AISA GN

__NOTOC__ Infobox Aircraft
name=GN


caption=
type=Autogyro
manufacturer=AISA
designer=
first flight=1982
introduced=
retired=
status=
primary user=
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produced=
number built=1
variants with their own articles=

The AISA GN was a prototype four-seat autogyro developed in Spain between 1974 and 1982. it featured an extensively-glazed cabin fitted with a pusher engine and tricycle undercarriage. A separate tail fin was carried at the end of two booms. The aircraft suffered from an extremely prolonged development, but finally took to the air on 20 July 1982. Shortly thereafter, however, it was damaged and finally abandoned.

pecifications

aerospecs
met or eng?= met

crew=one pilot
capacity=3 passengers
length m=6.50
length ft=21
length in=4
span m=
span ft=
span in=
dia m= 12.8
dia ft= 43
dia in= 0
height m=3.2
height ft=10
height in=6
wing area sqm=
wing area sqft=
rot area sqm= 128.7
rot area sqft= 1,390
aspect ratio=
empty weight kg=708
empty weight lb=1,560
gross weight kg=1,200
gross weight lb=2,650

eng1 number=1
eng1 type=Lycoming IO-540-K1A5
eng1 kw= 225
eng1 hp= 300
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=240
max speed mph=150
range km=800
range miles=500
endurance h=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
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armament4=
armament5=
armament6=

References

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ee also

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