History

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.

Technical information
Dimensions:
Length: 9,5 m Wingspan: 12 m
Height: 4,25 m Wing area: 31 m2
Weights:
Empty weight: 1320 kg Max. start weight: 1950 kg
Performances:
Max. speed: 230 km/hr Climbing speed: - m/min
Cruising speed: 190 km/hr    
Range: 4800 m Service ceiling: - m
Miscellaneous:
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