Ikarus 214

__NOTOC__ Infobox Aircraft
name=214


caption=
type=Military trainer
national origin=Yugoslavia
manufacturer=Ikarus
designer=Sima Milutinović
first flight=avyear|1949
introduced=
retired=
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primary user=
more users=
produced=
number built=21
variants with their own articles=The Ikarus 214 was a military aircraft produced in Yugoslavia in the early 1950s. Originally intended as a light reconnaissance-bomber (first prototype flight in 1949), it was produced as a trainer and transport aircraft Ikarus 214D when the flight testing of the prototype revealed it to have insufficient performance for the role. The Ikarus 214D first flew in avyear|1951. The 214 was a conventional, low-wing cantilever monoplane with twin tail and retractable tailwheel undercarriage. The twin engines were mounted on nacelles on the wings, and originally Ranger SVG-770s were fitted, although this was changed to the Pratt & Whitney R-1340-AN-1 in production.

pecifications

aerospecs
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crew=One or two pilots
capacity=8 passengers
length m=11.20
length ft=38
length in=9
span m=16.20
span ft=53
span in=2
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width m=
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height m=3.95
height ft=13
height in=0
wing area sqm=29.80
wing area sqft=321
swept area sqm=
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volume m3=
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aspect ratio=
empty weight kg=3,965
empty weight lb=3,741
gross weight kg=5,025
gross weight lb=11,078
lift kg=
lift lb=

eng1 number=2
eng1 type=Pratt & Whitney R-1340-AN-1
eng1 kw= 450
eng1 hp= 600
eng1 kn=
eng1 lbf=
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eng2 number=
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max speed kmh=365
max speed mph=227
max speed mach=
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range km=1,080
range miles=670
endurance h=
endurance min=
ceiling m=7,000
ceiling ft=23,000
glide ratio=
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climb rate ftmin=
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armament1=
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armament6= aircontent
see also=
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similar aircraft=
*Siebel Si 204
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References

*
* [http://www.airwar.ru/enc/other/214.html Уголок неба] (Ugolok Neba) ru icon

External links

* [http://www.airwar.ru/enc/other/214.html Photos at Уголок неба]