AEG C.I

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The AEG C.I was a two-seat biplane reconnaissance aircraft built by the Allgemeine Elektricitäts-Gesellschaft (AEG) during the First World War for the Imperial German Army's (Deutsches Heer) Imperial German Air Service (Luftstreitkräfte). It was a modified version of the B.II training aircraft with a machine gun added for the observer, a more powerful engine and different wings. First flown in 1915, it remained in front-line service until mid-1916, after which it became a trainer.

TypeReconnaissance aircraft
Introduction date1915
Quick facts General information, Type ...
AEG C.I
General information
TypeReconnaissance aircraft
ManufacturerAEG
Primary userImperial German Flying Corps
History
Introduction date1915
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Development

The C.I was based on the B.II although it was fitted with a water-cooled 150-horsepower (110 kW) Benz Bz.III straight-six piston engine and the two-bay wing planform had been changed. It did retain the B.II's wing-folding mechanism. The rear cockpit was modified to accommodate an observer armed with a single 7.92-millimetre (0.312 in) machine gun, usually a Parabellum MG 14 or, more rarely, a Bergmann MG 15nA.[1]

The Inspectorate of Flying Troops (Inspektion der Fliegertruppen) ordered a batch of six C.Is in early 1915 and the first aircraft was completed in March. Sixty-four more were ordered in four batches over the next several months. Front-line strength peaked at 34 aircraft on 28 February and 30 April 1916 and they were then transferred to training units as no C.Is are shown assigned to front-line units on 30 June.[2]

Specifications (AEG C.I)

Data from German Aircraft of the First World War;[3] A.E.G. Aircraft of WWI: A Centennial Perspective on Great War Airplanes[4]

General characteristics

  • Crew: 2
  • Length: 7.95 m (26 ft 1 in)
  • Upper wingspan: 13.07 m (42 ft 11 in)
  • Lower wingspan: 11.83 m (38 ft 10 in)
  • Wing area: 36 m2 (390 sq ft)
  • Empty weight: 710 kg (1,565 lb)
  • Gross weight: 1,125 kg (2,480 lb)
  • Powerplant: 1 × Benz Bz.III water-cooled, straight-six piston engine, 110 kW (150 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 130 km/h (81 mph, 70 kn)
  • Time to altitude: 11 minutes to 1,000 m (3,300 ft)
  • 25 minutes to 2,000 m (6,600 ft)

Armament

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