IAR-824

__NOTOC__ Infobox Aircraft
name=IS-24, IAR-824


caption=
type=Civil utility aircraft
national origin=Romania
manufacturer=ICA, IAR
designer=Iosif Silimon
first flight=avyear|1971
introduced=
retired=
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produced=
number built=
variants with their own articles=The IAR-824 (originally known as the ICA IS-24) was a utility aircraft built in Romania in the 1970s. Developed from the ICA IS-23A, it was a conventional high wing cantilever monoplane with fixed tricycle undercarriage and seating for six people within an enclosed cabin. A small number were built, with five going to Romania's Aeroclub for training and glider towing.

pecifications

aerospecs
ref=
met or eng?= met

crew=One pilot
capacity=5 passengers
length m=9.20
length ft=30
length in=2
span m=12.40
span ft=40
span in=8
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=3.30
height ft=10
height in=10
wing area sqm=23.6
wing area sqft=254
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=1,240
empty weight lb=2,730
gross weight kg=1,900
gross weight lb=4,100
lift kg=
lift lb=

eng1 number=1
eng1 type=Lycoming IO-540-G1D5
eng1 kw= 290
eng1 hp= 215
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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eng2 kw=
eng2 hp=
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max speed kmh=200
max speed mph=125
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=800
range miles=500
endurance h=
endurance min=
ceiling m=3,000
ceiling ft=9,800
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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References

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* [http://www.airwar.ru/enc/la/iar824.html Уголок неба]