Thatcher CX5
| {{Infobox aircraft begin
| name=CX5 | image= | caption= }}{{Infobox aircraft type | type=Homebuilt aircraft | national origin=United States | manufacturer= | designer=Dave Thatcher | first flight=17 December 2013 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Thatcher CX5 is an American homebuilt aircraft that was designed by Dave Thatcher.
Development
The CX5 is a two place, all metal, low-wing, tricycle gear-equipped aircraft. The prototype aircraft is outfitted with a Revmaster R-2300. The wings have upturned outer sections for dihedral.{{cite web|title=Dave Thatcher's CX5 Flies for the First Time|url=http://www.eaa.org/news/2013/2013-12-18_dave-thatchers-cx5-flies-for-the-first-time.asp|accessdate=27 December 2013}}{{cite web|url=http://www.flyingmag.com/aircraft/experimental-aircraft-homebuilts/thatcher-cx5-makes-first-flight|accessdate=27 December 2013|title=Thatcher CX5 Makes First Flight|date=19 December 2013 }}
Specifications (CX5)
{{Aircraft specs
|ref=EAA, Flying Magazine
|prime units?=kts
|genhide=
|crew= 2 tandem
|capacity= 2 passengers
|length m=
|length ft= 19.5
|length in=
|length note=
|span m=
|span ft= 28
|span in=
|span note=
|height m=
|height ft= 6.5
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb= 721
|empty weight note=
|gross weight kg=
|gross weight lb= 1320
|gross weight note=
|fuel capacity={{convert|10.5|u.s.gal}}
|more general=
|eng1 number=1
|eng1 name=Revmaster Volkswagen air-cooled engine conversion
|eng1 type=horizontally opposed piston engine
|eng1 kw=
|eng1 hp=85
|prop blade number=2
|prop name=wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|perfhide=
|max speed kmh=
|max speed mph=125
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=108
|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=
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}