The AEG C.I was a two-seat biplane reconnaissance aircraft produced in small numbers from March 1915. It was essentially an AEG B.II armed with a single Parabellum or Bergmann (rarely) machine gun mounted at the rear of the cockpit for the observer. A more powerful Benz engine increased maximum speed to a more respectable 130 km/h (81 mph). By October of 1915, it had begun to be replaced by the AEG C.II.
Specifications (AEG C.I)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: two, pilot and observer
- Length: 9 m (29 ft 6 in)
- Wingspan: 15 m (49 ft 2 in)
- Height: 3.50 m (11 ft 6 in)
- Wing area: 41.5 m² (447 ft²)
- Powerplant: 1× Benz Bz.III 6-cylinder, water-cooled, inline engine, 112 kW (150 hp)
Performance
- Maximum speed: 130 km/h (81 mph)
- Range: 480 km (300 miles)
- Service ceiling 4,800 m (15,748 ft)
Armament
- 1 × 7.92 mm Parabellum MG14 machine gun
Related content
Related development
Designation sequence
AEG C.I - AEG C.II - AEG C.III - AEG C.IV
Related lists
See also
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