| At the end of 1925, the second prototype D 12 single-seat
fighter was re-engined with a 500hp Hispano-
Suiza 12Gb (HS 50) 12-cylinder W-type water-cooled
engine and redesignated D 21. Intended essentially for
export, the D 21 was first demonstrated in January 1926
at Bruxelles-Evere. The first export contract came from
Turkey, this calling for two D 21s for evaluation.
Czechoslovakia ordered three and Argentina procured
18, plus the prototype. Of these, the three Czech aircraft
and seven of the Argentine aircraft were assembled by
the EKW in Switzerland. A manufacturing licence was
obtained by Czechoslovakia, Skoda building 26 D 21s
during 1928-29 (as Skoda D 1s) with Skoda L engines
(derived from the HS 12G) of 562hp. Argentina also procured
a manufacturing licence and the Fabrica Militar
de Aviones (FMA) built 40 examples during 1930-31,
but with Madsen machine guns and the licence-built
Lorraine-Dietrich 12Eb W-type engine. They thus became effectively D 12s, although the designation D 21
was retained. In the autumn of 1927, Turkey placed a
follow-on order for 10 D 21s, these being delivered
during 1928-29.
WEIGHTS |
Take-off weight | 1580 kg | 3483 lb |
Empty weight | 1090 kg | 2403 lb |
DIMENSIONS |
Wingspan | 12.80 m | 42 ft 0 in |
Length | 7.64 m | 25 ft 1 in |
Height | 3.00 m | 10 ft 10 in |
Wing area | 24.80 m2 | 266.94 sq ft |
PERFORMANCE |
Max. speed | 270 km/h | 168 mph |
EzequielLuque, e-mail, 22.04.2007 10:40 Por favor, información detallada sobre desempeño D-510 o similares en China y de los D-21 en Argentina. Muchas gracias. reply |
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