page_title: AEG C.IV
section_title: Specifications (AEG C.IV)
hierarchical_section_title: AEG C.IV / Specifications (AEG C.IV)
caption_attribution_description: English: AEG C.IV 1917
context_page_description: The AEG C.IV was a German two-seat biplane reconnaissance aircraft that entered service in 1916.
context_section_description: General characteristics
  Crew: 2
  Length: 7.15 m (23 ft 5 in)
  Wingspan: 13.46 m (44 ft 2 in)
  Height: 3.35 m (11 ft 0 in)
  Wing area: 39 m² (420 sq ft)
  Empty weight: 800 kg (1,764 lb)
  Gross weight: 1,120 kg (2,469 lb)
  Powerplant: 1 × Mercedes D.III 6-cylinder, water-cooled, inline piston engine, 120 kW (160 hp)
  Performance
  Maximum speed: 158 km/h (98 mph, 85 kn)
  Range: 450 km (280 mi, 240 nmi)
  Endurance: 4hr
  Service ceiling: 5,000 m (16,000 ft)
  Rate of climb: 2.78 m/s (547 ft/min)
  Time to altitude: 1,000m in 6min
  Armament
  Guns: * 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
  Bombs: * Bomb load up to 100 kg (220 lb)
caption: AEG C.IV
exif: {}