- Design and development
- Specifications (Phoenix)
- External links
| name=Freedom Aviation Phoenix | image=Phoenixaircraft1.jpg | caption= }}{{Infobox Aircraft Type | type=Utility aircraft | manufacturer=Freedom Aviation for homebuilding | designer=Freedom Aviation | first flight=20 August 2007 | introduced=26 April 2007 | retired= | status= | primary user= | more users= | produced= | number built= | variants with their own articles=
}} |
The Freedom Aviation Phoenix was a single-engine four-seat American airplane that was sold as a homebuilt composite canard aircraft. The kit was produced at a facility on St. Lucie County International Airport at Ft. Pierce, Florida. Design and developmentThe Phoenix airframe was formed of carbon-fiber composite materials on factory molds. The aircraft was assembled as a homebuilt, with a factory-sponsored builder-assist program available. The aircraft has a swept, dihedral canard mounted ahead of the cabin, and a swept main lifting surface. Each wing has a fin (with full-length rudder) mounted about midway to the tip. In addition, the wingtips have swept winglets, which provide additional yaw stability while decreasing induced drag. The Phoenix is powered by a six-cylinder horizontally-opposed piston engine driving a pusher propeller. The tricycle landing gear is retractable. Only one aircraft was ever built, and the company has since gone out of business. Specifications (Phoenix){{Aircraft specs
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|crew=1
|capacity=3 pax / maximum {{convert|1500|lb|kg|abbr=on}} / {{convert|750|lb|kg|abbr=on}} with full fuel
|length m=6.86
|length ft=
|length in=
|length note=
|span m=10.49
|span ft=
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|span note=
|height m=2.21
|height ft=
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|wing area sqm=
|wing area sqft=
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|swept area sqm=
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|volume m3=
|volume ft3=
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|empty weight lb=
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|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|125|USgal|impgal l|abbr=on}}
|lift kg=
|lift lb=
|lift note=
|more general=
- Cabin width: {{convert|50|in|mm|abbr=on}}
- Cabin height: {{convert|44|in|mm|abbr=on}}
- Cabin length: {{convert|129|in|mm|abbr=on}}
|eng1 number=1
|eng1 name=Continental IO-550
|eng1 type=6-cylinder horizontally-opposed air-cooled piston engine
|eng1 kw=
|eng1 hp=310
|eng1 shp=
|eng1 kn=
|eng1 lbf=
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|power original=
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|max speed kmh=
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|max speed kts=
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|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=185
|cruise speed note= at 65% power
|stall speed kmh=
|stall speed mph=
|stall speed kts=70
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=215
|never exceed speed note= IAS
|minimum control speed kmh=
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|minimum control speed kts=
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|range km=
|range miles=
|range nmi=1400
|range note=with 30 minute reserve
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|climb rate ms=6.6
|climb rate ftmin=
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|lift to drag=
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|disk loading kg/m2=
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|fuel consumption kg/km=
|fuel consumption lb/mi=0.423
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}}
External links- [https://web.archive.org/web/20100923093106/http://freedom-aviation.com/ Manufacturer's website via archive.org]
7 : United States civil utility aircraft 2000–2009|Homebuilt aircraft|Canard aircraft|Freedom Aviation aircraft|Twin-boom aircraft|Single-engined pusher aircraft|Aircraft first flown in 2007 |