- Design and development
- Specifications (Albar Albarian)
- See also
- References
- External links
| name=Albarian | image= | caption= }}{{Infobox Aircraft Type | type=Homebuilt aircraft | national origin=United States | manufacturer= | designer=Lavigne Albar | first flight= | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from=Luscombe | variants with their own articles=
}} |
The Albar Albarian is an American aircraft designed for homebuilt construction. Design and developmentThe Albarian is a two place, single engine, strut-braced, high wing aircraft with conventional landing gear. The fuselage is constructed of welded steel tubing with aircraft fabric covering. The wings are sourced from a Luscombe 8 with flap modifications for STOL performance.[1] Specifications (Albar Albarian) {{Aircraft specs
|ref=Air Progress
|prime units?=kts
|genhide=
|crew=1
|capacity=1
|length m=
|length ft=22
|length in=
|length note=
|span m=
|span ft=35
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=675
|empty weight note=
|gross weight kg=
|gross weight lb=995
|gross weight note=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Continental C-90B
|eng1 type=horizontally opposed piston aircraft engine
|eng1 kw=
|eng1 hp=90
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|perfhide=
|max speed kmh=
|max speed mph=140
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=105
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=38
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=950
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
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|avionics=
}}
See also{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}References1. ^{{cite journal|title=none|magazine=Air Progress|date=Winter 1969|page=8}}
External links 1 : Homebuilt aircraft |