ANBO I
__NOTOC__
{{Infobox aircraft
|name=ANBO I
|image=Anbo1.jpg
|caption=
|type=Prototype trainer aircraft
|manufacturer=Karo Aviacijos Tiekimo Skyrius
|designer=Antanas Gustaitis
|first_flight= 14 July 1925
|introduction=
|retired=1935
|status=
|primary_user=
|more_users=
|produced=
|number_built=1
|variants=
|developed_into=ANBO II
}}
The ANBO I was a single-seat aircraft developed in Lithuania, proposed as a trainer for the Lithuanian Army. It was a low-wing, braced monoplane of conventional tailwheel configuration. The fuselage structure was of fabric-covered welded steel tube, The wing had a wooden, two-spar structure and was fabric covered but the fuselage, also fabric covered, had a welded steel tube structure.
The first flight took place in 1925. Ten years later the aircraft was sold to the Lithuanian Aviation Museum in Kaunas where it is exhibited today.
Operators
;{{flag|Lithuania|1918}}
Specifications
File:Anbo_I_3-view_L'Air_January_15,_1926.png
File:LAM 2008-09 Anbo-1.jpg in Kaunas, Lithuania]]
{{Aircraft specs
|prime units?=met
|genhide=
|crew=One
|length m=5.75
|length note=
|span m=10
|span note=
|height m=1.95
|height note=
|wing area sqm=11.40
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=190
|empty weight note=equipped
|gross weight kg=300
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|35|kg|lb|abbr=on}} fuel and oil
|more general=
|eng1 number=1
|eng1 name=Anzani
|eng1 type=3-cylinder radial
|eng1 hp=40
|more power=
|prop blade number=2
|prop name=Dorand
|prop dia m=1.90
|prop dia note=
|perfhide=
|max speed kmh=142
|max speed note= at ground level
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=4 hr
|ceiling m=4200
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=7 min to {{convert|1000|m|ft|abbr=on}}
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
- Take-off distance: {{convert|30|m|ft|abbr=on}}
- Landing distance: {{convert|40|m|ft|abbr=on}}
}}
References
{{reflist|refs=
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{{commons category}}
Further reading
- {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London }}
{{ANBO aircraft}}
Category:Single-engined tractor aircraft
Category:1920s Lithuanian military trainer aircraft