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…I am looking for information relative to the Pratt and Whitney R- 1340 series engines, particulary the model called the Hornet with a propellor shaft ratio of 0:67:1 ratio. I understand it had a slightly larger cylinder bore and was in use in the mid 30's as well as 1950 and 1960 era as a power plant for the Canadian built DeHavilland Otter. 204.112.125.42 17:21, 5 September 2007 (UTC) ybbob@mts.net
Where does May 1931 came from as a start of designing the Twin Wasp? AFAIK design process started in 1929... Besides, I find hard to believe that just after a few months of designing an engine it is ready for a tests... —Preceding unsigned comment added by Tizoc ( talk • contribs) 21:19, 19 January 2008 (UTC)
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content assessment scale. It is of interest to the following WikiProjects: | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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…I am looking for information relative to the Pratt and Whitney R- 1340 series engines, particulary the model called the Hornet with a propellor shaft ratio of 0:67:1 ratio. I understand it had a slightly larger cylinder bore and was in use in the mid 30's as well as 1950 and 1960 era as a power plant for the Canadian built DeHavilland Otter. 204.112.125.42 17:21, 5 September 2007 (UTC) ybbob@mts.net
Where does May 1931 came from as a start of designing the Twin Wasp? AFAIK design process started in 1929... Besides, I find hard to believe that just after a few months of designing an engine it is ready for a tests... —Preceding unsigned comment added by Tizoc ( talk • contribs) 21:19, 19 January 2008 (UTC)