- Gabardini Lictor
__NOTOC__ Infobox Aircraft
name=Lictor
caption=
type=Civil utility aircraft
manufacturer=Gabardini
designer=
first flight=1935
introduced=
retired=
status=
primary user=
more users=
produced=
number built=2
variants with their own articles=The Gabardini Lictor was a light aircraft developed in Italy in the mid 1930s. It was a low-wing cantilever monoplane with fixed tailwheel undercarriage and a fully-enclosed cabin. Two versions were built, the Lictor 90 with a 90-hp Fiat engine, and that Lictor 130 with a 130-hp
de Havilland Gipsy Major engine built byAlfa Romeo . Development was abandoned at the same time as the firm was absorbed byFiat in early 1936.pecifications (Lictor 130)
aerospecs
met or eng?= metcrew=One pilot
capacity=2-3 passengers
length m=8.15
length ft=26
length in=8
span m=11.40
span ft=37
span in=5
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=
height ft=
height in=
wing area sqm=17.5
wing area sqft=188
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=650
empty weight lb=1,433
gross weight kg=1,000
gross weight lb=2,200
lift kg=
lift lb=eng1 number=1
eng1 type=Alfa Romeo 110
eng1 kw= 97
eng1 hp= 130
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=230
max speed mph=143
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6=References
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ee also
aircontent
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