About: Sawyer Skyjacker II

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The Sawyer Skyjacker II is an American homebuilt aircraft that was designed and produced by Ralph V. Sawyer of Lancaster, California, in 1974. It first flew on 3 July 1975. The aircraft was intended as a research project and as such only one was built.

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
rdfs:label	Sawyer Skyjacker II (en)
rdfs:comment	The Sawyer Skyjacker II is an American homebuilt aircraft that was designed and produced by Ralph V. Sawyer of Lancaster, California, in 1974. It first flew on 3 July 1975. The aircraft was intended as a research project and as such only one was built. (en)
dcterms:subject	Sawyer aircraft Homebuilt aircraft Single-engined pusher aircraft Aircraft first flown in 1975 1970s United States experimental aircraft Mid-wing aircraft
Wikipage page ID	40832790 (xsd:integer)
Wikipage revision ID	1092440183 (xsd:integer)
Link from a Wikipage to another Wikipage	Homebuilt aircraft United States Sawyer aircraft Lycoming O-360 Stall (flight) Tandem Aluminum Homebuilt aircraft Single-engined pusher aircraft Aircraft canopy Aircraft engine Aircraft registration Aircraft first flown in 1975 Federal Aviation Administration Pusher configuration 1970s United States experimental aircraft Mid-wing aircraft Lancaster, California Tricycle landing gear Aspect ratio (wing) Experimental aircraft Mid-wing Four stroke Fuel-injected Spin (flight) Wheel pants
Link from a Wikipage to an external page	http://svsm.org/gallery/skyjacker http://www.airport-data.com/aircraft/N7317.html
sameAs	Sawyer Skyjacker II Sawyer Skyjacker II Sawyer Skyjacker II
span ft	18 (xsd:integer)
span in	0 (xsd:integer)
stall speed mph	45 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:Short_description dbt:Use_American_English dbt:Use_dmy_dates dbt:Aircraft_specs
dbp:primeUnits%3F_	imp (en)
first flight	1975-07-03 (xsd:date)
national origin	United States
capacity	one passenger (en)
crew	one (en)
designer	Ralph V. Sawyer (en)
length ft	18 (xsd:integer)
ref	Plane and Pilot (en)
status	Production completed (en)
type	Homebuilt aircraft Experimental aircraft
has abstract	The Sawyer Skyjacker II is an American homebuilt aircraft that was designed and produced by Ralph V. Sawyer of Lancaster, California, in 1974. It first flew on 3 July 1975. The aircraft was intended as a research project and as such only one was built. (en)
climb rate ftmin	400 (xsd:integer)
cruise speed mph	105 (xsd:integer)
empty weight lb	1650 (xsd:integer)
eng1 hp	200 (xsd:integer)
eng1 name	Lycoming O-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	0 (xsd:integer)
max speed mph	130 (xsd:integer)
number built	One (en)
produced	1974 (xsd:integer)
range miles	525 (xsd:integer)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:Sawyer_Skyjacker_II?oldid=1092440183&ns=0
page length (characters) of wiki page	5715 (xsd:nonNegativeInteger)
production end year	1974-01-01 (xsd:gYear)
production start year	1974-01-01 (xsd:gYear)
origin	United States
type	Experimental aircraft
foaf:isPrimaryTopicOf	wikipedia-en:Sawyer_Skyjacker_II
is Link from a Wikipage to another Wikipage of	List of aircraft (Sa) List of experimental aircraft

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