This would be early 2000's maybe late 90's
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Originally posted by Scott View PostI think this illustrates the importance of maintaining a clean engine.
It can be seen even in the photos that this cylinder was cracked (up to 50% or more of the circumference) for quite some time prior to the final failure. The oil and soot buildup on the intake components and ignition wires below the cylinder is a telltail sign that the cylinder has been blowing oil and hot gases for a while.
Keep your engine clean and free of oil leaks and you'll see an impending failure before it develops this far. Just my opinion of courseN29787
'41 BC12-65
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Originally posted by Ragwing nut View Post
We had some O-300 cylinders here that was like that superior had to warranty.N29787
'41 BC12-65
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Pushrods tubes on the failed and adjacent cylinder, ignition wires and the tyraps that strap them to the intake, intake couplings and breez clamps, intake elbow on the adjacent cylinder, lifter housings, all look soaked with black grunge to me. It might be argued that what I see could have come from anything leaking in that area. The point is however that a crack like that will reveal itself if the engine is otherwise leak free and clean.
Oil between the fins in the vicinity of the cylinder-to-head joint is always cause for concern, but if everything is soaked and dirty how will you know. It's not going to show up during a compression test because the piston at tdc is beyond the crack. Oil leaking is your best hope of catching this before the catastrophic failure.Last edited by Scott; 09-16-2019, 22:45.Scott
CF-CLR Blog: http://c-fclr.blogspot.ca/
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Originally posted by astjp2 View Post
I wonder why it seems that I have only heard of O-300 failures and not 200? This is the first one I have actually seen in person. How many have you seen Mike? Tim
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Originally posted by Scott View PostPushrods tubes on the failed and adjacent cylinder, ignition wires and the tyraps that strap them to the intake, intake couplings and breez clamps, intake elbow on the adjacent cylinder, lifter housings, all look soaked with black grunge to me. It might be argued that what I see could have come from anything leaking in that area. The point is however that a crack like that will reveal itself if the engine is otherwise leak free and clean.
Oil between the fins in the vicinity of the cylinder-to-head joint is always cause for concern, but if everything is soaked and dirty how will you know. It's not going to show up during a compression test because the piston at tdc is beyond the crack. Oil leaking is your best hope of catching this before the catastrophic failure.
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Originally posted by astjp2 View Post
Actually Scott, the crank seal was leaking and was changed a couple of hours prior to the failure, that failure would not have put oil on the engine, even flying back it did not spray hardly any oil. I was mainly limited to the combustion chamber, even the pushrod tubes were still sealed surprisingly.
Anyway, here's what I see in the photo that suggests to me that if the engine had been otherwise clean and dry, the fatigue crack in that cylinder would have revealed itself reasonably clearly. While the area between the fins is not readily visible, there is evidence in this photo of liquid oil draining from the crack. Again, impossible to notice if the engine is otherwise generally wet with oil and grime, but if the engine is normally clean and dry.....
Scott
CF-CLR Blog: http://c-fclr.blogspot.ca/
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One reason to like the original alodine (gold) conversion coating that continental did on the cylinder heads.Scott
CF-CLR Blog: http://c-fclr.blogspot.ca/
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