- Indraéro Aéro 101
__NOTOC__ Infobox Aircraft
name=Aéro 101 and Aéro 110
caption=
type=Civil trainer
national origin=France
manufacturer=Indraéro
designer=Jean Chapeau and J. Blanchet
first flight=1 May avyear|1950
introduced=
retired=
status=
primary user=SALS
more users=
produced=
number built=13
variants with their own articles=The Indraéro Aéro 101 was a training biplane developed in France in the 1950s. It was a conventional design with single-bay staggered wings braced with an I-strut, and fixed tailskid undercarriage with divided main units. The pilot and instructor sat in tandem, open cockpits. A small batch of aircraft were ordered by SALS for aeroclub use, which differed from the prototype in having horizontally-opposedMinié 4 DC engines instead of aSalmson 9A radial.These were followed in 1951 by the Aéro 110, a generally similar design but where the Aéro 101's all-wooden structure was replaced by fabric-covered steel tube. Only a single prototype was built, again powered by a Salmson 9A.
pecifications (Aéro 101)
aerospecs
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met or eng?= metcrew=Two, pilot and instructor
capacity=
length m=5.60
length ft=18
length in=5
span m=7.60
span ft=24
span in=11
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=2.20
height ft=7
height in=3
wing area sqm=14.0
wing area sqft=151
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=312
empty weight lb=686
gross weight kg=505
gross weight lb=1,110
lift kg=
lift lb=eng1 number=1
eng1 type=Minié 4 DC-32
eng1 kw=
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eng1 kn=
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eng2 number=
eng2 type=
eng2 kw=
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eng2 lbf-ab=max speed kmh=178
max speed mph=111
max speed mach=
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cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
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sink rate ftmin=armament1=
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armament6=aircontent
see also=
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lists=References
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