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![]() Water's vapor pressure rises with temperature, if you remember your physics. Raising the vapor pressure drives it of sooner. It doesn't have to boil. 180 is a recommendation. Below that, the water might form in the case faster than it will evaporate, and you'll have increasing amounts accumulating in the engine. The research is there. Here are some who have experience in the area: http://www.sacskyranch.com/corrosion.htm http://doc.tms.org/ezMerchant/prodtms.nsf/ProductLookupItemID/JOM-0505-54/$FILE/JOM-0505-54F.pdf?OpenElement http://www.ramaircraft.com/Maintenan...mendations.htm http://www.memagazine.org/backissues...italsigns.html Lots more if you Google it. Dan I hope you're just baiting me on this one, but you've left the door too wide open, and I have to go through it just once. I read all four of the web sites that you posted, and frankly I don't really see where you might think that any of them deal with the issue that I thought we were talking about by giving specific data on a comparison basis. You know, like stating the moisture content and acidity of sample A is such and such and from sample B it is such and such. So I'll comment on them one by one. Sacramento sky ranch...... This page shows pictures of rusted (not dissolved or corroded by acid) lifter faces and such and talks about how important it is to guard against it and how quickly it can occur. It gives the same advice that we have been talking about, the importance of frequent flights, oil changes, etc. I don't see where it gives a comparison of oil moisture content or acidity for oil sampled from frequently flown aircraft versus that sampled from engines that were only ground run. Do you? If so please tell me where. We all understand that oil eventually drains off engine parts and the moisture in the air will cause it to rust. I thought we were discussing whether or not oil deposited from a ground run-up would protect the cam or corrode it, right? Like I said, many places say that you must fly often to evaporate the moisture, but samples from each with numbers showing how much the moisture and acidity increases to detrimental levels when you only ground run the engine have been hard to find. Website #2.... This is an article where a comparison of the corrosion resistance of two different magnesium alloys is presented. I think it best to quote a part of the article here. From the article: "The internal corrosion response concentrates solely on the behavior of the alloy within the coolant circiut of the engine." That's means they're looking at how a new alloy's corrosion performance compares to an old one when exposed to anti-freeze. They didn't even consider the oil circulating through the block. Probably because they know it doesn't corrode things but protects them. I don't see how they answered any of our questions. The cases on my Lyc are made from A356 aluminum, and the cam and lifters from steel and iron. The corrosion response of a magnesium alloy to anti-freeze relates to the corrosive effect of oil from a ground run on a camshaft just how Dan? website #3....RAM Aircraft....This is just mostly the same stuff as what was on the Sac sky ranch site. Mostly good advice, but certainly nothing that demonstrates with scientific data that oil from a ground run has such and such moisture content and PH level. They did however demonstrate that knowledgeable people can have different opinions. From the article, [RAM service history records indicate that Mineral Based AD oils perform significantly better than synthetic and semi-synthetic oils.] I see that you have had better results from Aeroshell Semi-Synthetic, ![]() website #4....This article talks about new devices being developed that are beginning to monitor in real time the chemical condition of the oil in an engine. Didn't see data giving a comparison of the moisture content or PH of frequently run oil versus that from a ground run here either. Like I've said, maybe some people have done it, but I haven't seen it published. These devices will sure make that possible though. Maybe we will see something in the future! Yea! I really don't think that anyone would think that those sites gave good scientific data that supported the opinion that ground runs will corrode your engine, but every year there are several forced landings with fatalities, due to engine failure that would not have happened had the engines not been allowed to rust. Maybe those engines would have been saved had someone not been told to just let them sit if you can't fly them. That is why I felt I should respond. After all, the ONLY scientific data I have seen on the subject is my own oil analysis results that told me there is 0.0% moisture in my oil sample. I ground run maybe 6 or so times during the winter, in between flights that is, and only when flying is not safe. Blue skies, Rusty |
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What sort of oil analysis service are you using? This outfit
here http://www.oillab.com/oil.html says that water is detected at levels of 1% or more using the physical test, and most other contaminants using spectroscopic analysis. My understanding of the spectroscopic test is that they burn a small amount of the oil, run the light generated through a prism to split it into its colors, and analyze the spectrum to get an idea of the elements present. Water doesn't burn. If they're not using the ASTM tests, your water content numbers may be useless. 1% is a lot of water, and besides, much of the water that may have been in your oil may have already turned to acids. 1% water in 6 quarts of oil is 2 ounces, a third of a coffee cup. This argument could go on for a long time. It will someday be settled when you finally get an overhaul and the technician reports on what he finds. My experience, and the experience of many others, is that condensation is real and it wrecks engines. Dan |
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