The Nord Aviation 3202 Master was a 1950s French military trainer aircraft designed and built by Nord Aviation to meet a French Army requirement for a two-seat basic trainer, as a replacement for the biplane Stampe SV.4.

• Role: Two-seat trainer
• National origin: France
• Manufacturer: Nord Aviation
• First flight: 17 April 1957
• Retired: 1978
• Status: Privately owned, or in museums
• Operator: French Army
• Number built: 101

Specifications (N 3202B)

General characteristics

• Crew: two, pilot and instructor
• Length: 8.12 m (26 ft 8 in)
• Wingspan: 9.5 m (31 ft 2 in)
• Height: 2.82 m (9 ft 3 in)
• Wing area: 16.25 m² (175 ft²)
• Empty weight: 860 kg (1,895 lb)
• Maximum takeoff: 1,220 kg (2,690 lb)
• Powerplant: 1 × Potez 4D34, 190 kW (260 hp)

Performance

• Maximum speed: 260 km/h (160 mph)
• Range: 1,000 km (620 mi)
• Service ceiling: m ( ft)
• Rate of climb: m/min ( ft/min)