AEG C.IV

· AEG · 1 × Mercedes D.III
Length
7.15 m
Flat Wing Span
13.46 m
Height
3.35 m
Flat Wing Area
39 m²
Max Speed
158 km/h
Max Ceiling
5000 m
Number of Engines
1
Aircraft Engine
Entry Into service
1916-01-01
Number Built
687
Maximum Range
450 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
AEG C.IV 450

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Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
AEG J.I Benz Bz.IV 7.2 13.46 Compare
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Caudron Type G 7.3 13.9 Compare
Dewoitine D.9 Bristol Jupiter 7.3 12.8 Compare
De Bruyne Snark De Havilland Gipsy Major 7.3152 12.8016 3 Compare
Delanne 11 7.7 13.5 Compare
All data (21 fields)
Name
AEG C.IV
Manufacturer
AEG
Description
The AEG C.IV was a two-seat biplane reconnaissance aircraft designed and produced by the German aircraft manufacturer Allgemeine Elektrizitäts-Gesellschaft.
Entry Into service
1916-01-01
Designer
AEG
Type
Reconnaissance aircraft
Length (m)
7.15
Height (m)
3.35
Cockpit Crew
2
Max Speed (km/h)
158
Max Ceiling (m)
5000
Rate of Climb (m/s)
2.78
Armament
1 × forward-firing 7.92 mm (.312 in) LMG 08/15 "Spandau" machine gun; 1 × 7.92 mm (.312 in) Parabellum MG14 machine gun in ring mount for observer; Bomb load up to 100 kg (220 lb)
Number Built
687
Powerplant Description
1 × Mercedes D.III six-cylinder, water-cooled, inline piston engine, 120 kW (161 hp) each
Primary Users
Luftstreitkräfte, Turkish Flying Corps , Polish Air Force
Wikipedia Article (URL)
en.wikipedia.org/wiki/AEG_C.IV
Flat Wing Span (m)
13.46
Flat Wing Area (m²)
39
Aircraft Engine
Mercedes D.III
Number of Engines
1