page_title: American Champion Citabria
section_title: Specifications (7GCAA Citabria)
hierarchical_section_title: American Champion Citabria / Specifications (7GCAA Citabria)
context_page_description: The Citabria is a light single-engine, two-seat, fixed conventional gear airplane which entered production in the United States in 1964. Designed for flight training, utility and personal use, it is capable of sustaining aerobatic stresses from +5g to -2g. Its name spelled backwards, "airbatic", reflects this.
context_section_description: Data from FAA Type certificate Data Sheet, The Incomplete Guide to Airfoil Usage and Pilot Friend
  General characteristics
  Crew: one
  Capacity: one passenger
  Airfoil: NACA 4412
  Empty weight: 1,140 lb (517 kg)
  Gross weight: 1,650 lb (748 kg)
  Fuel capacity: 39 U.S. gallons (150 L; 32 imp gal)
  Powerplant: 1 × Lycoming O-320-A2B four cylinder, four-stroke, horizontally opposed aircraft engine, 150 hp (110 kW)
  Propellers: 2-bladed fixed pitch
  Performance
  Maximum speed: 130 mph (209 km/h, 113 kn)
  Cruise speed: 125 mph (202 km/h, 109 kn)
  Stall speed: 49 mph (80 km/h, 43 kn)
  Never exceed speed: 162 mph (261 km/h, 141 kn)
  Range: 473 mi (761 km, 411 nmi)
  Service ceiling: 17,000 ft (5,200 m)
  Rate of climb: 1,120 ft/min (5.7 m/s)
caption: Citabria in flight
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