| dbo:abstract |
The Wolfsberg Aircraft Sparrow ML is a twin boom, pusher configuration ultralight aircraft seating two in tandem. Designed and built in the Czech Republic. (en) |
| dbo:numberBuilt |
13 (xsd:nonNegativeInteger) |
| dbo:origin |
dbr:Czech_Republic |
| dbo:type |
dbr:Tandem |
| dbo:unitCost |
100000.0 (dbd:euro) |
| dbo:wikiPageID |
46977635 (xsd:integer) |
| dbo:wikiPageLength |
6305 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1093889994 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Rotax_912 dbr:Ultralight dbr:Elevator_(aircraft) dbr:Tandem dbr:Trim_tab dbc:Low-wing_aircraft dbr:Aileron dbr:Fuselage dbr:Leading_edge dbc:Single-engined_pusher_aircraft dbr:Aircraft_fairing dbr:Czech_Republic dbr:Fin dbr:Pusher_configuration dbr:Flap_(aircraft) dbr:AERO_Friedrichshafen dbc:2010s_Czech_ultralight_aircraft dbc:Twin-boom_aircraft dbc:Aircraft_first_flown_in_2010 dbr:Landing_gear dbr:Tailplane dbr:Twin_boom dbr:Rudder dbr:Flat-four_engine dbr:Rotax_912_UL dbr:Carbon_fibre dbr:Woodcomp dbr:Flat-four |
| dbp:capacity |
one passenger (en) |
| dbp:climbRateNote |
at sea level (en) |
| dbp:crew |
one pilot (en) |
| dbp:cruiseSpeedKmh |
210 (xsd:integer) |
| dbp:designer |
Alec N Clark (en) |
| dbp:emptyWeightKg |
272 (xsd:integer) |
| dbp:eng1Hp |
80 (xsd:integer) |
| dbp:eng1Name |
dbr:Rotax_912_UL |
| dbp:eng1Number |
1 (xsd:integer) |
| dbp:eng1Type |
air and water-cooled horizontally opposed 4-cylinder in pusher configuration (en) |
| dbp:firstFlight |
2010-08-24 (xsd:date) |
| dbp:heightM |
1.760000 (xsd:double) |
| dbp:introduced |
March 2013 (en) |
| dbp:lengthM |
7 (xsd:integer) |
| dbp:manufacturer |
Wolfsberg Aircraft s.r.o. (en) |
| dbp:maxTakeoffWeightKg |
472.500000 (xsd:double) |
| dbp:minimumControlSpeedKmh |
60 (xsd:integer) |
| dbp:morePerformance |
900.0 (dbd:second) |
| dbp:nationalOrigin |
dbr:Czech_Republic |
| dbp:neverExceedSpeedKmh |
234 (xsd:integer) |
| dbp:numberBuilt |
13 (xsd:integer) |
| dbp:primeUnits?_ |
met (en) |
| dbp:propBladeNumber |
3 (xsd:integer) |
| dbp:propDiaM |
1.700000 (xsd:double) |
| dbp:propDiaNote |
composite, with ground adjustable pitch (en) |
| dbp:propName |
Woodcomp Klassic 170/3 (en) |
| dbp:ref |
Wolfsberg Aircraft (en) |
| dbp:spanM |
9.100000 (xsd:double) |
| dbp:stallSpeedKmh |
57 (xsd:integer) |
| dbp:stallSpeedNote |
flaps down (en) |
| dbp:status |
in production (en) |
| dbp:type |
Tandem seat ultralight (en) |
| dbp:unitCost |
€100,000 without tax (en) |
| dbp:wikiPageUsesTemplate |
dbt:Convert dbt:Dead_link dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircraft_specs |
| dbp:wingAreaSqm |
11.600000 (xsd:double) |
| dct:subject |
dbc:Low-wing_aircraft dbc:Single-engined_pusher_aircraft dbc:2010s_Czech_ultralight_aircraft dbc:Twin-boom_aircraft dbc:Aircraft_first_flown_in_2010 |
| gold:hypernym |
dbr:Boom |
| rdf:type |
owl:Thing schema:Product dbo:MeanOfTransportation wikidata:Q11436 dbo:Aircraft |
| rdfs:comment |
The Wolfsberg Aircraft Sparrow ML is a twin boom, pusher configuration ultralight aircraft seating two in tandem. Designed and built in the Czech Republic. (en) |
| rdfs:label |
WLT Sparrow (en) |
| owl:sameAs |
freebase:WLT Sparrow wikidata:WLT Sparrow https://global.dbpedia.org/id/2PVx5 |
| prov:wasDerivedFrom |
wikipedia-en:WLT_Sparrow?oldid=1093889994&ns=0 |
| foaf:isPrimaryTopicOf |
wikipedia-en:WLT_Sparrow |
| is dbo:wikiPageRedirects of |
dbr:Sparrow_ML |
| is dbo:wikiPageWikiLink of |
dbr:Rotax_912 dbr:List_of_aircraft_(W) dbr:List_of_pusher_aircraft_by_configuration_and_date dbr:Rotax_582 dbr:Twin-boom_aircraft dbr:Sparrow_ML |
| is foaf:primaryTopic of |
wikipedia-en:WLT_Sparrow |