Bellanca 8KCAB "Decathlon"
United States — two-seat light cabin monoplane

Archive Photos

Bellanca 8KCAB "Decathlon" (N986N) at the Hawthorne Air Faire, Hawthorne, CA

1979 Bellanca 8KCAB "Decathlon" (N5062E) at the 1990 MCAS El Toro Airshow

Bellanca 8KCAB "Decathlon" at the 1988 MCAS El Toro Airshow


  • Role: Sports plane and aerobatic trainer
  • Manufacturer: American Champion Aircraft
  • Designed by: Champion Aircraft Corporation
  • Introduced: 1970
  • Number built: Over 9,000

The 8KCAB Decathlon and Super Decathlon are two-seat fixed conventional gear light airplanes designed for flight training and personal use and capable of sustaining aerobatic stresses between +6g and -5g. The Decathlon entered production in the United States in 1970 as a more powerful and stronger complement to the Citabria line of aircraft.

The Decathlon was designed by the Champion Aircraft Corporation, and is a derivative of the 7-series Citabrias. While the Citabria designs remain successful, and the introduction of the 7KCAB variant of the Citabria had added limited inverted flight capability, the Citabrias are not capable of “outside” maneuvers, those requiring significant negative-g loads. Pilots wanted an aircraft capable of more maneuvers, and Champion introduced the 8KCAB Decathlon in response to this demand.

Production History

The Decathlon entered production at Champion in 1972, immediately before the company was acquired by Bellanca Aircraft Corporation, so only a handful were produced by Champion. Bellanca continued production of the Decathlon throughout the 1970s, moving to the Super Decathlon variant during 1976. Bellanca built over 600 of the 8KCAB design before production of the aircraft was interrupted when the company's assets were liquidated in 1981.

The Decathlon design passed through the hands of a number of companies through the 1980s, including a Champion Aircraft Company which was no relation to the Champion Aircraft of the 1960s, but no Decathlons were built in that period. American Champion Aircraft Corporation acquired the Decathlon design, along with the 8GCBC Scout and the group of Citabria and Champ variants, in 1990, bringing the Super Decathlon version back into production that same year. It is still being produced.


The Decathlon traces its lineage back to the Aeronca Champ, by way of the Citabria. Like the Citabria, the Decathlon features tandem seating and joystick controls. The fuselage and tail surfaces are constructed of welded metal tubing. The outer shape of the fuselage is created by a combination of wooden formers and longerons, covered with fabric. The cross-section of the metal fuselage truss is triangular, a design feature which can be traced back to the earliest Aeronca C-2 design of the late 1920s.

The strut-braced wings of the Decathlon are, like the fuselage and tail surfaces, fabric covered, using aluminum ribs. The wings of Champion and Bellanca Decathlons were built with wooden spars. American Champion has been using aluminum spars in the aircraft it has produced and has made the aluminum-spar wings available for retrofit installation on older aircraft. Compared to the Citabria’s wingspan of 33.5 feet (10.2 m), the Decathlon's wingspan is shorter, at 32 feet (9.8 m). One of the major developments of the 8KCAB Decathlon over the 7KCAB Citabria is the Decathlon’s wing, which employs a semi-symmetric airfoil, as opposed to the Citabria’s flat-bottomed airfoil. This change gives the Decathlon better inverted flight and negative-g maneuver capabilities.

The landing gear of the Decathlon is in a conventional arrangement. The main gear legs of most Decathlons are made of spring steel, though American Champion began to use aluminum gear legs in 2004.

Like the 7KCAB, the engine of the 8KCAB has a fuel injection system, as opposed to a carburetor. To facilitate negative-g flight, the fuel system incorporates a 1.5 gallon header tank beneath the instrument panel, and the engine is fitted with a Christen Industries inverted oil system.

Champion and Bellanca built the Decathlon with several Lycoming IO-320 engine variants, all of 150 horsepower (110 kW), and with the choice of a fixed-pitch or constant speed propeller. The major improvement in Bellanca’s introduction of the Super Decathlon was the change of engine to the Lycoming AEIO-360-H1A or -H1B, both of 180 horsepower (130 kW), which was accompanied by a selection of constant speed propellers. The American Champion Super Decathlon uses the AEIO-360-H1B, along with a constant speed propeller.

Operational History

Though the Decathlon went out of production within a decade of its introduction, this was not due to any fault in the design but rather to the slump in general aviation in the United States at the end of the 1970s and the beginning of the 1980s. Since its reintroduction, the Super Decathlon has sold steadily. Decathlons and Super Decathlons remain popular as aerobatic trainers, as beginning and intermediate aerobatic aircraft, and as personal aircraft.

Bellanca 8KCAB Specifications 3


  • Two-seat light cabin monoplane.


  • Braced high-wing monoplane.
  • Wing section NACA 1412 modified.
  • Dihedral 1°.
  • Incidence 1°30'.
  • Size of front spar substantially increased and ribs stronger and more closely spaced by comparison with Citabria.
  • Trusses added between front and rear spars in aileron area.
  • Aluminium (front) and steel tube (rear) Vee bracing struts each side, of enlarged section


  • Welded steel tube structure, fabric covered.

Tail Unit

  • Wire-braced welded steel tube structure.
  • Fixed-incidence tailplane.
  • Trim tab in elevator.

Landing Gear

  • Non-retractable tailwheel type.
  • Cantilever spring steel main gear.
  • Fairings on main wheels.

Power Plant

  • One 150-hp Lycoming IO-320-E1A or IO-320-E1B four-cylinder horizontally-opposed air-cooled engine, driving a Hartzell HC-C2YL-4/C7663-4 two-blade metal counterweighted constant-speed propeller.
  • Two wing fuel tanks, with total usable capacity of 40 US gallons (151.4 L).
  • Oil capacity 2 US gallons (7.5 L).


  • Enclosed cabin seating two persons in tandem.
  • Quick-jettison door on starboard side.
  • Space for 100 lb (45 kg) baggage.

Dimensions (external)

  • Wing span: 32 ft 0 in (9.75 m)
  • Wing chord (constant): 5 ft 4 in (1.63 m)
  • Length overall: 22 ft 10.75 in (6.98 m)
  • Height overall: 7 ft 9 in (2.36 m)
  • Wheel track: 6 ft 4 in (1.93 m
  • Wheelbase: 16 ft 4 in (4.98 m)


  • Wings, gross: 169 ft² (15.7 m²)
  • Ailerons (total): 20.68 ft² (1.92 m²)
  • Fin: 7.02 ft² (0.65 m²)
  • Rudder: 6.83 ft² (0.63 m²)
  • Tailplane: 12.25 ft² (1.14 m²)
  • Elevators, including tab: 14.58 ft² (1.35 m²)

Weights and Loadings

  • Weight empty: 1,275 lb (578 kg)
  • Max T-O weight: 1,800 lb (815 kg)
  • Max wing loading: 10.7 lb/ft² (52.2 kg/m²)
  • Max power loading: 12.0 lb/hp (5.44 kg/hp)

Performance @ max T-O weight

  • Max never-exceed speed: 156 knots (180 mph; 289 km/h)
  • Max level speed: 126 knots (145 mph; 233 km/h)
  • Max cruising speed @ 75% power at 8,000 ft (2,440 m): 121 knots (140 mph; 225 km/h)
  • Cruising speed @ 65% power: 114 knots (132 mph; 212 km/h)
  • Stalling speed: 46 knots (53 mph; 86 km/h)
  • Max rate of climb @ S/L: 1,025 ft/min (312 m/min)
  • Service ceiling: 16,000 ft (4,875 m)
  • Max range: 538 nm (620 miles; 998 km)


  1. Photos: John Shupek, Copyright © 2009 Skytamer Images. All Rights Reserved
  2. Wikepedia. American Champion Decathlon
  3. Taylor, John W.R., "Bellanca: Champion (Bellanca) Model 8CAB Decathelon." Jane’s All The World’s Aircraft 1975-76”. Jane's Yearbooks, New York, 1975. pp. 275

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