Variants
Data from:
- NC.210
- The initial design powered by 4x 1,641 kW (2,200 hp) Gnome-Rhône 18R 18-cylinder radial engines. Not built.
- NC.211
- The proposed production aircraft powered by 4x 1,193 kW (1,600 hp) SNECMA 14R 14-cylinder radial engines. One prototype and one production aircraft completed with nine more partially completed.
- NC.212
- A proposed version to have been powered by 4x 1,476 kW (1,980 hp) Bristol Hercules 730 14-cylinder sleeve-valve radial engines.
- NC.213
- A proposed version to have been powered by 4x 1,305 kW (1,750 hp) Junkers Jumo 213 inverted V-12 engines.
Read more about this topic: SNCAC NC 211
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