Franklin O-200

O-200/4AC-199
Franklin O-200 engine on display at the Hiller Aviation Museum
Type Piston aircraft engine
National origin United States
Manufacturer Franklin Engine Company
First run 1941

The Franklin O-200 (company designation 4AC-199) was an American air-cooled aircraft engine of the early 1940s. The engine was of four-cylinder, horizontally-opposed layout and displaced 200 cu in (3 L). The power output ranged between 65 hp (48 kW) and 100 hp (75 kW) depending on variant. The O-200-5 (4ACG-199) featured a geared propeller drive.

Variants

4AC-199
O-200-1
O-200-3
O-200-7
O-200-9
4ACG-199
O-200-5

Applications

Direct drive

Geared drive

Specifications (0-200-5/4ACG-199)

Data from

General characteristics

  • Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
  • Bore: 4.25 in (108 mm)
  • Stroke: 3.5 in (88.9 mm)
  • Displacement: 198.6 in³ (3.25 L)
  • Dry weight: 224 lb (102 kg)

Components

  • Cooling system: Air-cooled

Performance

  • Power output: 102 hp (76 kW) at 3,500 rpm

See also

Comparable engines

Related lists

References

Notes
    Bibliography

    • Gunston, Bill. (1986) World Encyclopedia of Aero Engines. Patrick Stephens: Wellingborough. p. 57
    This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.