Nord 2100 Norazur

Nord 2100 Norazur
2100 Norazur
Role Ten-passenger transport monoplane
National origin France
Manufacturer Nord Aviation
First flight 1947
Number built 1

The Nord 2100 Norazur was a 1940s French civil transport monoplane designed and built at Courbevoie near Paris by SNCAN.[1][2]

Contents

Design and development

The Norazur was a high-wing cantilever monoplane with a retractable tricycle landing gear.[1] Powered by two wing-mounted Potez piston engines in pusher configuration.[1] It had an enclosed cabin for ten passengers or freight.[1]

Designed to meet a post-war requirement for a light transport and training aircraft the Norazur first flew at Les Moreuax on 30 April 1947.[2] An additional prototype with 390hp Bearn 6D-07 engines is believed to have been built.[2] With other similar designs available the type did not enter production.[2]

Variants

N2100
Prototype light transport with two 420hp Potez 8D-03 piston engines in pusher configuration, one built.[2]
N2101
Prototype with alternate 390hp Beard 6D-07 engines, believed to have been built.[2]
N2102
Projected variant with two Snecma 125 engines in tractor configuration.[2]

Specifications

Data from [2]

General characteristics

  • Crew: 2
  • Capacity: 10 passengers
  • Length: 13.5 m (44 ft 3 in)
  • Wingspan: 18.0 m (59 ft 1 in)
  • Height: 3.85 m (12 ft 8 in)
  • Wing area: 38 m2 (410 sq ft)
  • Empty weight: 3,280 kg (7,231 lb)
  • Gross weight: 4,630 kg (10,207 lb)
  • Powerplant: 2 × Potez 8D-03 piston engines in pusher configuration, 310 kW (420 hp) each

Performance

  • Maximum speed: 340 km/h (210 mph; 180 kn) at 1500m
  • Cruising speed: 312 km/h (194 mph; 168 kn) at 3000m
  • Range: 1,100 km (684 mi; 594 nmi)
  • Service ceiling: 6,500 m (21,325 ft)

References

Notes

Bibliography

  • French Post-War Transport Aircraft. Air-Britain. 1990. ISBN 0 85130 078 2. 
  • Photo of N-2100

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