- Design and development
- Specifications (Capeña)
- References
- External links
| name=Capeña | image= | caption= }}{{Infobox Aircraft Type | type=Aerobatic amateur-built aircraft | national origin=France | manufacturer= | designer=Louis Peña | first flight=24 July 1984 | introduced= | retired= | status=Plans available (2012) | primary user= | more users= | produced= | number built= | program cost= | unit cost= €760 (plans only, 2011) | developed from= | variants with their own articles=Peña Bilouis
}} |
The Peña Capeña is a French aerobatic amateur-built aircraft that was designed by competitive aerobatic pilot Louis Peña of Dax, Landes and made available in the form of plans for amateur construction.[1][2] Design and developmentThe Capeña features a cantilever low-wing, a single seat enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.[1][2] The Capeña is made from wood. Its {{convert|6.8|m|ft|1|abbr=on}} span wing has an area of {{convert|7.65|m2|sqft|abbr=on}} and mounts flaps. The standard recommended engines is the {{convert|180|to|200|hp|kW|0|abbr=on}} Lycoming AEIO-360 four-stroke powerplant.[1][2] The aircraft was later developed into the two seat Peña Bilouis.[1][2] Specifications (Capeña) {{Aircraft specs
|ref=Bayerl and Tacke[1][2]
|prime units?=met
|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=6.8
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=7.65
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=440
|empty weight lb=
|empty weight note=
|gross weight kg=580
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|85|l}} in two tanks of {{convert|40|l}} and {{convert|45|l}}
|more general=
|eng1 number=1
|eng1 name=Lycoming AEIO-360
|eng1 type=four cylinder, air-cooled, four stroke aircraft engine
|eng1 kw=
|eng1 hp=200
|prop blade number=2
|prop name=metal constant speed propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=325
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=280
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=85
|stall speed mph=
|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=15
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=75.8
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}
References1. ^1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 109. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^1 2 3 4 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 115. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
External links- {{Official website|http://lpena.free.fr/capena.htm}}
{{Peña aircraft}}{{aerobatics}}{{DEFAULTSORT:Pena Capena}} 3 : Homebuilt aircraft|Single-engined tractor aircraft|Aerobatic aircraft |