About: Brutsche Freedom 210 STOL

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http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FBrutsche_Freedom_210_STOL&invfp=IFP_OFF&sas=SAME_AS_OFF

The Brutsche Freedom 210 STOL was a proposed American STOL homebuilt aircraft that was designed by Neal H. Brutsche and intended to be produced by Brutsche Aircraft Corporation of Salt Lake City, Utah, introduced in the mid-1990s. The aircraft was planned to be supplied as a kit for amateur construction.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	Brutsche Freedom 210 STOL (en)
rdfs:comment	The Brutsche Freedom 210 STOL was a proposed American STOL homebuilt aircraft that was designed by Neal H. Brutsche and intended to be produced by Brutsche Aircraft Corporation of Salt Lake City, Utah, introduced in the mid-1990s. The aircraft was planned to be supplied as a kit for amateur construction. (en)
foaf:depiction
dcterms:subject	High-wing aircraft Homebuilt aircraft Single-engined tractor aircraft 1990s United States civil utility aircraft Brutsche aircraft
Wikipage page ID	46446959 (xsd:integer)
Wikipage revision ID	896090797 (xsd:integer)
Link from a Wikipage to another Wikipage	Homebuilt aircraft United States Lycoming IO-360 Salt Lake City, Utah Conventional landing gear Lycoming O-360 STOL Brutsche Freedom 40 US$ Aluminum High-wing aircraft Homebuilt aircraft Single-engined tractor aircraft Aircraft engine Aircraft registration Federal Aviation Administration Floatplane High-wing Flap (aircraft) 1990s United States civil utility aircraft Tractor configuration Brutsche Aircraft Corporation Brutsche aircraft Four stroke Fuel-injected Brutsche Aircraft Wheel pants
sameAs	Brutsche Freedom 210 STOL Brutsche Freedom 210 STOL Brutsche Freedom 210 STOL Brutsche Freedom 210 STOL
span ft	31 (xsd:integer)
span in	0 (xsd:integer)
stall speed mph	49 (xsd:integer)
stall speed note	flaps down (en)
wing area sqft	135 (xsd:integer)
wing loading lb/sqft	16.700000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Brutsche_aircraft dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Brutsche_Freedom_210_STOL_three-view.png?width=300
dbp:primeUnits%3F_	imp (en)
national origin	United States
capacity	three passengers (en)
crew	one (en)
designer	Neal H. Brutsche (en)
length ft	24 (xsd:integer)
manufacturer	Brutsche Aircraft
ref	AeroCrafter (en)
status	Production completed (en)
type	Homebuilt aircraft
unit cost	21850.0 (usDollar)
has abstract	The Brutsche Freedom 210 STOL was a proposed American STOL homebuilt aircraft that was designed by Neal H. Brutsche and intended to be produced by Brutsche Aircraft Corporation of Salt Lake City, Utah, introduced in the mid-1990s. The aircraft was planned to be supplied as a kit for amateur construction. (en)
ceiling ft	22000 (xsd:integer)
climb rate ftmin	1630 (xsd:integer)
cruise speed mph	195 (xsd:integer)
empty weight lb	1250 (xsd:integer)
eng1 hp	108 (xsd:integer)
eng1 name	Lycoming IO-360
eng1 number	1 (xsd:integer)
eng1 type	four cylinder, air-cooled, fuel-injected, four stroke aircraft engine (en)
gross weight lb	2250 (xsd:integer)
length in	6 (xsd:integer)
max speed mph	207 (xsd:integer)
number built	None (en)
range miles	1290 (xsd:integer)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:Brutsche_Freedom_210_STOL?oldid=896090797&ns=0
page length (characters) of wiki page	6332 (xsd:nonNegativeInteger)
unit cost ($)	21850.0 (usDollar)
manufacturer	Brutsche Aircraft
origin	United States
type	Homebuilt aircraft
foaf:isPrimaryTopicOf	wikipedia-en:Brutsche_Freedom_210_STOL
is Link from a Wikipage to another Wikipage of	List of aircraft (Br–Bz) Lycoming O-360 Brutsche Aircraft Corporation Brutsche Freedom 180 STOL
is Wikipage redirect of	Brutsche Freedom 180 STOL
is foaf:primaryTopic of	wikipedia-en:Brutsche_Freedom_210_STOL

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