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Designed by a team led by Dr-Ir Erich Schatzki and retaining
traditional Fokker-type mixed construction, the
D XXI was conceived in answer to a specification formulated
by the KNIL (Koninklijk Nederlands Indisch
Leger), the aviation element of the Royal Netherlands
Indies Army, and was flown as a prototype on 27
February 1936. In the event, the initial production order
was placed by the Finnish government, which acquired
a manufacturing licence, a contract subsequently
being issued in the Netherlands on behalf of the homebased
LVA (Luchtvaartafdeling). The latter purchased
36 D XXIs powered by the 825hp Bristol Mercury VIII
nine-cylinder radial engine and armed with four wing-mounted
7.9mm FN-Browning M.36 guns. Seven were
acquired from the parent company by Finland, with delivery
flights commencing 27 August 1937, and a
further 35 were licence-built by VL (Valtion Lentokonetehdas), these being armed with four 7.7mm Brownings,
two being fuselage mounted, and having PZL- or
Tampella-built Mercury VII engines of 840hp. Two D
XXIs were purchased by Denmark which subsequently
licence-built a further 10, these mounting a pair of
20mm Madsen cannon and two 7.9mm machine guns,
and licence manufacture was also initiated in Spain by
Hispano Aviacion, assembly being undertaken at the
SAF-15 factory at La Rabasa, Alicante. At least one D
XXI was completed and flown in Spain with a Soviet
M-25 engine taken from an I-16 before the production
facility was overrun by Nationalist forces. At that time,
50 sets of wings, 25 fuselages and 25 undercarriages
for D XXIs were discovered. The D XXI was offered by
Fokker with various engines, including the Pratt &
Whitney Twin Wasp Junior, and the basic D XXI was
further developed with this engine in Finland by VL. The last Finnish-built Mercury-engined D
XXI was fitted with a Finnish-designed retractable
undercarriage after suffering a landing accident. It was
test flown on 19 June 1941, the fixed gear being restored
after another landing accident a month later.
| WEIGHTS |
| Take-off weight | 2 050 kg | 4 lb |
| Empty weight | 1450 kg | 3197 lb |
| DIMENSIONS |
| Wingspan | 11.00 m | 36 ft 1 in |
| Length | 8.20 m | 26 ft 11 in |
| Height | 2.95 m | 9 ft 8 in |
| Wing area | 16.20 m2 | 174.38 sq ft |
| PERFORMANCE |
| Max. speed | 460 km/h | 286 mph |
| Range | 930 km | 578 miles |
 | A three-view drawing (1280 x 952) |
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