Fokker D.XIV

__NOTOC__ Infobox Aircraft
name=D.XIV


caption=
type=Fighter
manufacturer=Fokker
designer=
first flight=28 March avyear|1925
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Fokker D.XIV was a fighter aircraft developed in the Netherlands in the mid 1920s but which was only produced as a single prototype. It was a low-wing, cantilever monoplane with fixed tailskid undercarriage, the basic concept of which was derived from the Fokker V.25 that had been developed during World War I. The pilot sat in an open cockpit aft of the wing's trailing edge. Flight testing revealed excellent performance, but development was ceased when the prototype crashed, killing the test pilot.

pecifications

aerospecs
ref=
met or eng?= met

crew=One pilot
capacity=
length m=7.90
length ft=25
length in=11
span m=10.76
span ft=35
span in=4
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=3.25
height ft=10
height in=8
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=950
empty weight lb=2,090
gross weight kg=1,350
gross weight lb=2,980
lift kg=
lift lb=

eng1 number=1
eng1 type=Hispano-Suiza 12Hb
eng1 kw= 440
eng1 hp= 590
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=274
max speed mph=170
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=7.1
climb rate ftmin=1,400
sink rate ms=
sink rate ftmin=

armament1=2 × fixed, forward-firing 7.9 mm machine guns
armament2=
armament3=
armament4=
armament5=
armament6= aircontent
see also=
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similar aircraft=
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References

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* [http://www.airwar.ru/enc/fww1/fokd14.html Уголок неба]