ANBO I

__NOTOC__ Infobox Aircraft
name=ANBO I


caption=
type=Prototype trainer aircraft
manufacturer=Karo Aviacijos Tiekimo Skyrius
designer=Antanas Gustaitis
first flight=1925
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=

The ANBO I was a single-seat aircraft developed in Lithuania as a trainer for the Army. It was a low-wing, braced monoplane of conventional tailwheel configuration. The fuselage structure was of fabric-covered welded steel tube, and the wing structure was of fabric-covered wood.

pecifications

aerospecs
met or eng?= met

crew=one pilot
capacity=
length m=5.75
length ft=18
length in=10
span m=10.00
span ft=32
span in=10
dia m=
dia ft=
dia in=
height m=
height ft=
height in=
wing area sqm=11.4
wing area sqft=123
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=190
empty weight lb=420
gross weight kg=300
gross weight lb=660

eng1 number=1
eng1 type=Anzani radial engine
eng1 kw= 26
eng1 hp= 35
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=142
max speed mph=89
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=4,200
ceiling ft=13,800
glide ratio=
climb rate ms=2.8
climb rate ftmin=550
sink rate ms=
sink rate ftmin=

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

References

*
* [http://www.lam.lt/old/istorija/karo_aviacija/gustaicio/anbo1/nfra1en.htm Lithuanian Aviation Museum]

ee also

aircontent

related=

similar aircraft=

sequence= ANBO I -
ANBO II -
ANBO III -
ANBO IV -
ANBO V -
ANBO VI -
ANBO VII -
ANBO VIII

lists=

see also=