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.
| 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 | ||
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