- AEG C.I
infobox Aircraft
name =AEG C.I
type =Reconnaissance aircraft
manufacturer =AEG
caption =
designer =
first flight =
introduced =1915
retired =
status =
primary user =
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produced =
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variants with their own articles =TheAEG C.I was a two-seatbiplane reconnaissance aircraft produced in small numbers from March 1915. It was essentially anAEG 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 1915, it had begun to be replaced by theAEG C.II .pecifications (AEG C.I)
aircraft specifications
plane or copter?= plane
jet or prop?= prop
ref=
crew=two, pilot and observer
capacity=
length main= 9 m
length alt= 29 ft 6 in
span main= 15 m
span alt= 49 ft 2 in
height main= 3.50 m
height alt= 11 ft 6 in
area main= 41.5 m²
area alt= 447 ft²
airfoil=
empty weight main=
empty weight alt=
loaded weight main=
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useful load main=
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max takeoff weight main=
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engine (prop)=Benz Bz.III
type of prop=6-cylinder, water-cooled, inline engine
number of props=1
power main= 112 kW
power alt= 150 hp
power original=
max speed main= 130 km/h
max speed alt= 81 mph
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 480 km
range alt= 300 miles
ceiling main= 4,800 m
ceiling alt= 15,748 ft
climb rate main=
climb rate alt=
loading main=
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armament=
* 1 × 7.92 mmParabellum MG14 machine gun
avionics=ee also
aircontent
related=AEG B.II
similar aircraft=
lists=
*List of military aircraft of Germany
see also=
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