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 Mureaux on 30 April 1947.^[2] An additional prototype with 290 kW (390 hp) Béarn 6D-07 engines is believed to have been built.^[2] With other similar designs available the type did not enter production.^[2]

N2100

Prototype light transport with two 310 kW (420 hp) Potez 8D-03 inverted, air-cooled V-8 piston engines in pusher configuration,^[3] one built.^[2]

N2101

Prototype with alternate 290 kW (390 hp) Béarn 6D-07 inverted, air-cooled V-6 piston engines in pusher configuration,^[3] believed to have been built.^[2]

N2102

Projected variant with two SNECMA 12S engines in tractor configuration.^[2]

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 inverted V-8 piston engines in pusher configuration^[3], 310 kW (420 hp) each

Performance

• Maximum speed: 340 km/h (210 mph, 180 kn) at 1500m
• Cruise speed: 312 km/h (194 mph, 168 kn) at 3000m
• Range: 1,100 km (680 mi, 590 nmi)
• Service ceiling: 6,500 m (21,300 ft)

• Bridgman, Leonard (1950). Jane's All the World's Aircraft 1950-51. London: Sampson, Low, Marston and Co. Ltd. p. 150c.
• Chillon, Jacques; Dubois, Jean-Pierre & Wegg, John (1980). French Post-War Transport Aircraft. Tonbridge, UK: Air-Britain. ISBN 0-85130-078-2.
• Photo of N-2100