Article · Wikipedia archive · Last revised Aug 7, 2026

Northrop Beta

The Northrop Beta was an American single-engine, all-metal, low-wing sporting monoplane built in 1931.

Last revised
Aug 7, 2026
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≈ 1 min
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323 w
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Source
Northrop Beta
Northrop Beta 3-view drawing from L'Aerophile Salon 1932
General information
TypeSporting Monoplane
ManufacturerNorthrop
Designer
Number built2 (1 Beta 3 and 1 Beta 3D)1
History
First flight3 March 1931
VariantsNorthrop Alpha
Northrop Gamma

The Northrop Beta was an American single-engine, all-metal, low-wing sporting monoplane built in 1931.1

Design and development

The Beta was a two-seater with a 160 hp (119 kW) Menasco Buccaneer inline engine. The first aircraft registered as NX963Y (later NC963Y) crashed in California. The second aircraft, N12214, was built as a single-seater and fitted with a 300 hp (224 kW) Pratt & Whitney Wasp Jr. radial engine, and became the first aircraft of such power to exceed 200 mph (322 km/h).1 Only two were built.

The aircraft was flown to Wichita for sister company Stearman Aircraft to use as a demonstrator but with the poor economy at the time, none were sold. The aircraft was sold to a wealthy pilot in New York and during its delivery, it passed through Wright Field in order to allow a thorough examination by Army Air Corps Engineers as the Air Corps was still using obsolete biplanes.

After being rarely flown during 1932, the aircraft was sold to a new owner who kept it at Roosevelt Field until it was flipped over at a nearby airport. The aircraft was repaired at the Stearman factory in Wichita and used as an experimental test platform for various flap designs until it crashed due to a wing structural failure on May 4, 1934.

Specifications (Beta 3D)

General characteristics

  • Crew: 1
  • Length: 66 m (21 ft 8 in)
  • Wingspan: 9.75 m (32 ft 0 in)
  • Powerplant: 1 × Pratt & Whitney Wasp Jr. radial, 224 kW (300 hp)

Performance

  • Maximum speed: 341 km/h (212 mph, 184 kn)
  • Cruise speed: 297 km/h (185 mph, 160 kn)
See also

See also

Related development

References

References

  1. The Complete Encyclopedia of World Aircraft. Eds: Paul Eden, Soph Moeng. Amber Books Ltd., London (2002) ISBN 0-7607-3432-1