Editing Advanced Aviation Cobra

<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{{Infobox aircraft
 |name=Cobra
 |image=
 |caption=
 |type=[[Homebuilt aircraft|Homebuilt]] [[ultralight aviation|ultralight aircraft]]
 |manufacturer=[[Advanced Aviation]]
 |designer=
 |first_flight=1980s
 |introduction=
 |retired=
 |status=
 |primary_user=
 |more_users=
 |produced=
 |number_built=
 |unit cost=
 |developed_from= [[Eipper Quicksilver]]
 |variants=
}}
The '''Advanced Aviation Cobra''' was a U.S. [[ultralight aviation|ultralight aircraft]] of extremely minimalist design marketed for [[homebuilt aircraft|homebuilding]], developed from the [[Advanced Aviation Husky]]. The pilot is seated in an open framework suspended beneath a fabric-covered wing on which the [[Piston engine|engine]] (adapted from a [[snowmobile]]) and [[pusher configuration|pusher propeller]] are also mounted. Early Cobras ('''Model A''') had [[Spoiler (aeronautics)|spoilers]] for roll control, while the '''Model B''' had traditional full three-axis control using [[aileron]]s. A two-seat [[Trainer (aircraft)|training version]], known as the '''King Cobra''' was also available.<ref name="Cliche">Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-11. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}</ref>

==Specifications (Model B)==
{{Aircraft specs
|ref=Cliche<ref name="Cliche" />
|prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, 
met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
        General characteristics
-->
|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=<!-- sailplanes -->
|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=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Cuyuna 430R]]
|eng1 type=twin cylinder, [[two-stroke]] engine with reduction drive
|eng1 kw=<!-- prop engines -->
|eng1 hp=30<!-- prop engines -->
|eng1 shp=<!-- prop engines -->

|prop blade number=<!-- propeller aircraft -->
|prop name=
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop note=

<!--
        Performance
-->
|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=<!-- if range unknown -->
|ceiling m=
|ceiling ft=9900
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=9:1
|climb rate ms=
|climb rate ftmin=1000
|climb rate note=
|time to altitude=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

<!-- ==See also== -->
{{Aircontent
|lists=

}}

==References==
{{Reflist}}

{{Advanced Aviation aircraft}}

[[Category:Homebuilt aircraft]]
[[Category:1980s United States ultralight aircraft]]
[[Category:Single-engined pusher aircraft]]
[[Category:Advanced Aviation aircraft|Cobra]]