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Statements

Subject Item
dbr:Boisavia_Anjou
rdf:type
yago:Cognition100023271 wikidata:Q11436 yago:Event100029378 dbo:Aircraft yago:Act100030358 owl:Thing umbel-rc:Model_airplane dbo:MeanOfTransportation yago:Activity100407535 yago:Abstraction100002137 yago:Type105840188 yago:PsychologicalFeature100023100 yago:Category105838765 yago:YagoPermanentlyLocatedEntity yago:Content105809192 yago:Kind105839024 yago:WikicatCancelledAircraftProjects schema:Product yago:Concept105835747 yago:Idea105833840 yago:Undertaking100795720 yago:Work100575741
rdfs:label
Boisavia Anjou Boisavia Anjou
rdfs:comment
Die Boisavia Anjou (später von SIPA als Sipavia Anjou weiterentwickelt) war ein Reiseflugzeug des französischen Herstellers Boisaiva. The Boisavia B.260 Anjou (later developed by SIPA as the Sipavia Anjou) was a four-seat twin-engine light aircraft developed in France in the 1950s. It was a low-wing cantilever monoplane of conventional configuration with retractable tricycle undercarriage. Intended by Boisavia as a touring aircraft, it did not find a market and only the single prototype was constructed. At this point, the firm sold the design to SIPA, which modified the design and re-engined it with Lycoming O-360 engines, but found that they could not sell it either. At a time when the twin-engine light plane market was already dominated by all-metal American aircraft, the Anjou's fabric-over-tube construction was something of an anachronism, and all development was soon ceased. Plans to develop a stretched version with
dcterms:subject
dbc:SIPA_aircraft dbc:Aircraft_first_flown_in_1956 dbc:Abandoned_civil_aircraft_projects dbc:1950s_French_civil_utility_aircraft dbc:Twin_piston-engined_tractor_aircraft dbc:Boisavia_aircraft dbc:Low-wing_aircraft
dbo:wikiPageID
12253879
dbo:wikiPageRevisionID
1123839860
dbo:wikiPageWikiLink
dbr:Société_Industrielle_Pour_l’Aéronautique dbr:United_States dbc:SIPA_aircraft dbc:Aircraft_first_flown_in_1956 dbr:Prototype dbr:Piston_engine dbr:Boisavia dbc:Abandoned_civil_aircraft_projects dbc:1950s_French_civil_utility_aircraft dbr:Landing_gear dbr:France dbr:Potez_4D dbc:Twin_piston-engined_tractor_aircraft dbr:Cantilever dbr:Regnier_4L dbr:SNECMA_Régnier_4L-02 dbr:Lycoming_O-360 dbc:Boisavia_aircraft dbr:1956_in_aviation dbr:Aluminium dbr:Monoplane dbc:Low-wing_aircraft dbr:SNECMA
dbo:wikiPageExternalLink
n13:Flugzeugtypen.asp%3FType=Link&ID=T3536&Name=S-261_Anjou&SID=128172970 n19:9700.htm
owl:sameAs
dbpedia-de:Boisavia_Anjou wikidata:Q154285 freebase:m.02vxrv2 yago-res:Boisavia_Anjou n23:Boisavia_Anjou n24:XnGy
dbp:spanM
13
dbp:stallSpeedKmh
90
dbp:wingAreaSqm
21.5
dbp:wikiPageUsesTemplate
dbt:Cvt dbt:SIPA_aircraft dbt:Infobox_Aircraft_Type dbt:Boisavia_aircraft dbt:Reflist dbt:Aircraft_specs dbt:Cite_book
dbp:primeUnits%3F_
met
dbp:firstFlight
1956-06-02
dbp:capacity
3
dbp:crew
1
dbp:fuelCapacity
in two wing tanks + 2x optional wing-tip tanks
dbp:manufacturer
dbr:Société_Industrielle_Pour_l’Aéronautique dbr:Boisavia
dbp:ref
Jane's All the World's Aircraft 1958-59
dbp:type
Civil utility aircraft
dbo:abstract
The Boisavia B.260 Anjou (later developed by SIPA as the Sipavia Anjou) was a four-seat twin-engine light aircraft developed in France in the 1950s. It was a low-wing cantilever monoplane of conventional configuration with retractable tricycle undercarriage. Intended by Boisavia as a touring aircraft, it did not find a market and only the single prototype was constructed. At this point, the firm sold the design to SIPA, which modified the design and re-engined it with Lycoming O-360 engines, but found that they could not sell it either. At a time when the twin-engine light plane market was already dominated by all-metal American aircraft, the Anjou's fabric-over-tube construction was something of an anachronism, and all development was soon ceased. Plans to develop a stretched version with three extra seats and Potez 4D engines were also abandoned. Die Boisavia Anjou (später von SIPA als Sipavia Anjou weiterentwickelt) war ein Reiseflugzeug des französischen Herstellers Boisaiva.
dbp:aspectRatio
7.6
dbp:ceilingM
6800
dbp:climbRateMs
6
dbp:climbRateNote
:::: on one engine at
dbp:cruiseSpeedKmh
240
dbp:cruiseSpeedNote
dbp:emptyWeightKg
1300
dbp:eng1Hp
170
dbp:eng1Name
dbr:SNECMA_Régnier_4L-02
dbp:eng1Note
::::
dbp:eng1Number
2
dbp:eng1Type
4
dbp:grossWeightKg
2000
dbp:heightM
3
dbp:lengthM
7.2
dbp:maxSpeedKmh
300
dbp:morePerformance
*Take-off run: *Landing run:
dbp:numberBuilt
1
dbp:propBladeNumber
2
dbp:propName
fixed-pitch propellers
dbp:rangeKm
1500
gold:hypernym
dbr:Aircraft
prov:wasDerivedFrom
wikipedia-en:Boisavia_Anjou?oldid=1123839860&ns=0
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5012
dbo:numberBuilt
1
dbo:manufacturer
dbr:Boisavia dbr:Société_Industrielle_Pour_l’Aéronautique
foaf:isPrimaryTopicOf
wikipedia-en:Boisavia_Anjou