North 3202
| North 3202 | |
|---|---|
 Modified Nord 3202 with a Lycoming boxer engine |
|
| Type: | Trainer aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
April 17, 1957 |
| Number of pieces: |
101 |
The Nord 3202 was a French trainer aircraft designed by Nord Aviation in the 1950s .
history
The Nord 3202 was developed on the basis of a tender by the French Army for a two-seater trainer and was intended to replace the Stampe SV.4 double-decker . A total of 101 copies were built. The first flight took place on April 17, 1957.
construction
Nord 3202B of the Association Nord & Co in La Ferté-Alais , 2010
The 3202 is a cantilever low wing aircraft with a fixed tail wheel landing gear and a closed tandem cockpit for students (front) and teachers (rear). It is driven by a piston engine. The one-piece and one-spar wing has a metal structure and is covered with fabric. A welded steel construction forms the fuselage structure, which is planked with metal in the front part and covered with fabric at the rear.
variants
- North 3200
- Prototype with a Salmson 8AS04 engine (240 hp , 179 kW)
- North 3201
- Prototype with a Regnier 4L22 engine (170 hp, 127 kW)
- North 3202
- Series model with a Potez 4D32 engine, 50 produced
- North 3202B
- Series model with a Potez 4D34 engine (260 hp, 194 kW), 50 produced
- North 3202B1B
- modified by Aérospatiale for the aerobatic team of the French army
- North 3212
- revised 3202 equipped with a radio compass for instrument flight training
Military users
Technical specifications
| Parameter | Data (Nord 3202B) |
|---|---|
| crew | 1 + 1 |
| length | 8.12 m |
| span | 9.5 m |
| height | 2.82 m |
| Wing area | 16.25 m² |
| Empty mass | 860 kg |
| Max. Takeoff mass | 1220 kg |
| Top speed | 259 km / h |
| Service ceiling | 4000 m |
| Range | 1000 km |
| Engines | 1 × Potez 4D34 , 190 kW (258 PS) |
Web links
Commons : Nord 3202 - Collection of images, videos and audio files
Individual evidence
- ^ Leonard Bridgman (Ed.): Jane's All The World's Aircraft - 1959-60. Sampson Low, Marston & Company Ltd., London 1959, p. 136.
- ↑ Data from Flugzeuginfo.net