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Fairchild 21

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First flight
  
1928

Designer
  
Manufacturer
  
Fairchild 21 httpsuploadwikimediaorgwikipediacommonsthu

The Kreider-Reisner KR-21-A was a 1928 American two-seat monoplane. They were designed and built by the Kreider-Reisner Aircraft Company of Hagerstown, Maryland. Fairchild Aircraft took over Kreider-Reisner in 1929 and continued to build them, as the Fairchild KR-21, later the Fairchild 21.

Contents

Design and development

The KR-21-A was a low-wing braced monoplane with two open tandem cockpits and powered by an 80 hp (60 kW) Armstrong Siddeley Genet radial piston engine. It was of mixed construction and had a fixed tailwheel landing gear and was fitted with dual controls.

The KR-21-B was a more powerful biplane development, using a 125 bhp Kinner B-5 engine. Five were produced, three built as -B models and two converted from the -A.

At least three, most of the production, survive today

  • NC107M
  • NC236V
  • NC954V
  • The KR-21 would in turn form the basis of the KR-22 parasol-wing monoplane design.

    Specifications ( -A )

    Data from

    General characteristics

  • Crew: 2
  • Length: 21 ft 6 in (6.55 m)
  • Wingspan: 28 ft 3 in (8.61 m)
  • Wing area: 139 sq ft (12.9 m2)
  • Empty weight: 755 lb (342 kg)
  • Max takeoff weight: 1,250 lb (567 kg)
  • Powerplant: 1 × Armstrong Siddeley Genet 5-cylinder radial piston engine, 80 hp (60 kW)
  • Performance

  • Maximum speed: 105 mph (169 km/h; 91 kn)
  • Cruise speed: 90 mph (145 km/h; 78 kn)
  • Range: 425 mi (369 nmi; 684 km)
  • Service ceiling: 9,440 ft (2,880 m)
  • References

    Fairchild 21 Wikipedia


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