Nord Norélan
| Norélan | |
|---|---|
| |
| Nord 1223 Norélan No. 02 F-BFDU at Meaux - Esbly airfield in June 1969 | |
| Role | Three-seat light trainer |
| National origin | France |
| Manufacturer | Nord Aviation |
| First flight | Template:Avyear |
| Number built | 3 |
The Nord 1221 Norélan was a 1940s three-seat training monoplane designed and built in France by Nord Aviation.
Design and development
Designed as a three-seat trainer and first flown on 30 June 1948 the Norélan was a single-engined low-wing cantilever monoplane with a distinctive large dihedral angle to the wings. Originally to have a retractable tricycle landing gear the design was changed to a fixed tailwheel landing gear. A number of variants with different engines were produced but no production orders were received.
Variants
- 1221
- Prototype with 180hp (134kW) Mathis 8G-20 inverted Vee engine, later converted to 1222.
- 1222
- Prototype re-engined with a 180hp (134kW) Régnier 4L-02 inline engine
- 1223
- Powered by a 240hp (179kW) Argus As 10C inverted Vee engine, one built and prototype re-engined.
- 1226
- Engine-testbed for the 240hp (179kW) Potez 6D-0 inline engine. one built.
Specifications (1221)
General characteristics
- Crew: three
Performance
References
Wikimedia Commons has media related to Nord Aviation aircraft.