Supriya Ghosh (Editor)

Spartan NP

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Top speed
  
174 km/h

Length
  
7.39 m

Wingspan
  
10 m

Manufacturer
  
Spartan Aircraft Company

Spartan NP httpsuploadwikimediaorgwikipediacommonsthu

The Spartan NP-1 was a two-seat primary trainer designed and built by the Spartan Aircraft Company for the United States Navy reserve units.

Contents

Development

On 10 July 1940 the company received an order from the United States Navy for 201 aircraft for use as a biplane primary trainer, it was to be a modernised version of the companies earlier C-3. It was a conventional biplane with two-seats in tandem open cockpits. Designated by the company as the NS-1 it was given the military designation NP-1. The NP-1 was powered by a 220 hp (164 kW) Lycoming R-680-8 radial engine.

Operators

 United States
  • United States Navy

    • Specifications (NP-1)

    Data from United States Navy Aircraft since 1911

    General characteristics

  • Crew: 2 (pilot, student)
  • Length: 24 ft 3 in (7.39 m)
  • Wingspan: 33 ft 9 in (10.29 m)
  • Gross weight: 3006 lb (1366 kg)
  • Powerplant: 1 × Lycoming R-680-8 radial engine, 220 hp (164 kW)

    • Performance

  • Maximum speed: 108 mph (174 km/h)

    • References

    Spartan NP Wikipedia
    (Text) CC BY-SA


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