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Statements

Subject Item
dbr:Franklin_O-425
rdfs:label
Franklin O-425
rdfs:comment
The Franklin O-425 (company designation 6AG/6V6) was an American air-cooled aircraft engine that first ran in the mid-1940s. The engine was of six-cylinder, horizontally-opposed layout and displaced 425 cu in (7 L). The power output was between 240 hp (179 kW) and 285 hp (213 kW) depending on variant. The O-405-13 (6V6-300-D16FT) of 1955 was a vertically mounted, turbocharged and fan cooled version for helicopters.
dcterms:subject
dbc:Franklin_aircraft_engines dbc:1940s_aircraft_piston_engines dbc:Boxer_engines
dbo:wikiPageID
38302257
dbo:wikiPageRevisionID
1110204357
dbo:wikiPageWikiLink
dbr:Republic_RC-3_Seabee dbr:80_Octane dbr:Horizontally-opposed dbr:Sikorsky_S-52 dbc:Franklin_aircraft_engines dbr:Turbocharger dbr:Aircraft_engine dbr:Stinson_L-13 dbr:Piston dbr:Flat-six_engine dbc:Boxer_engines dbr:Lycoming_O-480 dbc:1940s_aircraft_piston_engines dbr:List_of_aircraft_engines dbr:Continental_O-470 dbr:Franklin_Engine_Company dbr:Engine_displacement
dbo:wikiPageExternalLink
n9:isbn_9781557509390
owl:sameAs
wikidata:Q48834704 n16:4Wwzu
dbp:similarEngines
*Continental O-470 *Lycoming O-480
dbp:valvetrain
1
dbp:wikiPageUsesTemplate
dbt:Pistonspecs dbt:Franklin_aeroengines dbt:Cite_book dbt:Aircontent dbt:US_military_piston_aeroengines dbt:Infobox_Aircraft_Engine dbt:Convert dbt:Cvt dbt:Reflist
dbp:nationalOrigin
United States
dbp:manufacturer
dbr:Franklin_Engine_Company
dbp:power
:*Take-off: at 3,300 rpm :*Normal: at 3,200 rpm at sea level :*Cruise: at 2,840 rpm at sea level
dbp:ref
Aircraft engines of the World 1950.
dbp:type
6 dbr:Piston dbr:Aircraft_engine
dbo:abstract
The Franklin O-425 (company designation 6AG/6V6) was an American air-cooled aircraft engine that first ran in the mid-1940s. The engine was of six-cylinder, horizontally-opposed layout and displaced 425 cu in (7 L). The power output was between 240 hp (179 kW) and 285 hp (213 kW) depending on variant. The O-405-13 (6V6-300-D16FT) of 1955 was a vertically mounted, turbocharged and fan cooled version for helicopters.
dbp:compression
7.4
dbp:coolingsystem
Air-cooled
dbp:firstRun
1944
dbp:fuelsystem
1
dbp:fueltype
80
dbp:lists
*List of aircraft engines
dbp:oilsystem
Pressure system at
n14:weight
*Reduction gear: Planetary reduction gearing at 0.623:1
prov:wasDerivedFrom
wikipedia-en:Franklin_O-425?oldid=1110204357&ns=0
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4601
foaf:isPrimaryTopicOf
wikipedia-en:Franklin_O-425