ANBO V

__NOTOC__ Infobox Aircraft
name=ANBO V


caption=
type=Military trainer
manufacturer=Karo Aviacijos Tiekimo Skyrius
designer=Antanas Gustaitis
first flight=1931
introduced=
retired=
status=
primary user=
more users=
produced=
number built=15
variants with their own articles=

The ANBO V was a parasol-wing monoplane training aircraft designed for the Lithuanian Army in 1931. It was of conventional configuration with fixed, tailwheel undercarriage. The pilot and instructor sat in tandem open cockpits. The prototype was powered by a Walter Vega I engine, but the small series produced had either Walter Venus or Armstrong Siddeley Genet Major engines.

In 1936, an improved version appeared, designated ANBO 51, all Genet-powered and featuring strengthened wings.

pecifications (ANBO 51)

aerospecs
met or eng?= met

crew=two, pilot and instructor
capacity=
length m=7.30
length ft=23
length in=11
span m=11.35
span ft=37
span in=3
dia m=
dia ft=
dia in=
height m=
height ft=
height in=
wing area sqm=20.7
wing area sqft=222
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=680
empty weight lb=1,500
gross weight kg=950
gross weight lb=2,090

eng1 number=1
eng1 type=Armstrong Siddeley Genet Major IV
eng1 kw= 120
eng1 hp= 160
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=200
max speed mph=125
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=4,000
ceiling ft=13,100
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
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armament5=
armament6=

References

*
* [http://www.lam.lt/old/istorija/karo_aviacija/gustaicio/anbo5/nfra5en.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=