About: Dyn'Aéro Twin-R

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The Dyn'Aéro Twin-R is a twin engine kit-built light aircraft based on the single-engine Dyn'Aéro MCR4S, designed and built in France. Its first flight was in March 2011.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	Dyn'Aéro Twin-R (en) Dyn'Aéro Twin-R (fr)
rdfs:comment	The Dyn'Aéro Twin-R is a twin engine kit-built light aircraft based on the single-engine Dyn'Aéro MCR4S, designed and built in France. Its first flight was in March 2011. (en) Le Dyn'Aéro Twin-R est un avion léger bimoteur de la société Dyn'Aéro. (fr)
dcterms:subject	Dyn'Aéro aircraft Low-wing aircraft 2010s French sport aircraft Aircraft first flown in 2011 Twin piston-engined tractor aircraft
Wikipage page ID	32445826 (xsd:integer)
Wikipage revision ID	1050846714 (xsd:integer)
Link from a Wikipage to another Wikipage	Rotax 912 Homebuilt aircraft Dyn'Aéro aircraft Dyn'Aéro MCR4S Light aircraft Low-wing aircraft Aileron 2010s French sport aircraft Fuselage Aircraft canopy Fin France Monocoque AERO Friedrichshafen Aircraft first flown in 2011 Twin piston-engined tractor aircraft Trapezoid Fairing (aircraft) Rudder Spar (aviation) T-tail Stabilator Yaw (rotation) Rib (aircraft) Carbon fibre Tricycle undercarriage EFIS Rotax 912ULS Flaps (aircraft) Flat four engine Ventral fin Winglet
sameAs	Dyn'Aéro Twin-R Dyn'Aéro Twin-R Dyn'Aéro Twin-R Dyn'Aéro Twin-R
span m	9.240000 (xsd:double)
stall speed kmh	92 (xsd:integer)
stall speed note	flaps down (en)
wing area sqm	8.600000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Short_description dbt:Dyn'Aéro_aircraft dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	2011-03-03 (xsd:date)
national origin	France
capacity	4 (xsd:integer)
designer	Pierre and Christophe Robin (en)
fuel capacity	110 (xsd:integer)
manufacturer	Dyn'Aéro (en)
ref	Jane's All the World's Aircraft 2011/12 (en)
type	Four seat twin engine kitbuilt (en)
unit cost	110000.0 (euro)
has abstract	The Dyn'Aéro Twin-R is a twin engine kit-built light aircraft based on the single-engine Dyn'Aéro MCR4S, designed and built in France. Its first flight was in March 2011. (en) Le Dyn'Aéro Twin-R est un avion léger bimoteur de la société Dyn'Aéro. (fr)
avionics	*Dynon Skyview 3-screen EFIS recommended (en)
climb rate ms	7.600000 (xsd:double)
cruise speed kmh	326 (xsd:integer)
cruise speed note	146280.0 (second)
developed from	Dyn'Aéro MCR4S
empty weight kg	425 (xsd:integer)
eng1 kw	73.500000 (xsd:double)
eng1 name	Rotax 912ULS (en)
eng1 number	2 (xsd:integer)
eng1 type	flat four, air- and water-cooled piston (en)
height m	1.900000 (xsd:double)
length m	7.100000 (xsd:double)
max speed kmh	335 (xsd:integer)
max takeoff weight kg	950 (xsd:integer)
prop blade number	2 (xsd:integer)
range km	2129 (xsd:integer)
range note	with maximum fuel (en)

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