Advanced Aviation Cobra
{{Infobox aircraft
|name=Cobra
|image=
|caption=
|type=Homebuilt ultralight aircraft
|manufacturer=Advanced Aviation
|designer=
|first_flight=1980s
|introduction=
|retired=
|status=
|primary_user=
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|produced=
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|developed_from= Eipper Quicksilver
|variants=
}}
The Advanced Aviation Cobra was a U.S. ultralight aircraft of extremely minimalist design marketed for homebuilding, developed from the Advanced Aviation Husky. The pilot is seated in an open framework suspended beneath a fabric-covered wing on which the engine (adapted from a snowmobile) and pusher propeller are also mounted. Early Cobras (Model A) had spoilers for roll control, while the Model B had traditional full three-axis control using ailerons. A two-seat training version, known as the King Cobra was also available.Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-11. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}
Specifications (Model B)
{{Aircraft specs
|prime units?=imp
|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|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=152
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=235
|empty weight note=
|gross weight kg=
|gross weight lb=525
|gross weight note=
|fuel capacity={{convert|4.8|u.s.gal}}
|more general=
|eng1 number=1
|eng1 name=Cuyuna 430R
|eng1 type=twin cylinder, two-stroke engine with reduction drive
|eng1 kw=
|eng1 hp=30
|eng1 shp=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
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|prop note=
|perfhide=
|max speed kmh=
|max speed mph=65
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=55
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=24
|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=130
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=9900
|ceiling note=
|g limits=
|roll rate=
|glide ratio=9:1
|climb rate ms=
|climb rate ftmin=1000
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
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|avionics=
}}
{{Aircontent
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References
{{Reflist}}
{{Advanced Aviation aircraft}}
Category:1980s United States ultralight aircraft