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#1
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#1 Rear Still Hot
So the factory remans are in and I have 30+ hours on them. The breakin went smoothly, temps and oil consumption are down and everything is going great except for my old nemesis - high #1 rear cylinder head temps. Argh!
Up here in Canada I am flying around in 0 to -20C and even then I am breaking 400 degrees on #1 rear often and have to crack open the rear cowl flaps. Not normal and not great! Here is the data from a very recent flight on the NEW ENGINES:https://www.savvyanalysis.com/flight...1-9ec59eaf0ef8 I did have this problem though a little less pronounced with the old, original engines as seen here - https://www.savvyanalysis.com/flight...0-e62f33991d3d Obviously, the fact that this problem has followed me through both sets of engines points to the fact that the root of my problem is NOT the engines at all. In our never ending quest to fix the snag we have checked and redone all the baffling in the rear, rerouted the air intake hose that was slightly over #1R and gone so far as to use the high heat sealant to caulk and attach the metal baffles to the cylinder heads forcing all air past the cylinder fins (there were a few openings and holes etc.). A friend of mine (Hi John) has the identical year 337G and he has difficulty getting his engines hot enough this time of year and is constantly bragging about taking off with his cowl flaps closed. This, of course drives me crazy as I am bewildered how a seemingly identical piece of hardware can create such different results. Obviously all airplanes are different and mine is French after all so it is even more so BUT I really want to get to the bottom of this puzzle. Help!
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TC 1977 Reims Built F337G CYFD |
#2
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Follow Up Question...
On both front and rear engine #1 & #2 start out colder for both EGT & CHT. The only difference on the front engine the temps all converge and stay together for the most part once warmed up whereas in the rear #1 just stays much hotter. Not sure if them initially being colder means anything or if that is normal?
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TC 1977 Reims Built F337G CYFD |
#3
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Are we positive the CHT is really 400....?? Just a thought here but have you tried swapping the CHT probe from the suspect cylinder to another cylinder and vice versa? Are these the same probes in the exact same locations from the previous engines? It would be an interesting experiment nonetheless. If swapping probes leads to the same temps, then you know the 400 is valid.
I know another favorite of Mike Busch is to check the flow of the injector for that cylinder. Maybe that single injector is all jacked up. Just a thought.... Good Luck my friend! I feel your pain. Ed |
#4
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Quote:
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TC 1977 Reims Built F337G CYFD |
#5
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OK, I was hoping you had the same old probes in the same locations on the new engines as in the old engines. If that were the case, I thought a likely probe issue but that would appear not the case based on your probe swapping attempts.
I agree it is probably unlikely your new GAMI injector has an issue but it would still be worth verifying. It's not impossible. I'm guessing you have a relationship with Savvy Maintenance and Mike Busch.?.? What do they say about that cylinder temp and what to attempt to do to solve the problem? |
#6
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A picture of all of the baffling around the engine would certainly be helpful.
Dave |
#7
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Also should put the factory cht probe on the #1 cyl to confirm temps.
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_________ John K 1977 337G CNC3 |
#8
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Quote:
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Did they re-use the harness from the old GEM or lay in a new harness?
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_________ John K 1977 337G CNC3 |
#9
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Also, I neglected to mention rigging in my previous posts. Crucially important that pushing the mixture lever forward pushes the mixture control on the pump to the forward stop.
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_________ John K 1977 337G CNC3 |
#10
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Bunch of thoughts here; some of which you and I have discussed. I'll break it down into a few different posts.
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_________ John K 1977 337G CNC3 |
#11
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Front engine
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Looking at the data I think there's one or two smoking guns and it's the fuel flows and possibly timing. I've attached two flights from this week; one yours and one mine so we have similar ambient temps, etc. The book calls for 18.1GPH takeoff fuel flows and the conventional wisdom has been to pad that a bit. Comparing the two, your front engine ranges from 17.6GPH to 17.8GPH at takeoff power and my front engine seems to stay at 18.3GPH. So the front needs more fuel. The other thing to look at is ignition timing and the rate with which your cylinder temps rise. Your CHT's climb FAST and this can be an indication of timing that's advanced. As a matter of fact, I'm going to be checking my timing for the opposite reason; I think mine might be a degree or two retarded. Action items:
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_________ John K 1977 337G CNC3 Last edited by kilr4d : 02-11-19 at 07:45 PM. |
#12
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Rear engine
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The rear engine (except for cyl#1) is way happier than the front....higher fuel flow, gentler CHT rise, consistently cooler temps, etc. From what I see the #1 cylinder is an isolated issue. Action items:
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_________ John K 1977 337G CNC3 Last edited by kilr4d : 02-11-19 at 09:28 AM. |
#13
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I know it's a pain in the butt to get work done away from your home 'drome but there's a couple other guys around that should take a look at your plane. This needs a methodical process of elimination starting with the basics...fuel and spark.
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_________ John K 1977 337G CNC3 |
#14
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Good Advice
I am with John - if you have eliminated the easy stuff (Indication issue), you need to look at Fuel, spark and timing.
Some great articles to read were written a few years ago by John Deakin on Avweb, and you can still find them: https://www.avweb.com/news/pelican/182084-1.html https://www.avweb.com/news/pelican/182179-1.html These are just 2 links to get you started - but essential reading to bring focus to the relationship that fuel air mixture and spark have to do with you CHT. Jeff |