93 928 gts oil consumption
#227
I'll have to check it out. Need to filter out the eventual whining.
#228
I have seen this bulletin many years go- now that I have a GTS with a blown motor do you think I can write to Porsche and ask them for a new set of R2 rods? One could argue that the original motor from my GTS was stripped for maintenance [when it TBF'd].
I have a mind to pull a gudgeon pin from one of my pistons just to see if there are any signs of wear on the pin if anyone is interested.
By the way has anyone actually seen a R1 rod fail becuase of the perceived weakness Porsche chose to strengthen. that they did so just after the GTS was released suggggests to me they should have issued a general recall of all GTS motors but then of course they were all but bust at the time.
I have a mind to pull a gudgeon pin from one of my pistons just to see if there are any signs of wear on the pin if anyone is interested.
By the way has anyone actually seen a R1 rod fail becuase of the perceived weakness Porsche chose to strengthen. that they did so just after the GTS was released suggggests to me they should have issued a general recall of all GTS motors but then of course they were all but bust at the time.
I've never seen a broken R1 rod, unless the bearings spun, first.
#229
The added material is in what I consider the big end and right next to the rod bolt saddle. Porsche calls it the "connecting rod bolt surface," but I think saddle is catchier. See below:
Attachment 816075
It would make sense that a failing rod might start pulling up, rotating, and binding the bolt in R1 rods. Specifically, the edge of the narrow saddle might bite into the bolt allow this failure mode.
Now that I am back from PR, I can see Rob's failed R1 rod bolts in fact sticking out a bit on the top in the debris (which proves nothing.) Here's a photo from an earlier thread:
I recall reading from some document that the problem was nuts backing up. I may have confused this with the criterion for rod replacement, which is a possibility. Human memory is a living thing.
I am also seeing Rob's piston pin photos for the first time with any clarity on my computer. I don't think one can draw any conclusions from those since they came from a failed engine. If you have metal in the oil, anything can wear/fail in many/any way, including the piston wrist pins. It would be more informative to see GTS piston pins which come from an engine that didn't fail catastrophically.
Attachment 816075
It would make sense that a failing rod might start pulling up, rotating, and binding the bolt in R1 rods. Specifically, the edge of the narrow saddle might bite into the bolt allow this failure mode.
Now that I am back from PR, I can see Rob's failed R1 rod bolts in fact sticking out a bit on the top in the debris (which proves nothing.) Here's a photo from an earlier thread:
I recall reading from some document that the problem was nuts backing up. I may have confused this with the criterion for rod replacement, which is a possibility. Human memory is a living thing.
I am also seeing Rob's piston pin photos for the first time with any clarity on my computer. I don't think one can draw any conclusions from those since they came from a failed engine. If you have metal in the oil, anything can wear/fail in many/any way, including the piston wrist pins. It would be more informative to see GTS piston pins which come from an engine that didn't fail catastrophically.
I've become a sort of a detective, having seen so many engines apart and so many engines fail, over the years. Racing gave me plenty of engines to look at.....
If you can't figure out what happened to the engine that is blown up in front of you, how would you be able to ensure the next one doesn't do the same thing? I had a good friend who used to say, "You have to be 1% smarter than what you are working on!"
There are clues to every failure, if you are logical. "Advanced reading of the tea leaves."
Anytime a fastener to a rod breaks or becomes compromised, an engine fail dramatically, very quickly. The rod simply will not stay on the crankshaft for more than a few seconds, before the forces tear the rod into pieces. This leaves its own set of clues. There will be pieces of rod bearing that will still be intact...all of the layer will still be attached and it will look normal. This is because the rod separates at the parting line and part of the bearing will remain untouched.
Clearly, Rob's failure was bearing first....there was barely any of the steel backing left and the crank was worn considerably.
#231
It would be nice to convert my 90 S4 motor to GTS spec but the more I read the more I reckon it is probably better to leave it as an S4. Even the 8 bob crank seems to get indifferent reviews from you experts.
Regards
Fred
#232
I am not necessarily saying that the conrod nuts backing off is the reason for the engine failure. Since it's 2/6 journal, it's probably more likely the usual 928 problem of sending anything but oil to the 2/6 journal. If it were some other journal, then I'd entertain more novel theories more seriously as the underlying cause. I am merely commenting on how it's possible that the nuts came off from the bolts in one piece, regardless of what the original failure cause was, which I understood to be the question asked.
When the rod fastener fails at high rpm, I would expect the engine to stop rotating in a short number of cycles. However, if the rod fastener fails at low rpms, it may not be as instantaneous. If the redline rpm is 6000, and the rod fastener starts to fail at 1500 rpm, then it's only being subjected to about 6% of the forces that it would be subject to at 6000 rpm. This makes me believe that things can happen at cruise rpms that would never happen at redline rpm. If Rob's engine failed at cruise rpm, rod bolt or nut backing off relatively slowly is a lot more plausible theory than if it failed at the redline rpm.
It appears from a casual search that airplane and marine engines have conrod nuts back off relatively frequently compared to other kinds of failures. Those engines are often operated at very low rpms (relative to redline) for long periods of time. Especially airplane engine failures get researched thoroughly, so there are a lot interesting investigative techniques for doing post mortems on piston aircraft engines. For example, if the rod nut backs off while the engine is still running for a little while, one can see coked oil on the rod cap in the area that is usually covered by the rod nut. The same holds for the rod bolt backing off from the saddle, if there's coked oil on the saddle the bolt backed off before the engine stopped.
If the engine rattled (at cruise rpm) for a while before stopping, that could be consistent with the rod running with the rod cap loose. (It would also be consistent with garden variety rod bearing issue.) The rod running loose, even if properly oiled, will generate a very large amount of heat even at cruise rpm. The resulting bearing shell and journal will probably look just like a garden variety rod bearing failure due to oil starvation, even though the bearing was never starved of oil.
So I guess my questions to Rob would be the following:
- Did the engine fail at cruise rpm or near redline rpm? If it was closer to cruise rpm, then rod bolt or nut backing off slowly is more plausible theory. If it was closer to redline rpm, then oil starvation is the more plausible theory.
- Did the rod big end "saddle" have oil coked under where the bolt should have been covering the surface? How about the cap under the nut? If there's oil coking there, then the fastener backing up is a more plausible theory.
When the rod fastener fails at high rpm, I would expect the engine to stop rotating in a short number of cycles. However, if the rod fastener fails at low rpms, it may not be as instantaneous. If the redline rpm is 6000, and the rod fastener starts to fail at 1500 rpm, then it's only being subjected to about 6% of the forces that it would be subject to at 6000 rpm. This makes me believe that things can happen at cruise rpms that would never happen at redline rpm. If Rob's engine failed at cruise rpm, rod bolt or nut backing off relatively slowly is a lot more plausible theory than if it failed at the redline rpm.
It appears from a casual search that airplane and marine engines have conrod nuts back off relatively frequently compared to other kinds of failures. Those engines are often operated at very low rpms (relative to redline) for long periods of time. Especially airplane engine failures get researched thoroughly, so there are a lot interesting investigative techniques for doing post mortems on piston aircraft engines. For example, if the rod nut backs off while the engine is still running for a little while, one can see coked oil on the rod cap in the area that is usually covered by the rod nut. The same holds for the rod bolt backing off from the saddle, if there's coked oil on the saddle the bolt backed off before the engine stopped.
If the engine rattled (at cruise rpm) for a while before stopping, that could be consistent with the rod running with the rod cap loose. (It would also be consistent with garden variety rod bearing issue.) The rod running loose, even if properly oiled, will generate a very large amount of heat even at cruise rpm. The resulting bearing shell and journal will probably look just like a garden variety rod bearing failure due to oil starvation, even though the bearing was never starved of oil.
So I guess my questions to Rob would be the following:
- Did the engine fail at cruise rpm or near redline rpm? If it was closer to cruise rpm, then rod bolt or nut backing off slowly is more plausible theory. If it was closer to redline rpm, then oil starvation is the more plausible theory.
- Did the rod big end "saddle" have oil coked under where the bolt should have been covering the surface? How about the cap under the nut? If there's oil coking there, then the fastener backing up is a more plausible theory.
Last edited by ptuomov; 03-18-2014 at 04:23 PM.
#234
I was in the far left lane, 4th gear, ~4000 rpm for 5-7 miles uphill, when the temp gauge rose, and the oil pressure gauge dropped to ~2.5 bar. Dropped over a lane or two, put it in 5th, turned on the heat, and lugged it for a while while I was thinking about what to do. so probably 2700 rpm or so in 5th gear. Put up the windows so I could actually hear the motor, I heard an audible rod knock for a couple of seconds just as I was passing the Tejon pass sign, and it let go in a big way- audible explosion, and felt it through the wheel, my feet, my butt... Much more explosive than when the interim motor in the Zombie let go, and there's a lot more insulation between motor and me in the GTS. The jolt was probably the #2 rod being bent 90 degrees between the crank and the block:
The crank was worn .040" on backside of the 2/6 throw, and the crank ws bent .008"
So it was turning less than 3K when it went.
RE: the coking under the rod bolt end, dunno. I think I still have the pieces, somewhere.
The crank was worn .040" on backside of the 2/6 throw, and the crank ws bent .008"
So it was turning less than 3K when it went.
RE: the coking under the rod bolt end, dunno. I think I still have the pieces, somewhere.
#235
I am not necessarily saying that the conrod nuts backing off is the reason for the engine failure. Since it's 2/6 journal, it's probably more likely the usual 928 problem of sending anything but oil to the 2/6 journal. If it were some other journal, then I'd entertain more novel theories more seriously as the underlying cause. I am merely commenting on how it's possible that the nuts came off from the bolts in one piece, regardless of what the original failure cause was, which I understood to be the question asked.
When the rod fastener fails at high rpm, I would expect the engine to stop rotating in a short number of cycles. However, if the rod fastener fails at low rpms, it may not be as instantaneous. If the redline rpm is 6000, and the rod fastener starts to fail at 1500 rpm, then it's only being subjected to about 6% of the forces that it would be subject to at 6000 rpm. This makes me believe that things can happen at cruise rpms that would never happen at redline rpm. If Rob's engine failed at cruise rpm, rod bolt or nut backing off relatively slowly is a lot more plausible theory than if it failed at the redline rpm.
It appears from a casual search that airplane and marine engines have conrod nuts back off relatively frequently compared to other kinds of failures. Those engines are often operated at very low rpms (relative to redline) for long periods of time. Especially airplane engine failures get researched thoroughly, so there are a lot interesting investigative techniques for doing post mortems on piston aircraft engines. For example, if the rod nut backs off while the engine is still running for a little while, one can see coked oil on the rod cap in the area that is usually covered by the rod nut. The same holds for the rod bolt backing off from the saddle, if there's coked oil on the saddle the bolt backed off before the engine stopped.
If the engine rattled (at cruise rpm) for a while before stopping, that could be consistent with the rod running with the rod cap loose. (It would also be consistent with garden variety rod bearing issue.) The rod running loose, even if properly oiled, will generate a very large amount of heat even at cruise rpm. The resulting bearing shell and journal will probably look just like a garden variety rod bearing failure due to oil starvation, even though the bearing was never starved of oil.
So I guess my questions to Rob would be the following:
- Did the engine fail at cruise rpm or near redline rpm? If it was closer to cruise rpm, then rod bolt or nut backing off slowly is more plausible theory. If it was closer to redline rpm, then oil starvation is the more plausible theory.
- Did the rod big end "saddle" have oil coked under where the bolt should have been covering the surface? How about the cap under the nut? If there's oil coking there, then the fastener backing up is a more plausible theory.
When the rod fastener fails at high rpm, I would expect the engine to stop rotating in a short number of cycles. However, if the rod fastener fails at low rpms, it may not be as instantaneous. If the redline rpm is 6000, and the rod fastener starts to fail at 1500 rpm, then it's only being subjected to about 6% of the forces that it would be subject to at 6000 rpm. This makes me believe that things can happen at cruise rpms that would never happen at redline rpm. If Rob's engine failed at cruise rpm, rod bolt or nut backing off relatively slowly is a lot more plausible theory than if it failed at the redline rpm.
It appears from a casual search that airplane and marine engines have conrod nuts back off relatively frequently compared to other kinds of failures. Those engines are often operated at very low rpms (relative to redline) for long periods of time. Especially airplane engine failures get researched thoroughly, so there are a lot interesting investigative techniques for doing post mortems on piston aircraft engines. For example, if the rod nut backs off while the engine is still running for a little while, one can see coked oil on the rod cap in the area that is usually covered by the rod nut. The same holds for the rod bolt backing off from the saddle, if there's coked oil on the saddle the bolt backed off before the engine stopped.
If the engine rattled (at cruise rpm) for a while before stopping, that could be consistent with the rod running with the rod cap loose. (It would also be consistent with garden variety rod bearing issue.) The rod running loose, even if properly oiled, will generate a very large amount of heat even at cruise rpm. The resulting bearing shell and journal will probably look just like a garden variety rod bearing failure due to oil starvation, even though the bearing was never starved of oil.
So I guess my questions to Rob would be the following:
- Did the engine fail at cruise rpm or near redline rpm? If it was closer to cruise rpm, then rod bolt or nut backing off slowly is more plausible theory. If it was closer to redline rpm, then oil starvation is the more plausible theory.
- Did the rod big end "saddle" have oil coked under where the bolt should have been covering the surface? How about the cap under the nut? If there's oil coking there, then the fastener backing up is a more plausible theory.
My background is racing, not airplanes, so hardware failures are instantly a disaster.
#238
I've never seen a broken R1 rod, unless the bearings spun, first.
__________________
Does it have the "Do It Yourself" manual transmission, or the superior "Fully Equipped by Porsche" Automatic Transmission? George Layton March 2014
928 Owners are ".....a secret sect of quietly assured Porsche pragmatists who in near anonymity appreciate the prodigious, easy going prowess of the 928."
Does it have the "Do It Yourself" manual transmission, or the superior "Fully Equipped by Porsche" Automatic Transmission? George Layton March 2014
928 Owners are ".....a secret sect of quietly assured Porsche pragmatists who in near anonymity appreciate the prodigious, easy going prowess of the 928."
#239
There was a local Porsche shop that was doing 968 engines and using Carrillos.
To increase their profits, they then were selling the 968 rods to the 951 guys.
Fixed a couple of those with broken/bent rods.