About: Aerial Engineering Corporation Standard 6W-3

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An Entity of Type : dbo:Aircraft, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FAerial_Engineering_Corporation_Standard_6W-3&invfp=IFP_OFF&sas=SAME_AS_OFF

The Aerial Engineering Corporation Standard 6W-3 was a commercial transport modification of the US Standard J-1 biplane military trainer aircraft, with new wings, engine and accommodation for four passengers. First flown in 1925, it was built in small numbers.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	Aerial Engineering Corporation Standard 6W-3 (en)
rdfs:comment	The Aerial Engineering Corporation Standard 6W-3 was a commercial transport modification of the US Standard J-1 biplane military trainer aircraft, with new wings, engine and accommodation for four passengers. First flown in 1925, it was built in small numbers. (en)
foaf:depiction
dcterms:subject	Single-engined tractor aircraft 1920s United States civil utility aircraft Aircraft first flown in 1925 Biplanes
Wikipage page ID	54093210 (xsd:integer)
Wikipage revision ID	1113329620 (xsd:integer)
Link from a Wikipage to another Wikipage	Elevator (aeronautics) Curtiss C-6 United States dbr:Harvey_C._Mummert Clark Y Glenn Curtiss Chord (aeronautics) Empennage Spar (aeronautics) Tandem Trainer (aircraft) US Ailerons Airfoil Single-engined tractor aircraft Aircraft fairing Airliner Balanced rudder Radiator (engine cooling) 1920s United States civil utility aircraft Aircraft first flown in 1925 Biplanes Landing gear Biplane Tailplane Dihedral (aeronautics) Aspect ratio (aeronautics) Spruce Cabane strut World War I Longeron Rudder Stagger (aeronautics) Straight engine Interplane strut Fin (aeronautics) Standard J-1 dbr:Harvey_Mummert
sameAs	Aerial Engineering Corporation Standard 6W-3 Aerial Engineering Corporation Standard 6W-3
span m	10.570000 (xsd:double)
stall speed kmh	73 (xsd:integer)
stall speed note	minimum speed (en)
wing area sqm	33.850000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Mercury_Standard_6W-3_Les_Ailes_February_18,1926.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1925 (xsd:integer)
national origin	United States
capacity	four passengers (en)
crew	One (en)
designer	dbr:Harvey_C._Mummert
manufacturer	Aerial Engineering Corporation (en)
ref	Les Ailes, February 1926 (en)
type	Commercial transport aircraft (en)
has abstract	The Aerial Engineering Corporation Standard 6W-3 was a commercial transport modification of the US Standard J-1 biplane military trainer aircraft, with new wings, engine and accommodation for four passengers. First flown in 1925, it was built in small numbers. (en)
airfoil	Clark Y
ceiling m	4575 (xsd:integer)
cruise speed kmh	145 (xsd:integer)
empty weight kg	713 (xsd:integer)
eng1 hp	160 (xsd:integer)
eng1 name	Curtiss C-6
eng1 number	1 (xsd:integer)
eng1 type	water-cooled 6-cylinder inline (en)
gross weight kg	1198 (xsd:integer)
height m	3.330000 (xsd:double)
length m	8.200000 (xsd:double)
max speed kmh	169 (xsd:integer)
number built	<10 (en)
prop blade number	2 (xsd:integer)
prop dia m	2.600000 (xsd:double)
range km	580 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:Aerial_Engineering_Corporation_Standard_6W-3?oldid=1113329620&ns=0
page length (characters) of wiki page	6625 (xsd:nonNegativeInteger)
number built	10 (xsd:nonNegativeInteger)
designer	dbr:Harvey_C._Mummert
origin	United States
type	Airliner
foaf:isPrimaryTopicOf	wikipedia-en:Aerial_Engineering_Corporation_Standard_6W-3
is Link from a Wikipage to another Wikipage of	Standard J Aerial Service Mercury Standard 6W-3

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