Nord 2800
Nord Aviation · France · first flew 1950 · light aircraft
The Nord 2800 was a 1950s training monoplane designed and built in France by Nord Aviation.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Span of 12 metres on an 8.64 metre fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Low-wing light trainer monoplane
- Single Salmson 8As-00 engine in the nose
- Span of 12 metres on an 8.64 metre fuselage
A small all-metal three-seat trainer monoplane with a retractable tail-wheel landing gear and a 240 hp Salmson 8As-00 engine in the nose.
Specifications
- The Nord 2800 has a length of 8.64 m (28 ft).
- It has a wingspan of 12 m (39 ft).
- Its maximum speed is 265 km/h (165 mph).
- Typical crew: 3.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew on 4 August 1950.
Variants
Only one Nord 2800 was built.
Where you'll see it
It was a light trainer powered by a Salmson 8As-00 engine.
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