About: ATEC 212 Solo

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

The ATEC 212 Solo is a Czech ultralight aircraft, designed and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft.

Property	Value
dbo:abstract	The ATEC 212 Solo is a Czech ultralight aircraft, designed and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft. (en)
dbo:manufacturer	dbr:ATEC_v.o.s.
dbo:origin	dbr:Czech_Republic
dbo:type	dbr:Ultralight_aircraft
dbo:unitCost	43225.0 (dbd:euro)
dbo:wikiPageExternalLink	https://www.atecaircraft.eu/en/planes/atec-212-solo
dbo:wikiPageID	35710454 (xsd:integer)
dbo:wikiPageLength	4397 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	1113333521 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Fédération_Aéronautique_Internationale dbr:Conventional_landing_gear dbr:Libice_nad_Cidlinou dbr:Low-wing dbr:ATEC_122_Zephyr_2000 dbr:ATEC_321_Faeta dbr:Airfoil dbc:Single-engined_tractor_aircraft dbr:Czech_Republic dbr:Euro dbr:Flap_(aircraft) dbr:ATEC_v.o.s. dbc:2000s_Czech_ultralight_aircraft dbc:ATEC_aircraft dbr:Tractor_configuration dbr:Bubble_canopy dbr:Four-stroke dbr:Rotax_582 dbr:Ultralight_aircraft dbr:Two-stroke dbr:Carbon_fibre dbr:Rotax_912UL dbr:Two_stroke
dbp:climbRateMs	7 (xsd:integer)
dbp:crew	one (en)
dbp:cruiseSpeedKmh	220 (xsd:integer)
dbp:emptyWeightKg	200 (xsd:integer)
dbp:eng1Kw	48 (xsd:integer)
dbp:eng1Name	dbr:Rotax_582
dbp:eng1Number	1 (xsd:integer)
dbp:eng1Type	twin cylinder, liquid-cooled, two stroke (en)
dbp:grossWeightKg	315 (xsd:integer)
dbp:manufacturer	dbr:ATEC_v.o.s.
dbp:maxSpeedKmh	250 (xsd:integer)
dbp:nationalOrigin	dbr:Czech_Republic
dbp:primeUnits?_	met (en)
dbp:propBladeNumber	3 (xsd:integer)
dbp:propName	composite (en)
dbp:ref	Bayerl (en)
dbp:spanM	7.480000 (xsd:double)
dbp:stallSpeedKmh	65 (xsd:integer)
dbp:status	In production (en)
dbp:type	dbr:Ultralight_aircraft
dbp:unitCost	43225.0 (dbd:euro)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:ATEC_aircraft dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:wingAreaSqm	7.270000 (xsd:double)
dbp:wingLoadingKg/m	43.320000 (xsd:double)
dct:subject	dbc:Single-engined_tractor_aircraft dbc:2000s_Czech_ultralight_aircraft dbc:ATEC_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 ATEC 212 Solo is a Czech ultralight aircraft, designed and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft. (en)
rdfs:label	ATEC 212 Solo (en)
owl:sameAs	freebase:ATEC 212 Solo wikidata:ATEC 212 Solo http://tg.dbpedia.org/resource/ATEC_212_Solo https://global.dbpedia.org/id/4KKmw
prov:wasDerivedFrom	wikipedia-en:ATEC_212_Solo?oldid=1113333521&ns=0
foaf:isPrimaryTopicOf	wikipedia-en:ATEC_212_Solo
is dbo:wikiPageWikiLink of	dbr:Rotax_912 dbr:List_of_aircraft_(An–Az) dbr:ATEC_v.o.s. dbr:Rotax_582
is foaf:primaryTopic of	wikipedia-en:ATEC_212_Solo