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Statements

Subject Item
dbr:Davis_DA-5
rdf:type
wikidata:Q11436 yago:Content105809192 yago:Type105840188 umbel-rc:Model_airplane schema:Product yago:Cognition100023271 dbo:Aircraft yago:Abstraction100002137 yago:Concept105835747 owl:Thing yago:PsychologicalFeature100023100 yago:Idea105833840 yago:Category105838765 dbo:MeanOfTransportation yago:Kind105839024
rdfs:label
Davis DA-5
rdfs:comment
The Davis DA-5, a.k.a. DA-5A, is a single-seat sport aircraft designed in the United States in the 1970s and marketed for homebuilding. Like designer Leeon D. Davis's successful DA-2, it is a low-wing monoplane with fixed tricycle undercarriage and a V-tail, but with a much narrower fuselage accommodating only the pilot, and a lengthened nose. Design work was carried out in 1972, but the prototype was not built until 1974, when it was completed in only 67 days.
dcterms:subject
dbc:V-tail_aircraft dbc:Aircraft_first_flown_in_1974 dbc:1970s_United_States_sport_aircraft dbc:Single-engined_tractor_aircraft dbc:Low-wing_aircraft dbc:Homebuilt_aircraft dbc:Davis_aircraft
dbo:wikiPageID
15813782
dbo:wikiPageRevisionID
1016919023
dbo:wikiPageWikiLink
dbr:Davis_DA-2 dbc:Aircraft_first_flown_in_1974 dbc:V-tail_aircraft dbc:1970s_United_States_sport_aircraft dbr:V-tail dbr:Continental_A65 dbc:Low-wing_aircraft dbc:Single-engined_tractor_aircraft dbr:Homebuilt_aircraft dbr:1974_in_aviation dbr:Leeon_D._Davis dbc:Davis_aircraft dbc:Homebuilt_aircraft
dbo:wikiPageExternalLink
n17:davisda2.com
owl:sameAs
wikidata:Q5241881 n18:4j2x3 n19:Davis_DA-5 freebase:m.03nwnbc
dbp:spanFt
15
dbp:spanIn
7
dbp:stallSpeedMph
60
dbp:wingAreaSqft
57.2
dbp:wikiPageUsesTemplate
dbt:Aircraft_specs dbt:Aircontent dbt:Cite_book dbt:Davis_aircraft dbt:Infobox_Aircraft_Type dbt:Aero-1970s-stub dbt:Convert dbt:Reflist
dbp:primeUnits%3F_
imp
dbp:firstFlight
1974-07-22
dbp:crew
1
dbp:designer
dbr:Leeon_D._Davis
dbp:heightFt
4
dbp:heightIn
5
dbp:lengthFt
15
dbp:manufacturer
dbr:Homebuilt_aircraft
dbp:ref
Jane's All the World's Aircraft 1976–77
dbp:type
Sport aircraft
dbo:abstract
The Davis DA-5, a.k.a. DA-5A, is a single-seat sport aircraft designed in the United States in the 1970s and marketed for homebuilding. Like designer Leeon D. Davis's successful DA-2, it is a low-wing monoplane with fixed tricycle undercarriage and a V-tail, but with a much narrower fuselage accommodating only the pilot, and a lengthened nose. Design work was carried out in 1972, but the prototype was not built until 1974, when it was completed in only 67 days.
dbp:airfoil
Clark Y
dbp:aspectRatio
4.26
dbp:ceilingFt
14500
dbp:climbRateFtmin
800
dbp:cruiseSpeedMph
120
dbp:cruiseSpeedNote
dbp:emptyWeightLb
460
dbp:eng1Hp
65
dbp:eng1Name
dbr:Continental_A65
dbp:eng1Number
1
dbp:eng1Type
horizontally-opposed four-cylinder piston engine
dbp:lengthIn
9
dbp:maxSpeedMph
160
dbp:maxSpeedNote
at sea level
dbp:maxTakeoffWeightLb
775
dbp:morePerformance
*Takeoff run to 50 ft : *Landing run from 50 ft :
dbp:neverExceedSpeedMph
170
dbp:propBladeNumber
2
dbp:propDiaFt
5
dbp:propDiaIn
0
dbp:propName
Hegy type 60-70 fixed pitch wooden propeller
dbp:rangeMiles
450
gold:hypernym
dbr:Aircraft
prov:wasDerivedFrom
wikipedia-en:Davis_DA-5?oldid=1016919023&ns=0
dbo:wikiPageLength
3809
dbo:designer
dbr:Leeon_D._Davis
dbo:manufacturer
dbr:Homebuilt_aircraft
foaf:isPrimaryTopicOf
wikipedia-en:Davis_DA-5