL.I LFG/Roland C.I C.II C.III C.V C.VIII LVG C.I C.II C.III C.IV C.V C.VI C.VIII OAW C.I C.II Otto C.I C.II Pfalz C.I Rumpler C.I C.III C.IV C.V C.VI C.VII C.VIII C.IX C.X Sablatnig C.I C.II C.III Schütte-Lanz C.I Zeppelin-Friedrichshafen C.I C.II Zeppelin-Lindau C.I C.II

CLS-	Albatros CLS.I Halberstadt CLS.I CLS.II (see also main sequence above) Junkers CLS.I

CS-	Zeppelin-Lindau CS.I

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