The Fokker C.XIVw was developed in 1938 as a successor of the Fokker C.VIIw to be used for reconaissance and advance trainer.
The aircraft was built in the usual manner, a steel tube fuselage, which was clothed with linen and wooden wings.
The Duthc Navy ordered twentyfour aircraft in mid-January 1939. All of which were delivered by the end of the year.
|Length:||9,5 m||Wingspan:||12 m|
|Height:||4,25 m||Wing area:||31 m2|
|Empty weight:||1320 kg||Max. start weight:||1950 kg|
|Max. speed:||230 km/hr||Climbing speed:||- m/min|
|Cruising speed:||190 km/hr|
|Range:||4800 m||Service ceiling:||- m|
|Engine type:||One Wright Whirlwind R-975-E3 rated 425 hp|
|Crew:||Two men: one aviator pus one observer|
|Armament:||Two 7,9 mm machine guns|
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