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Statements

Subject Item
dbr:TL_Ultralight_TL-32_Typhoon
rdf:type
yago:Category105838765 schema:Product yago:Idea105833840 yago:Concept105835747 dbo:Aircraft yago:Kind105839024 yago:Content105809192 dbo:MeanOfTransportation yago:PsychologicalFeature100023100 yago:Type105840188 yago:Abstraction100002137 wikidata:Q11436 owl:Thing yago:Cognition100023271
rdfs:label
TL Ultralight TL-32 Typhoon
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.
foaf:depiction
n17:OK-OUR-15_TL-32_Day.jpg n17:OK-OUR-15_TL-32_Night.jpg
dcterms:subject
dbc:TL_Ultralight_aircraft dbc:1990s_Czech_and_Czechoslovakian_ultralight_aircraft
dbo:wikiPageID
34059366
dbo:wikiPageRevisionID
993822822
dbo:wikiPageWikiLink
dbr:Two-stroke dbr:Ailerons dbr:Tandem dbr:Lift_strut dbr:Russia dbr:Tricycle_undercarriage dbr:Jury_strut dbr:Fin dbr:Fairing_(aircraft) dbr:High_wing dbr:Rotax_462 dbr:Rotax_582 dbr:Ultralight dbr:Two_stroke dbr:Králové dbc:TL_Ultralight_aircraft dbr:Rudder dbr:Tailplane dbr:Trim_tab dbr:Aircraft_fabric_covering dbr:Elevator_(aircraft) dbr:Czech_Republic n19:OK-OUR-15_TL-32_Day.JPG dbr:Cockpit dbr:Rotax_503 dbr:TL_Ultralight dbc:1990s_Czech_and_Czechoslovakian_ultralight_aircraft
owl:sameAs
freebase:m.0hr34lr wikidata:Q7670625 n20:4vp9S
dbp:spanM
10.7
dbp:stallSpeedKmh
45
dbp:wingAreaNote
gross
dbp:wingAreaSqm
15.2
dbp:wikiPageUsesTemplate
dbt:Aircraft_specs dbt:Aircontent dbt:TL_Ultralight_aircraft dbt:Commons_category dbt:Reflist dbt:Infobox_aircraft_type
dbo:thumbnail
n17:OK-OUR-15_TL-32_Night.jpg?width=300
dbp:primeUnits%3F_
met
dbp:nationalOrigin
dbr:Czech_Republic
dbp:capacity
2
dbp:introduced
1991
dbp:manufacturer
dbr:Králové dbr:TL_Ultralight
dbp:ref
Jane's All the World's Aircraft 2000/01
dbp:type
Two seat ultralight
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.
dbp:cruiseSpeedKmh
90
dbp:emptyWeightKg
200
dbp:eng1Name
Rotax
dbp:eng1Number
1
dbp:eng1Type
two cylinder two stroke
dbp:heightM
2.45
dbp:lengthM
5.9
dbp:maxSpeedKmh
110
dbp:maxTakeoffWeightKg
400
dbp:numberBuilt
More than 200
dbp:rangeKm
300
gold:hypernym
dbr:Wing
prov:wasDerivedFrom
wikipedia-en:TL_Ultralight_TL-32_Typhoon?oldid=993822822&ns=0
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6184
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dbr:TL_Ultralight dbr:Králové
dbo:origin
dbr:Czech_Republic
dbo:type
dbr:Ultralight
foaf:isPrimaryTopicOf
wikipedia-en:TL_Ultralight_TL-32_Typhoon