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Evolved in parallel with the D 9 as a contender in the
1923 C1 programme, in which it was eventually to take
third place after the Nieuport-Delage 42 and the Gourdou-
Leseurre 32, the D 12 differed essentially in engine
type. Possessing a basically similar fuselage to that of
the D 1, the D 12 was powered by a 450hp Lorraine-
Dietrich 12EW 12-cylinder W-type water-cooled engine.
First flown, like the D 9, in June 1924, the D 12 had an
armament of two 7.7mm Vickers guns, and, in September, was fitted with a higher compression ratio 12Eb
engine and a pair of 7.5mm Darne modele 19 guns on
the wing centre section. The paired Lamblin radiators
on the undercarriage legs gave place to a frontal
radiator and a wing similar to that finally adopted on
the D 9 was fitted. On 5 February 1926, the D 12 was
written off in an accident at Cazaux. A second prototype
had meanwhile entered flight test, having flown at
the end of 1925, this having a W-type Hispano-Suiza
12Gb engine, but further development was discontinued.
| WEIGHTS |
| Take-off weight | 1636 kg | 3607 lb |
| Empty weight | 1070 kg | 2359 lb |
| DIMENSIONS |
| Wingspan | 12.80 m | 41 ft 12 in |
| Length | 7.60 m | 24 ft 11 in |
| Height | 3.00 m | 9 ft 10 in |
| Wing area | 25.00 m2 | 269.10 sq ft |
| PERFORMANCE |
| Max. speed | 239 km/h | 149 mph |
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