- Specifications (AV.42)
- References
| name=AV.42 | image= | caption= }}{{Infobox aircraft type | type=Jet-powered tourism aircraft project | national origin=France | manufacturer= | designer=Charles Fauvel | first flight= | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles=
}} |
The Fauvel AV.42 was a (AV for aile volante ({{trans|flying wing}}) was a tail-less tourism cabin monoplane designed, but not built, in France. Specifications (AV.42) {{Aircraft specs
|ref=[1], Charles Fauvel and his Flying Wings[2]
|prime units?=met
|genhide=
|crew=One
|capacity=5 pax
|length m=6.50
|length note=including elevator
|span m=10.00
|width m=
|height m=
|wing area sqm=19.7
|aspect ratio=
|airfoil=
|empty weight kg=
|gross weight kg=
|max takeoff weight kg=
|fuel capacity=
|more general=
|eng1 number=3
|eng1 name=Turbomeca Palas
|eng1 type=turbojet
|eng1 lbf=350
|eng1 note=for take-off (note:centre engine for take-off and climb only)
|max speed kmh=610
|cruise speed kmh=500
|stall speed kmh=
|never exceed speed kmh=
|minimum control speed kmh=
|range km=1000
|range note= to {{cvt|3000|km|mi nmi}}
|combat range km=
|ferry range km=
|endurance=
|ceiling m=
|g limits=
|roll rate=
|climb rate ms=
|time to altitude=
|wing loading kg/m2=
|fuel consumption kg/km=
|power/mass=
|thrust/weight=
|more performance=
}}
References1. ^{{cite web |title=Fauvel AV.42 |url=http://all-aero.com/index.php/contactus/45-planes-d-e-f/3517-fauvel-av42 |website=all-aero.com |accessdate=1 March 2019}}
2. ^{{cite web |title=Charles Fauvel and his Flying Wings |url=http://www.nurflugel.com/Nurflugel/Fauvel/e_AV42.htm |website=www.nurflugel.com |accessdate=1 March 2019 |language=French}}
{{Fauvel aircraft}}{{Aero-stub}} 3 : Tailless aircraft|Flying wings|Fauvel aircraft |