| http://dbpedia.org/ontology/abstract
|
The ATEC 122 Zephyr 2000 is a Czech ultralight aircraft, designed by Oldrich Olansky and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.
|
| http://dbpedia.org/ontology/manufacturer
|
http://dbpedia.org/resource/ATEC_v.o.s. +
|
| http://dbpedia.org/ontology/origin
|
http://dbpedia.org/resource/Czech_Republic +
|
| http://dbpedia.org/ontology/successor
|
http://dbpedia.org/resource/ATEC_321_Faeta +
|
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|
http://commons.wikimedia.org/wiki/Special:FilePath/Zephyr_2000_OK-MUG_48.jpg?width=300 +
|
| http://dbpedia.org/ontology/type
|
http://dbpedia.org/resource/Ultralight_aircraft +
, http://dbpedia.org/resource/Light-sport_aircraft +
|
| http://dbpedia.org/ontology/unitCost
|
53675.0
|
| http://dbpedia.org/ontology/wikiPageExternalLink
|
https://www.atecaircraft.eu/en/planes/atec-122-zephyr +
|
| http://dbpedia.org/ontology/wikiPageID
|
35726565
|
| http://dbpedia.org/ontology/wikiPageLength
|
6009
|
| http://dbpedia.org/ontology/wikiPageRevisionID
|
1113333518
|
| http://dbpedia.org/ontology/wikiPageWikiLink
|
http://dbpedia.org/resource/Four_stroke +
, http://dbpedia.org/resource/Aircraft_fabric +
, http://dbpedia.org/resource/ATEC_321_Faeta +
, http://dbpedia.org/resource/Tricycle_landing_gear +
, http://dbpedia.org/resource/T-tail +
, http://dbpedia.org/resource/Category:Single-engined_tractor_aircraft +
, http://dbpedia.org/resource/Low-wing +
, http://dbpedia.org/resource/Airfoil +
, http://dbpedia.org/resource/Light-sport_aircraft +
, http://dbpedia.org/resource/Category:Light-sport_aircraft +
, http://dbpedia.org/resource/Ultralight_aircraft +
, http://dbpedia.org/resource/Leading_edge +
, http://dbpedia.org/resource/F%C3%A9d%C3%A9ration_A%C3%A9ronautique_Internationale +
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, http://dbpedia.org/resource/Category:2000s_Czech_ultralight_aircraft +
, http://dbpedia.org/resource/Tractor_configuration +
, http://dbpedia.org/resource/Plywood +
, http://dbpedia.org/resource/Side-by-side_configuration +
, http://dbpedia.org/resource/Bubble_canopy +
, http://dbpedia.org/resource/Rotax_912ULS +
, http://dbpedia.org/resource/Fuselage +
, http://dbpedia.org/resource/Aircraft_dope +
, http://dbpedia.org/resource/ATEC_v.o.s. +
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, http://dbpedia.org/resource/Spar_%28aviation%29 +
, http://dbpedia.org/resource/Category:ATEC_aircraft +
, http://dbpedia.org/resource/Libice_nad_Cidlinou +
, http://dbpedia.org/resource/File:Zephyr_2000_D-MAHL.jpg +
, http://dbpedia.org/resource/Euro +
|
| http://dbpedia.org/property/airfoil
|
UA-2
|
| http://dbpedia.org/property/capacity
|
one passenger
|
| http://dbpedia.org/property/climbRateMs
|
6.5
|
| http://dbpedia.org/property/crew
|
one
|
| http://dbpedia.org/property/cruiseSpeedKmh
|
215
|
| http://dbpedia.org/property/designer
|
Oldrich Olansky
|
| http://dbpedia.org/property/emptyWeightKg
|
275
|
| http://dbpedia.org/property/eng1Kw
|
75
|
| http://dbpedia.org/property/eng1Name
|
http://dbpedia.org/resource/Rotax_912ULS +
|
| http://dbpedia.org/property/eng1Number
|
1
|
| http://dbpedia.org/property/eng1Type
|
four cylinder, liquid and air-cooled, four stroke
|
| http://dbpedia.org/property/grossWeightKg
|
472.5
|
| http://dbpedia.org/property/introduced
|
1996
|
| http://dbpedia.org/property/manufacturer
|
http://dbpedia.org/resource/ATEC_v.o.s. +
|
| http://dbpedia.org/property/maxSpeedKmh
|
265
|
| http://dbpedia.org/property/nationalOrigin
|
http://dbpedia.org/resource/Czech_Republic +
|
| http://dbpedia.org/property/numberBuilt
|
more than 200
|
| http://dbpedia.org/property/primeUnits%3F
|
met
|
| http://dbpedia.org/property/ref
|
Bertrand and Purdy
|
| http://dbpedia.org/property/spanM
|
9.6
|
| http://dbpedia.org/property/stallSpeedKmh
|
65
|
| http://dbpedia.org/property/status
|
In production
|
| http://dbpedia.org/property/type
|
Ultralight aircraft and Light-sport aircraft
|
| http://dbpedia.org/property/unitCost
|
53675.0
|
| http://dbpedia.org/property/variantsWithTheirOwnArticles
|
http://dbpedia.org/resource/ATEC_321_Faeta +
|
| http://dbpedia.org/property/wikiPageUsesTemplate
|
http://dbpedia.org/resource/Template:Aircraft_specs +
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, http://dbpedia.org/resource/Template:Convert +
|
| http://dbpedia.org/property/wingAreaSqm
|
10.07
|
| http://dbpedia.org/property/wingLoadingKg/m
|
46.92
|
| http://purl.org/dc/terms/subject
|
http://dbpedia.org/resource/Category:2000s_Czech_ultralight_aircraft +
, http://dbpedia.org/resource/Category:Single-engined_tractor_aircraft +
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, http://dbpedia.org/resource/Category:Light-sport_aircraft +
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http://dbpedia.org/resource/Aircraft +
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http://en.wikipedia.org/wiki/ATEC_122_Zephyr_2000?oldid=1113333518&ns=0 +
|
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|
http://commons.wikimedia.org/wiki/Special:FilePath/Zephyr_2000_D-MAHL.jpg +
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http://en.wikipedia.org/wiki/ATEC_122_Zephyr_2000 +
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http://rdf.freebase.com/ns/m.0jt7_gf +
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|
| rdfs:comment |
The ATEC 122 Zephyr 2000 is a Czech ultralight aircraft, designed by Oldrich Olansky and produced by ATEC v.o.s. of Libice nad Cidlinou. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.
|
| rdfs:label |
ATEC 122 Zephyr 2000
|
