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Intended to fulfil the demands of an October 1934
specification calling for a three-seat fighter to serve as
an aerial command post for single-seat fighters - a role
to which were subsequently added those of bomber
interception and escort - the R-110 was flown for the
first time on 30 March 1938. Of mixed construction, with
plywood-covered wooden wings and a welded steeltube
fuselage, the R-110 was powered by two 450hp
Renault 12 Ro 2/3 12-cylinder air-cooled engines and
carried an armament of two fixed 20mm cannon and a
single 7.5mm machine gun on a flexible mount in the
aft cockpit. The R-110 was unusual in that the pilot and
aircraft commander were seated behind separate vertically-
staggered stepped windscreens. The competing
Potez 630 had appeared in production form before the
R-110 prototype entered flight test and further development
of the latter was discontinued.
 | A three-view drawing (1280 x 838) |
| WEIGHTS |
| Take-off weight | 3 300 kg | 7 lb |
| Empty weight | 2165 kg | 4773 lb |
| DIMENSIONS |
| Wingspan | 12.80 m | 41 ft 12 in |
| Length | 9.66 m | 31 ft 8 in |
| Height | 3.37 m | 11 ft 1 in |
| Wing area | 24.00 m2 | 258.33 sq ft |
| PERFORMANCE |
| Max. speed | 470 km/h | 292 mph |
| Range | 1280 km | 795 miles |
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