Fanaero-Chile Chincol

Fanaero-Chile Chincol

__NOTOC__ Infobox Aircraft

first flight=14 December 1955
primary user=
more users=
number built=
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The Fanaero-Chile Chincol (named for a South American sparrow) was a prototype trainer aircraft developed in Chile in 1955 for air force use. It was a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage. The pilot and instructor sat in tandem, and were enclosed under a long canopy. The Chilean Air Force responded positively to the design, and placed an order for 50 machines. However, technical problems significantly delayed manufacture, and the order was cancelled before the aircraft were produced.


met or eng?= met

crew=Two, pilot and instructor
length m=7.22
length ft=23
length in=8
span m=10.40
span ft=34
span in=1
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
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width m=
width ft=
width in=
height m=2.10
height ft=6
height in=11
wing area sqm=15.7
wing area sqft=169
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=740
empty weight lb=1,630
gross weight kg=1,050
gross weight lb=2,310
lift kg=
lift lb=

eng1 number=1
eng1 type=Continental O-470
eng1 kw= 160
eng1 hp= 215
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
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max speed kmh=210
max speed mph=130
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=650
range miles=400
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=4.1
climb rate ftmin=807
sink rate ms=
sink rate ftmin=

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* [ Уголок неба]

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