- Focke-Wulf F 19
__NOTOC__ Infobox Aircraft
name=F 19 Ente
caption=
type=Civil utility aircraft
manufacturer=Focke-Wulf
designer=
first flight=2 September avyear|1927
introduced=
retired=
status=
primary user=
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produced=
number built=2
variants with their own articles=The Focke-Wulf F 19 "Ente" (German: "Duck") was a light aircraft of unusual design built in Germany in the late 1920s. It was a high-wing monoplane with a canard layout and fixed tricycle undercarriage. The pilot sat in an open cockpit, while an enclosed cabin was provided for the passengers. The canard was mounted on short struts above the nose of the aircraft, ahead of the cockpit, and the twin engines were housed in nacelles carried in struts under the wings.The first example flew on 2 September 1927, but crashed on 29 September during a demonstration of single-engine flight. Focke-Wulf co-founder
Georg Wulf had been at the controls, and was killed in the crash, the cause of which was found to have been a control rod that snapped during the display. Nevertheless, a second aircraft was built, which flew in late 1930. This was used for a promotional tour of Europe the following year that took it to Denmark, Sweden, the Netherlands, Belgium, and the UK. Afterwards, it was put on display at theDeutsche Luftfahrtsammlung , where it was destroyed in an Allied air raid in 1944.pecifications
aerospecs
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met or eng?= metcrew=One pilot
capacity=3 passengers
length m=10.53
length ft=34
length in=7
span m=10.00
span ft=32
span in=9
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=4.15
height ft=13
height in=7
wing area sqm=29.5
wing area sqft=318
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=1,175
empty weight lb=2,590
gross weight kg=1,650
gross weight lb=3,638
lift kg=
lift lb=eng1 number=2
eng1 type=Siemens Sh 14
eng1 kw= 82
eng1 hp= 110
eng1 kn=
eng1 lbf=
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eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
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eng2 lbf-ab=max speed kmh=142
max speed mph=88
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=3,000
ceiling ft=9,840
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
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armament6=aircontent
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lists=References
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