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Kari-Keen 90 Sioux Coupe

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The Kari-Keen 90 Sioux coupe is a two-seat cabin monoplane.[1]

TypeSport monoplane
National origin
United States
ManufacturerKari-Keen Aircraft Corp, Sioux Aircraft Corporation
Designer
Quick facts Sioux Coupe, General information ...
Sioux Coupe
General information
TypeSport monoplane
National origin
United States
ManufacturerKari-Keen Aircraft Corp, Sioux Aircraft Corporation
Designer
Number built32
History
Manufactured1929-1933
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Development

Kari-Keen was an automotive luggage producer that started in the growing aviation business in 1929. Production of the Sioux coupe began in 1929 and ended on 1 August 1933. The first model, the Kari-Keen 60 Sioux Coup, featured a 60 hp (45 kW) Velie M-5 engine. 22 aircraft were built without a type certificate. In 1930, six more model 90s were built with a type certificate. In 1931, the Sioux Aircraft Corporation bought the company assets, changing the name of the Kari-Keen 90 into the Sioux Coupe 90.[2]

Design

The Kari-Keen 90 Sioux Coupe was designed by Swen Swanson and was a two-seat side-by-side high-wing monoplane with conventional landing gear. The wing was fully cantilevered, with skylights built in. The fuel tank sat above the pilot's head and was part of the leading edge. Ole Fahlin built all the propellers and test-flew the aircraft.[3]

Variants

Kari-Keen 60 Sioux coupe
Sioux Coupe 90
Lambert R-266 radial engine 90 hp.[4]
Sioux Coupe 90A
powered with a 90 hp Brownback Tiger[5]
Sioux Coupe 90B Junior
powered with a 90 hp Warner Scarab Junior - one built
Sioux Coupe 90C Senior
powered with a 110 hp Warner Scarab - one built [6]

Aircraft on display

Specifications (Kari-Keen 90-C Sioux coupe)

Data from FAA TCDS, Sport Aviation

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wing area: 150 sq ft (14 m2)
  • Airfoil: Eieffel 385
  • Gross weight: 1,580 lb (717 kg)
  • Fuel capacity: 25 US gallons (95 L; 21 imp gal)
  • Powerplant: 1 × Warner Scarab Radial, 110 hp (82 kW)
  • Propellers: 2-bladed Ole Fahlin

Performance

  • Cruise speed: 66 kn (76 mph, 122 km/h)

See also

Aircraft of comparable role, configuration, and era

References

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