About: UL-Jih Evolution

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The UL-Jih Evolution is a conventionally laid out, two-seat, high-wing, single-engine ultralight, designed and built in the Czech Republic. Two variants were available in 2010.

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	UL-Jih Evolution (en)
rdfs:comment	The UL-Jih Evolution is a conventionally laid out, two-seat, high-wing, single-engine ultralight, designed and built in the Czech Republic. Two variants were available in 2010. (en)
dct:subject	UL-Jih aircraft 2000s Czech ultralight aircraft
Wikipage page ID	34054560 (xsd:integer)
Wikipage revision ID	993823122 (xsd:integer)
Link from a Wikipage to another Wikipage	UL-Jih Fascination Homebuilt aircraft Ultralight Elevator (aircraft) UL-Jih Sedláĉek Spol s.r.o. Russia Germany UL-Jih aircraft Trapezoidal Empennage Trim tab UL-Jih Fuselage Czech Republic Euro Fin Ballistic parachute Fowler flaps High-wing 2000s Czech ultralight aircraft Tailplane Cantilever Rudder Rotax 912UL Tricycle undercarriage Rotax 912ULS Side-by-side configuration
Link from a Wikipage to an external page	http://www.uljih.cz/homeeng.php%7Cname=UL-Jih
sameAs	UL-Jih Evolution UL-Jih Evolution UL-Jih Evolution
span m	9 (xsd:integer)
stall speed kmh	65 (xsd:integer)
stall speed note	flaps extended (en)
wing area note	gross (en)
wing area sqm	10.760000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Short_description dbt:UL-Jih_aircraft dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	2002-02-16 (xsd:date)
national origin	Czech Republic
capacity	two (en)
designer	Jaroslav Sedláĉek (en)
fuel capacity	120.0 (litre)
manufacturer	UL-Jih Sedláĉek Spol s.r.o.
ref	Jane's All the World's Aircraft 2011/12 (en)
type	Two seat ultralight/kitbuilt (en)
unit cost	E100: €83,300 (en) E80: €62,500 (en)
has abstract	The UL-Jih Evolution is a conventionally laid out, two-seat, high-wing, single-engine ultralight, designed and built in the Czech Republic. Two variants were available in 2010. (en)
ceiling m	4570 (xsd:integer)
climb rate ms	8.500000 (xsd:double)
climb rate note	maximum at sea level (en)
cruise speed kmh	270 (xsd:integer)
empty weight kg	305 (xsd:integer)
eng1 kw	73.500000 (xsd:double)
eng1 name	Rotax 912ULS
eng1 note	geared down 1.43:1 (en)
eng1 number	1 (xsd:integer)
eng1 type	Four cylinder four stroke, air- and water-cooled (en)
g limits	+4.0/-2.0 (en)
height m	2.100000 (xsd:double)
length m	6.980000 (xsd:double)
max speed kmh	290 (xsd:integer)
max takeoff weight kg	472.500000 (xsd:double)
number built	at least six by 2005 (en)
prop blade number	3 (xsd:integer)
prop name	Rospeller constant speed (en)
range km	1400 (xsd:integer)
range note	with maximum fuel (en)
prov:wasDerivedFrom	wikipedia-en:UL-Jih_Evolution?oldid=993823122&ns=0
page length (characters) of wiki page	6032 (xsd:nonNegativeInteger)
manufacturer	UL-Jih Sedláĉek Spol s.r.o.
origin	Czech Republic
type	Homebuilt aircraft Ultralight

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