FMA AeC.1

__NOTOC__ Infobox Aircraft
name=AeC.1


caption=
type=Utility aircraft
manufacturer=FMA
designer=
first flight=28 October avyear|1931
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The FMA AeC.1 was a light utility aircraft built in Argentina in 1931; it was the first aircraft of domestic design to be produced by FMA. It was a low-wing cantilever monoplane of conventional configuration with fixed tailskid undercarriage. As originally designed, the fully enclosed cabin had three seats, but this was later reduced to two. The passenger seat could be readily removed to make way for a stretcher to facilitate its use as an air ambulance.

pecifications

aerospecs
ref=
met or eng?= met

crew=One pilot
capacity=2 passengers
length m=7.75
length ft=25
length in=5
span m=12.00
span ft=39
span in=4
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=3.16
height ft=10
height in=4
wing area sqm=16.9
wing area sqft=182
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=700
empty weight lb=1,540
gross weight kg=1,120
gross weight lb=2,470
lift kg=
lift lb=

eng1 number=1
eng1 type=Armstrong Siddeley Mongoose
eng1 kw= 112
eng1 hp= 150
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=180
max speed mph=110
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,300
range miles=810
endurance h=
endurance min=
ceiling m=4,300
ceiling ft=14,100
glide ratio=
climb rate ms=3.3
climb rate ftmin=660
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

aircontent
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similar aircraft=
lists=

References

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