About: Kappa 77 KP 2U-SOVA

Property	Value
dbo:abstract	The Kappa 77 KP-2U Sova, later produced as the Jihlavan KP-2U Skyleader and most recently as the Jihlavan Skyleader, is a two-seat civil utility aircraft designed in the Czech Republic and available in kit form for home building. It is a conventional low-wing monoplane featuring all-metal construction and tricycle undercarriage. (en)
dbo:manufacturer	dbr:Skyleader_a.s. dbr:Jihlavan_Aircraft dbr:Kappa_77_a.s.
dbo:numberBuilt	210 (xsd:nonNegativeInteger)
dbo:origin	dbr:Czech_Republic
dbo:thumbnail	wiki-commons:Special:FilePath/Skyleader200_brasov.jpg?width=300
dbo:unitCost	66100.0
dbo:wikiPageExternalLink	http://www.skyleader.aero/en/skyleader-100/ http://www.airliners.net/photo/Kappa-KP-2UR-Sova/1328831/L/
dbo:wikiPageID	1064002 (xsd:integer)
dbo:wikiPageLength	11461 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	1084071095 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Canada dbr:Rotax_914 dbr:Electric_aircraft dbr:Monoplane dbr:Homebuilt_aircraft dbr:Rhoadesville,_Virginia dbr:United_States dbc:Aircraft_manufactured_in_the_Czech_Republic_and_Czechoslovakia dbr:Elevator_(aircraft) dbr:Light-sport_aircraft dbr:Wing_tip dbr:Rotax_912S dbr:Low-wing dbc:Skyleader_aircraft dbr:Tandem dbr:Trim_tab dbr:Australia dbc:Low-wing_aircraft dbr:Bulgaria dbc:1990s_Czech_and_Czechoslovakian_ultralight_aircraft dbr:Fuselage dbr:Aluminium dbc:Homebuilt_aircraft dbc:Single-engined_tractor_aircraft dbr:Czech_Republic dbr:Fin dbr:Ballistic_parachute dbr:Flap_(aircraft) dbr:AERO_Friedrichshafen dbc:Electric_aircraft dbr:Jabiru_2200 dbr:Tailplane dbr:Skyleader_a.s. dbr:Sofia dbr:Rudder dbr:Dihedral_(aircraft) dbr:Four-stroke dbr:Rotax_582 dbr:Spar_(aviation) dbr:Rotax_912_UL dbr:Two-stroke dbr:Carbon_fibre dbr:Rotax_912UL dbr:Tricycle_undercarriage dbr:Rotax_912ULS dbr:Skyleader_Aircraft dbr:Jihlavan_Aircraft dbr:Kitplane dbr:Kappa_77_a.s. dbr:File:KP2U-Sova_OK-BUU_23.jpg dbr:File:Prototipo_aereo_elettrico_Rigenergia_2.JPG dbr:File:Skyleader600.jpg dbr:Galaxy_Rescue_Systems dbr:Küchemann
dbp:airfoil	root: NASA GA-1; tip:N NASA GA-2 (en)
dbp:capacity	1 (xsd:integer)
dbp:climbRateMs	6.500000 (xsd:double)
dbp:crew	1 (xsd:integer)
dbp:cruiseSpeedKmh	200 (xsd:integer)
dbp:cruiseSpeedNote	at 75% power (en)
dbp:emptyWeightKg	285 (xsd:integer)
dbp:eng1Kw	59.600000 (xsd:double)
dbp:eng1Name	dbr:Rotax_912UL
dbp:eng1Number	1 (xsd:integer)
dbp:eng1Type	4 (xsd:integer)
dbp:firstFlight	1996-05-26 (xsd:date)
dbp:fuelCapacity	:::: (en)
dbp:gLimits	+4 -2 (en)
dbp:heightM	2.600000 (xsd:double)
dbp:lengthM	7.170000 (xsd:double)
dbp:manufacturer	dbr:Skyleader_a.s. dbr:Jihlavan_Aircraft dbr:Kappa_77_a.s. ACS (en)
dbp:maxSpeedKmh	240 (xsd:integer)
dbp:maxTakeoffWeightKg	450 (xsd:integer)
dbp:maxTakeoffWeightNote	:::: :::: (en)
dbp:morePerformance	Take-off run: Landing run: (en)
dbp:nationalOrigin	dbr:Czech_Republic
dbp:numberBuilt	Over 210 by November 2010 (en)
dbp:primeUnits?_	met (en)
dbp:propBladeNumber	2 (xsd:integer)
dbp:propDiaM	1.730000 (xsd:double)
dbp:propDiaNote	(en)
dbp:propName	variable-pitch propeller (en)
dbp:rangeKm	960 (xsd:integer)
dbp:ref	Jane's All The World's Aircraft 2004–2005, Jane's All The World's Aircraft 2003–2004 (en)
dbp:spanM	9.900000 (xsd:double)
dbp:stallSpeedKmh	71 (xsd:integer)
dbp:stallSpeedNote	flaps up :::: flaps down (en)
dbp:status	In production (en)
dbp:type	Light aircraft (en)
dbp:unitCost	Skyleader 150: (en) €66,100 flyaway, excluding tax (en)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Convert dbt:Cvt dbt:Infobox_aircraft_type dbt:Reflist dbt:Aero_Adventure_aircraft dbt:Aircraft_specs dbt:Skyleader_Aircraft
dbp:wingAreaSqm	11.850000 (xsd:double)
dcterms:subject	dbc:Aircraft_manufactured_in_the_Czech_Republic_and_Czechoslovakia dbc:Skyleader_aircraft dbc:Low-wing_aircraft dbc:1990s_Czech_and_Czechoslovakian_ultralight_aircraft dbc:Homebuilt_aircraft dbc:Single-engined_tractor_aircraft dbc:Electric_aircraft
gold:hypernym	dbr:Aircraft
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 Kappa 77 KP-2U Sova, later produced as the Jihlavan KP-2U Skyleader and most recently as the Jihlavan Skyleader, is a two-seat civil utility aircraft designed in the Czech Republic and available in kit form for home building. It is a conventional low-wing monoplane featuring all-metal construction and tricycle undercarriage. (en)
rdfs:label	Kappa 77 KP 2U-SOVA (en)
owl:sameAs	freebase:Kappa 77 KP 2U-SOVA wikidata:Kappa 77 KP 2U-SOVA dbpedia-sl:Kappa 77 KP 2U-SOVA http://tg.dbpedia.org/resource/Kappa_77_KP_2U-SOVA https://global.dbpedia.org/id/4pPyH
prov:wasDerivedFrom	wikipedia-en:Kappa_77_KP_2U-SOVA?oldid=1084071095&ns=0
foaf:depiction	wiki-commons:Special:FilePath/KP2U-Sova_OK-BUU_23.jpg wiki-commons:Special:FilePath/Prototipo_aereo_elettrico_Rigenergia_2.jpg wiki-commons:Special:FilePath/Skyleader200_brasov.jpg wiki-commons:Special:FilePath/Skyleader600.jpg
foaf:isPrimaryTopicOf	wikipedia-en:Kappa_77_KP_2U-SOVA
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is foaf:primaryTopic of	wikipedia-en:Kappa_77_KP_2U-SOVA