About: TL Ultralight TL-32 Typhoon

An Entity of Type: Ultralight, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s.

Property	Value
dbo:abstract	The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s. (en)
dbo:manufacturer	dbr:TL_Ultralight dbr:Králové
dbo:origin	dbr:Czech_Republic
dbo:thumbnail	wiki-commons:Special:FilePath/OK-OUR-15_TL-32_Night.jpg?width=300
dbo:type	dbr:Ultralight
dbo:wikiPageID	34059366 (xsd:integer)
dbo:wikiPageLength	6184 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	993822822 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Rotax_462 dbr:Ultralight dbr:Elevator_(aircraft) dbr:Russia dbr:Tandem dbr:Trim_tab dbc:1990s_Czech_and_Czechoslovakian_ultralight_aircraft dbr:TL_Ultralight dbr:Ailerons dbr:Aircraft_fabric_covering dbr:Czech_Republic dbr:Fin dbr:Cockpit dbr:Tailplane dbr:Fairing_(aircraft) dbr:Rudder dbc:TL_Ultralight_aircraft dbr:Rotax_582 dbr:Rotax_503 dbr:High_wing dbr:Two-stroke dbr:Tricycle_undercarriage dbr:Two_stroke dbr:Jury_strut dbr:Lift_strut dbr:Králové dbr:File:OK-OUR-15_TL-32_Day.JPG
dbp:capacity	2 (xsd:integer)
dbp:cruiseSpeedKmh	90 (xsd:integer)
dbp:emptyWeightKg	200 (xsd:integer)
dbp:eng1Name	Rotax (en)
dbp:eng1Number	1 (xsd:integer)
dbp:eng1Type	two cylinder two stroke (en)
dbp:heightM	2.450000 (xsd:double)
dbp:introduced	1991 (xsd:integer)
dbp:lengthM	5.900000 (xsd:double)
dbp:manufacturer	dbr:TL_Ultralight dbr:Králové
dbp:maxSpeedKmh	110 (xsd:integer)
dbp:maxTakeoffWeightKg	400 (xsd:integer)
dbp:nationalOrigin	dbr:Czech_Republic
dbp:numberBuilt	More than 200 (en)
dbp:primeUnits?_	met (en)
dbp:rangeKm	300 (xsd:integer)
dbp:ref	Jane's All the World's Aircraft 2000/01 (en)
dbp:spanM	10.700000 (xsd:double)
dbp:stallSpeedKmh	45 (xsd:integer)
dbp:type	Two seat ultralight (en)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:TL_Ultralight_aircraft dbt:Aircontent dbt:Aircraft_specs
dbp:wingAreaNote	gross (en)
dbp:wingAreaSqm	15.200000 (xsd:double)
dcterms:subject	dbc:1990s_Czech_and_Czechoslovakian_ultralight_aircraft dbc:TL_Ultralight_aircraft
gold:hypernym	dbr:Wing
rdf:type	owl:Thing schema:Product dbo:MeanOfTransportation wikidata:Q11436 yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 dbo:Aircraft yago:Type105840188
rdfs:comment	The TL Ultralight TL-32 Typhoon is a wing and boom, high wing ultralight with its engine mounted above and ahead of the wing, seating two in side-by-side configuration. It was designed and built in the Czech Republic in the 1990s. (en)
rdfs:label	TL Ultralight TL-32 Typhoon (en)
owl:sameAs	freebase:TL Ultralight TL-32 Typhoon wikidata:TL Ultralight TL-32 Typhoon https://global.dbpedia.org/id/4vp9S
prov:wasDerivedFrom	wikipedia-en:TL_Ultralight_TL-32_Typhoon?oldid=993822822&ns=0
foaf:depiction	wiki-commons:Special:FilePath/OK-OUR-15_TL-32_Day.jpg wiki-commons:Special:FilePath/OK-OUR-15_TL-32_Night.jpg
foaf:isPrimaryTopicOf	wikipedia-en:TL_Ultralight_TL-32_Typhoon
is dbo:wikiPageWikiLink of	dbr:List_of_aircraft_(Tl) dbr:Letov_LK-2_Sluka dbr:Rotax_582 dbr:Rotax_503 dbr:TL–Ultralight
is foaf:primaryTopic of	wikipedia-en:TL_Ultralight_TL-32_Typhoon