ASJA Viking II

__NOTOC__ Infobox Aircraft
name=Viking II


caption=
type=Utility aircraft
manufacturer=ASJA
designer=
first flight=
introduced=
retired=
status=
primary user=
more users=
produced=
number built=
variants with their own articles=

The ASJA Viking II was a four-seat light aircraft built in Sweden in the early 1930s. It was a development of the Viking, a high-wing braced cabin monoplane of taildragger configuration. It was available with either wheeled or float undercarriage.

pecifications

aerospecs
met or eng?= met

crew=one pilot
capacity=2-3 passengers
length m=
length ft=
length in=
span m=
span ft=
span in=
dia m=
dia ft=
dia in=
height m=
height ft=
height in=
wing area sqm=
wing area sqft=
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=
gross weight lb=

eng1 number=1
eng1 type=de Havilland Gipsy Six inline engine
eng1 kw= 150
eng1 hp= 200
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=
max speed mph=
range km=
range miles=
endurance h=
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

*

ee also

aircontent

related=

similar aircraft=

sequence=

lists=

see also=