- Operators
- Specifications
- References
- Further reading
| name=ANBO I | image=Anbo1.jpg | caption= }}{{Infobox Aircraft Type | type=Prototype trainer aircraft | manufacturer=Karo Aviacijos Tiekimo Skyrius | designer=Antanas Gustaitis | first flight= 14 July 1925 | introduced= | retired=1935 | 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, proposed 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, 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 Lithuanian Aviation Museum in Kaunas where it is exhibited today.[2][3] Operators- {{flag|Lithuania|1918}}
Specifications{{Aircraft specs
|ref=Les Ailes, November 1925
|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}}
}}References1. ^1 {{cite web|url=http://www.lam.lt/old/istorija/karo_aviacija/gustaicio/anbo1/nfra1en.htm |title=Latvian Air Force Museum, - ANBO I |accessdate=12 May 2017 |deadurl=bot: unknown |archiveurl=https://web.archive.org/web/20070927074530/http://www.lam.lt/old/istorija/karo_aviacija/gustaicio/anbo1/nfra1en.htm |archivedate=27 September 2007 }}
2. ^1 {{cite book |title=Aviation Museums and Collections of Mainland Europe |last= Ogden |first=Bob |coauthors= |edition= |year=2009|publisher= Air Britain (Historians) Ltd|page=357 |isbn=978 0 85130 418 2}}
}}{{commons category|ANBO I}}Further reading- {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= }}
{{ANBO aircraft}} 5 : Low-wing aircraft|Single-engined tractor aircraft|Lithuanian military trainer aircraft 1920–1929|ANBO aircraft|Aircraft first flown in 1925 |