Gabardini Lictor

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 by Alfa Romeo. Development was abandoned at the same time as the firm was absorbed by Fiat in early 1936.

pecifications (Lictor 130)

aerospecs
met or eng?= met

crew=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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sequence=

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