The N.3201 was designed for an official competition for a tandem two-seat primary trainer for the government-sponsored flying schools.
The N.3201 first flew on 22 June 1954, powered by a 170 hp SNECMA-Regnier engine.
The N.3200 prototype first flew on 10 September 1954, powered by a 260 hp Salmson-Argus 8AS-03 engine.
Apart from the engine installed, both models are identical,
N.3200
Engine: Salmson-Argus 8AS-03, 260 hp
Wingspan: 32 ft 1.5 in
Length: 26 ft 2.5 in
Height: 10 ft 2.75 in
N.3201
Engine: SNECMA-Regnier, 170 hp
Wingspan: 32 ft 1.5 in
Length: 26 ft 2.5 in
Height: 10 ft 2.75 in
Empty weight: 1742 lb
Loaded weight: 2405 lb
Max speed: 150 mph at SL
Cruise: 124 mph
ROC: 984 fpm
Endurance: 2 hr
All Aero 