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From Wikipedia, the free encyclopedia

Boeing NB-1 landplane in flight near NAS Pensacola.jpeg
Boeing NB-1
Role Military trainer
Manufacturer Boeing
First flight 20 October 1923
Number built ca. 72

The Boeing NB (or Model 21) was a primary training aircraft developed for the United States Navy in 1923. It was a two-bay, equal-span biplane of conventional configuration with interchangeable wheeled and float undercarriage. The pilot and instructor sat in tandem, open cockpits.

The NBs were produced in two batches; the first (NB-1) were powered by radial engines and the second by war-surplus V-8s still in the Navy's inventory. The original prototype evaluated by the Navy had been assessed as being too easy to fly, and therefore of limited use as a trainer. In particular, it was noted that the aircraft was impossible to spin. The NB-1 design attempted to introduce some instability, but it was soon discovered that while it was now possible to get the aircraft into a spin, it was virtually impossible to recover from one. A series of modifications were made to attempt a compromise.

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An NB-1 floatplane at the National Advisory Committee for Aeronautics, in 1926.
An NB-1 floatplane at the National Advisory Committee for Aeronautics, in 1926.
  • VNB-1 - prototype (one built)
  • NB-1 - original production machine with Lawrance J-1 radial engine (41 built)
Boeing NB-2 at Langley
Boeing NB-2 at Langley
  • NB-2 - production machine with Wright-Hispano E engine (30 built)
  • NB-3 - one NB-1 with lengthened fuselage and modified empennage to improve handling, and Hispano-Suiza E engine. Later refitted to standard NB-1
  • NB-4 - one NB-1 converted similar to NB-3, but with Lawrance J-1 engine. Later refitted to standard NB-1


 United States

Specifications (NB-1)

General characteristics

  • Crew: two, pilot and instructor
  • Length: 28 ft 9 in (8.76 m)
  • Wingspan: 36 ft 10 in (11.23 m)
  • Height: 11 ft 8 in (3.56 m)
  • Wing area: 344 ft2 (32.0 m2)
  • Empty weight: 2,136 lb (969 kg)
  • Gross weight: 2,837 lb (1,287 kg)
  • Powerplant: 1 × Lawrance J-1, 200 hp (149 kW)


  • Maximum speed: 100 mph (160 km/h)
  • Range: 300 miles (480 km)
  • Service ceiling: 10.200 ft (3,110 m)
  • Rate of climb: 510 ft/min (2.6 m/s) 


  • 1 × trainable rearward-firing .30 machine gun (optional, for gunnery training)


  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 170.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 51.

This page was last edited on 3 February 2019, at 02:52
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