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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.

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rdfs:label
  • Franklin O-425 (en)
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. (en)
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sameAs
similar engines
  • *Continental O-470 *Lycoming O-480 (en)
valvetrain
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national origin
  • United States (en)
manufacturer
power
  • :*Take-off: at 3,300 rpm :*Normal: at 3,200 rpm at sea level :*Cruise: at 2,840 rpm at sea level (en)
ref
  • Aircraft engines of the World 1950. (en)
type
has 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. (en)
compression
coolingsystem
  • Air-cooled (en)
first run
fuelsystem
fueltype
lists
  • *List of aircraft engines (en)
oilsystem
  • Pressure system at (en)
power/weight
  • *Reduction gear: Planetary reduction gearing at 0.623:1 (en)
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