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After the partial destruction of the H.220, major redesign
was initiated by the Societe Nationale de Constructions
Aeronautiques du Centre, or SNCA du
Centre, which had absorbed the Hanriot facility at
Bourges on 1 February 1937. The oval-section monocoque
fuselage of the original H.220 was discarded in
favour of a fuselage built as two half shells mated by a
central keel. An entirely new tail assembly with twin
endplate vertical surfaces was fitted and the Gnome-Rhone 14M radial engines were enclosed by low-drag
nacelles. These features were mated with the wing of
the original H.220 to result in the H.220-2, which was
first flown (as the H.220 No 02) on 17 March 1939. Four
months later, in July 1939, this prototype was to be displayed
statically as the NC 600 No 01 multi-seat fighter
at the Salon de l'Aeronautique. In fact, the genuine NC
600 was to differ from the H.220-2 in several major respects.
| WEIGHTS |
| Take-off weight | 3850 kg | 8488 lb |
| Empty weight | 2820 kg | 6217 lb |
| DIMENSIONS |
| Wingspan | 12.80 m | 42 ft 0 in |
| Length | 7.87 m | 26 ft 10 in |
| Height | 3.40 m | 11 ft 2 in |
| Wing area | 21.16 m2 | 227.76 sq ft |
| PERFORMANCE |
| Max. speed | 532 km/h | 331 mph |
| Range | 770 km | 478 miles |
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