Allen O-675

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search
O-675
TypeEight-cylinder horizontally opposed
National originUSA
ManufacturerAllen Aircraft Corporation
First run1927
Manufactured1928

The Allen Aircraft Engine Co. of Compton, a suburb of Los Angeles California, developed an eight-cylinder horizontally opposed aircraft engine during 1928–1929.

Little is known about this engine, other than that it was never given a Type Certificate and that it was not used on any known aircraft.

Specifications (O-675)

[edit | edit source]

Data from Aeroengines

General characteristics

Components

Performance

  • Power output: 200 hp@1800 rpm

References

[edit | edit source]
  • Aeroengines
  • Aerofiles.com
  • Ricardo Miguel, VidalLos Motores Aeroespaciales A-Z, (Spanish), 2002, p. 157, Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).