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#18
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"C J Campbell" wrote in message ... I think Deakin is worth reading, but some of what he says should be taken with a grain of salt. His columns are mostly based on experiments with his own highly modified Bonanza, a few high performance radial engines, and some theory. In fact, a careful reading of his columns will show no test data for the most common engine and propeller combinations in use today. You've not read hiscolumns about the test beds they've run at GAMI? The reasons for this are fairly simple -- few airplanes have the instrumentation that Deakin needs to test his theories. This is why Deakin's theories for running lean of peak remain a minority view. Granted, it is a very noisy minority, but remember that it is also a small minority. I think they have a point. They may even be right. But they don't have nearly the evidence that they think they have. See above. Deakin's remarks are mostly pertinent to running TCM engines, which are much different than engines from other manufacturers. I bellieve they run Lycoming on the test bed as well, everything from pipsqueaks to the big 540's. Not to put too fine a point on it, some TCM engines are the only ones I know of that so consistently develop cracks that the most part of an annual inspection basically consists of measuring and cataloging the spread of these cracks. The engine used in the early 70's Cessna T206 rarely made it to its 1400 hour TBO, for example. Barring solid data to the contrary (and Deakin, remember, does not give you solid data -- he only appears to do that), your airplane should be operated in accordance with the manufacturer's recommendations. This will ensure that you maintain your insurance coverage, if nothing else. I think GAMI generated enough data on their stand to run a computer dry. http://www.engineteststand.com/ |
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