About: PZL-105 Flaming

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An Entity of Type : umbel-rc:TransportationDevice_Vehicle, within Data Space : dbpedia.org associated with source document(s)
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http://dbpedia.org/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FPZL-105_Flaming

The PZL-105 Flaming (flamingo) is a Polish short-takeoff-and-landing (STOL) utility aircraft designed by PZL "Warszawa-Okęcie". It remained a prototype.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188 umbel-rc:Model_airplane umbel-rc:TransportationDevice_Vehicle
rdfs:label	PZL-105 Flaming (en)
rdfs:comment	The PZL-105 Flaming (flamingo) is a Polish short-takeoff-and-landing (STOL) utility aircraft designed by PZL "Warszawa-Okęcie". It remained a prototype. (en)
foaf:depiction
dcterms:subject	PZL aircraft 1980s Polish civil utility aircraft High-wing aircraft Single-engined tractor aircraft Aircraft first flown in 1989
Wikipage page ID	11053982 (xsd:integer)
Wikipage revision ID	1063863948 (xsd:integer)
Link from a Wikipage to another Wikipage	PZL aircraft Duralumin PZL-104 Wilga 1989 in aviation 1991 in aviation 1980s Polish civil utility aircraft Glider aircraft STOL Hartzell Propeller Seaplane High-wing aircraft Single-engined tractor aircraft PZL PZL-130 Orlik Monocoque Parachute Flap (aircraft) Aircraft first flown in 1989 Aerial application Landing gear Air ambulance Kraków Lycoming O-540 Vedeneyev M-14P Flaperon Polish Aviation Museum Lycoming IO-720-A1B Lycoming O-720
Link from a Wikipage to an external page	http://lotnictwo.net/galselect.php%3Fp=0&ui=133&mi=52&quer=1=1&ti=296&selectby=fotoID%20DESC&wpis=
sameAs	PZL-105 Flaming PZL-105 Flaming PZL-105 Flaming PZL-105 Flaming PZL-105 Flaming
span m	12.970000 (xsd:double)
stall speed kmh	102 (xsd:integer)
stall speed note	flaps down engine idling (en)
wing area sqm	16.900000 (xsd:double)
wing loading kg/m	109.500000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Commons_category dbt:Cvt dbt:Infobox_aircraft_type dbt:Portal dbt:Reflist dbt:PZL_aircraft dbt:Aircontent dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/PZL105_Flaming_PICT0049.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1989-11-09 (xsd:date)
primary user	Polish civilian aviation (en)
capacity	5 (xsd:integer)
crew	1 (xsd:integer)
fuel capacity	in two integral wing tanks (en)
manufacturer	PZL
ref	Jane's All The World's Aircraft 1993-94. (en)
related	* PZL-104 Wilga (en)
status	Prototype (en)
type	Utility aircraft (en)
has abstract	The PZL-105 Flaming (flamingo) is a Polish short-takeoff-and-landing (STOL) utility aircraft designed by PZL "Warszawa-Okęcie". It remained a prototype. (en)
airfoil	NASA GA-1 (en)
aspect ratio	9.950000 (xsd:double)
ceiling m	4140 (xsd:integer)
ceiling note	::::PZL-105L (en)
climb rate ms	5.500000 (xsd:double)
climb rate note	at sea level ::::PZL-105L (en)
cruise speed kmh	205 (xsd:integer)
cruise speed note	max ::: economical ::::PZL-105L max ::::PZL-105L economical (en)
empty weight kg	1130 (xsd:integer)
empty weight note	::::PZL-105L (en)
eng1 kw	268.500000 (xsd:double)
eng1 name	Vedeneyev M-14P
eng1 note	::::PZL-105L Lycoming IO-720-A1B (en)

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