Max EGT
Moderators: GAHorn, Karl Towle, Bruce Fenstermacher
- jatkins
- Posts: 218
- Joined: Mon Nov 18, 2002 7:33 pm
Max EGT
I cannot seem to find an absolute number for a max EGT. I realize that the max , will vary day to day , with altitude and temperature , as well with power settings. The reason I am looking for this value ,is I am installing a 6 cyl EGT guage , and I need to program it to the max value for the engine.I found the max CHT 525, but I cannot sem to locate the Max EGT ? Any one out there have a number / source ??
CF-HER
52 170B 20292
52 170B 20292
- jrenwick
- Posts: 2045
- Joined: Thu Apr 01, 2004 8:34 pm
There isn't any max EGT value; EGTs are not absolute values in the first place, because the temperature varies over the length of the exhaust path, so what you see depends a lot on where you inserted the probe. Assuming the probes are all at the same distance from the flange, then what's important is the temperatures of all the exhausts relative to each other. With fuel injection, they should be pretty close if the jets are balanced well. With a carburetor, expect to see variations of 100 degrees or more between cylinders. It's just in the nature of the beast, and you can't do much about it.
The electronic EGT instruments have high and low alarms. If you have the EI instrument, the manual has a recommendation for setting the maximum EGT limits, and I think it's some number of degrees above the highest reading you can get for each cylinder (I don't have the manual handy, or I'd look it up). I don't know what JPI recommends.
Best Regards,
John
The electronic EGT instruments have high and low alarms. If you have the EI instrument, the manual has a recommendation for setting the maximum EGT limits, and I think it's some number of degrees above the highest reading you can get for each cylinder (I don't have the manual handy, or I'd look it up). I don't know what JPI recommends.
Best Regards,
John
John Renwick
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
- jatkins
- Posts: 218
- Joined: Mon Nov 18, 2002 7:33 pm
I have installed the probes very close to the exact same location from the flange in all the exhaust stub pipes. I guess the value which I will
( should ) never exceed, is what I am looking for??
I do follow that what the gauge shows will depend on the temp, at the exact location of the probe, and the length of each stub pipe varies slightly.I am thinking that after flying it some I could reset the value up or down as required ?
( should ) never exceed, is what I am looking for??
I do follow that what the gauge shows will depend on the temp, at the exact location of the probe, and the length of each stub pipe varies slightly.I am thinking that after flying it some I could reset the value up or down as required ?
CF-HER
52 170B 20292
52 170B 20292
- jrenwick
- Posts: 2045
- Joined: Thu Apr 01, 2004 8:34 pm
What you set the max/min EGT values to is a matter of experimentation with your particular aircraft and installation. They may be different for each cylinder. The manufacturer's installation manual or user's guide should have instructions on how to do it.
The idea should be to set them such that the alarm will be activated whenever one of them goes outside of the "normal" range by some factor, and what's "normal" is really unique to each cylinder on your particular engine. There is no general guideline.
Best Regards,
John
The idea should be to set them such that the alarm will be activated whenever one of them goes outside of the "normal" range by some factor, and what's "normal" is really unique to each cylinder on your particular engine. There is no general guideline.
Best Regards,
John
John Renwick
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
- blueldr
- Posts: 4442
- Joined: Thu May 02, 2002 3:16 am
You're going to have to determine the highest or peak EGT for each unit and then decide if you're going to operate either rich or lean of that peak.
Most naturally aspirated engines cannot be over leaned at or above about six thousand ft.MSL. If you're flying below that altitude, be cautious leaning when at or over about 70% of max power.
On an O-300 engine the fuel mixture distribution is really too erratic to gain much from accurate instrumentation.
Most naturally aspirated engines cannot be over leaned at or above about six thousand ft.MSL. If you're flying below that altitude, be cautious leaning when at or over about 70% of max power.
On an O-300 engine the fuel mixture distribution is really too erratic to gain much from accurate instrumentation.
BL
- jrenwick
- Posts: 2045
- Joined: Thu Apr 01, 2004 8:34 pm
What BL said! You can use the EGT to lean the engine, but I long ago gave up doing that. I lean for peak RPM, sort of like what the owner's manual says to do, and then just monitor the EGT for something unusual going on. If you get a bad plug, the EGT (with a mag check) can tell you pretty quickly which one to look at. It can help you debug other problems as well, but as has been pointed out here in the past, for leaning, it's overkill for the O300. I like it mostly because I have additional sensors on it for oil temperature and oil pressure, and I can set limits that will light an idiot light. Because as I once heard Dick Rutan say, the gauge you're not looking at isn't working! 

John Renwick
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
-
- Posts: 70
- Joined: Sat Jan 29, 2005 5:38 pm
Howdy All,
After reading the info on this thread, I think I have a pretty good understanding of what has been stated. My 170 has a single probe EGT and no CHT. I have an 0300A with a D accessory case. I am not shy about leaning...even on the ground...and for run up and take off....field elevation is 2000'...On the ground and for take off I lean by the tach, in the air/cruise I have been leaning by the EGT. In cruise flight I lean to about 1325 degrees indicated on the EGT and then enrich the mixture to about 1250 degrees....I burn about 8 gallons an hour over all and cruise at 2450 rpm. My oil temps are good, well below red line and in the lower portion of the green arc.....Plug fouling is a thing of the past... I use avgas only.... Are these temps that I see displayed, are they in the "ball park"????? Should I just disregard the EGT and do all leaning by the tach? Any comment or suggestion would be appreciated...
Thanx,
Richard...
After reading the info on this thread, I think I have a pretty good understanding of what has been stated. My 170 has a single probe EGT and no CHT. I have an 0300A with a D accessory case. I am not shy about leaning...even on the ground...and for run up and take off....field elevation is 2000'...On the ground and for take off I lean by the tach, in the air/cruise I have been leaning by the EGT. In cruise flight I lean to about 1325 degrees indicated on the EGT and then enrich the mixture to about 1250 degrees....I burn about 8 gallons an hour over all and cruise at 2450 rpm. My oil temps are good, well below red line and in the lower portion of the green arc.....Plug fouling is a thing of the past... I use avgas only.... Are these temps that I see displayed, are they in the "ball park"????? Should I just disregard the EGT and do all leaning by the tach? Any comment or suggestion would be appreciated...
Thanx,
Richard...
Richard Haydon
'49 170A
Ducote Airpark TS65
'49 170A
Ducote Airpark TS65
- jrenwick
- Posts: 2045
- Joined: Thu Apr 01, 2004 8:34 pm
1250-1325 is lower than what I see on my EGT, but remember that the only valid comparison is between cylinders on the same engine. The temps you see depend very much on how far away the probe is from the flange, and there's no standard for that.
Another way to say it is, the readings are all relative to where you see the peak EGT value. One temperature reading, by itself, doesn't really mean anything.
At higher power settings, the danger of leaning to too high an EGT is that the exhaust valves don't get enough cooling, and they can burn.
If you're running at 75% power or less, you can lean to the absolute peak EGT without hurting the engine. And with our O300s, that's almost always the case. The Cessna recommended method of leaning until roughness and then enriching until smoothness returns is basically leaning to peak EGT on the first cylinder that peaks. All the others are running rich of peak. Your single EGT gauge may or may not be on the leanest cylinder, so unless you know it is, maybe leaning the recommended way will give you better performance. The problem is that with our carburetors, the fuel is distributed rather unevenly, and they'll all generally be running at different mixtures.
Another way to say it is, the readings are all relative to where you see the peak EGT value. One temperature reading, by itself, doesn't really mean anything.
At higher power settings, the danger of leaning to too high an EGT is that the exhaust valves don't get enough cooling, and they can burn.
If you're running at 75% power or less, you can lean to the absolute peak EGT without hurting the engine. And with our O300s, that's almost always the case. The Cessna recommended method of leaning until roughness and then enriching until smoothness returns is basically leaning to peak EGT on the first cylinder that peaks. All the others are running rich of peak. Your single EGT gauge may or may not be on the leanest cylinder, so unless you know it is, maybe leaning the recommended way will give you better performance. The problem is that with our carburetors, the fuel is distributed rather unevenly, and they'll all generally be running at different mixtures.
John Renwick
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
- blueldr
- Posts: 4442
- Joined: Thu May 02, 2002 3:16 am
Haydon,
The standard tach in this airplane is usually very difficult to read fine enough for leaning purposes. In my experience, the best method is as the factory recommends. Lean to roughness and then enrichen just to smoothness. If you are cruising at 2450 RPM and somewhere arounf six thousand feet MSL, your fuel burn is a little high by my experience. On a relatively long leg, I would expect the burn to run between 6.8 and 7.3 GPH.
Between my home base in California and Idaho with a cruise climb from 1600 MSL to 9500 MSL and a 7000 ft descent over about twenty minutes (About 350 ft/min.) I will usually burn about 6.7 GPH for the 3.9 hr. leg.
I'm running a 50 inch pitch and cruise at about 2550to 2600 RPM. My tach runs slow so I set the power with my electronic tach checker.
The standard tach in this airplane is usually very difficult to read fine enough for leaning purposes. In my experience, the best method is as the factory recommends. Lean to roughness and then enrichen just to smoothness. If you are cruising at 2450 RPM and somewhere arounf six thousand feet MSL, your fuel burn is a little high by my experience. On a relatively long leg, I would expect the burn to run between 6.8 and 7.3 GPH.
Between my home base in California and Idaho with a cruise climb from 1600 MSL to 9500 MSL and a 7000 ft descent over about twenty minutes (About 350 ft/min.) I will usually burn about 6.7 GPH for the 3.9 hr. leg.
I'm running a 50 inch pitch and cruise at about 2550to 2600 RPM. My tach runs slow so I set the power with my electronic tach checker.
BL
-
- Posts: 70
- Joined: Sat Jan 29, 2005 5:38 pm
Thank You John and "Blu-elder"
I have a lot of respect for my"elders and my betters." From now on I will lean by engine sound. Guess I will have to "duck tape" over the EGT gauge.... I would be inclined to remove it....but, the hole in the exhaust would probably whistle...warning George that I was about to pass him.......
Richard......


Richard......
Richard Haydon
'49 170A
Ducote Airpark TS65
'49 170A
Ducote Airpark TS65
- GAHorn
- Posts: 21295
- Joined: Fri Apr 12, 2002 8:45 pm
Ha!
Well,.. the instructions I have regarding the "factory" techniques for leaning do not mention "listening" or leaning for "roughness".
The instructions I have call for leaning very slowly to max RPM, then continuing to lean until the first sign of loss of RPM, then enrichening back to the point of max RPM. (My own technique is to push the mixture very slightly further rich from that point.)
There is a term called "Best Power" that is generally accepted as somewhat rich of peak EGT. While that may not give the absolute greatest range, it will give the best speed/shortest flight time all other things being equal. It is a bit richer (according to the texts I've read, anywhere from 50-100 degrees richer than peak EGT) than I personally enjoy. But it is where I prefer to be as opposed to the absolute leanest possible (within the capabilities of still having a smooth engine.)
I don't subscribe (or perhaps I just don't fully understand) to all the logic of Mr. Deakin...(aviation author) ... but he makes a good argument that an engine can be in a range of increasing RPM while leaning... yet have one or more cylinders that have become lean beyond peak. I can see the validity of that. (If 6 cylinders have 2 very rich, 2 almost at peak, and 2 right at peak EGT... then further leaning will take the 2 at peak beyond peak and down the lean-of-peak side of operations. Yet the 2 almost at peak cylinders have improved their horsepower output as have the 2 very rich cylinders. In other words, of the 6 available cyls, 4 have increased power output as they approached closer to peak EGT, while only 2 have begun the downhill slide on the other side of peak EGT. Therefore the engine may actually exhibit a slight increase in RPM despite the fact that two cylinders are lean of peak (LOP), 2 cyls are at peak, and 2 are rich of peak (ROP).
Also, it's been postulated that an engine running at peak, or even slightly rich of peak, can suffer damage as conditions change and one or more cylinders have cause to lean still further. (A change of density altitude, for example.) In the above example of the 6 cylinders.... any further leaning OR richening, regardless of cause....might place 2 cylinders at risk of excessive EGT. If the power setting of the engine is above 65%, it's possible to damage those cylinders that become leaner...because they are running hotter. Capt. Deakin makes a persuasive case for running lean of peak because further leaning will only result in a cooler EGT. Of course that can only be accomplished in properly instrumented, fuel injected engines. (And it ignores the possibility that an engine might have an equal chance of an inflight change that makes it run richer....and therefore hotter.)
The problem is, with our engines, we're back to measuring things with a micrometer when we use digital EGT gauges. We then mark it with a grease pencil when we are running a variable-length induction engine like this one. (Or when we're "listening" for roughness.) And we're then cutting it with a hatchet with this carburetor and mixture control. (Does it sound as if I have very low regard for digital gauges in these fairly crude engine installations we have?)
I am quite happy with using the tachometer, and my fuel burns average 7.8 gph and speeds run right at 104 kts/120 mph like the factory claims.
What is an EGT gauge going to tell me that I don't already know?
Well,.. the instructions I have regarding the "factory" techniques for leaning do not mention "listening" or leaning for "roughness".
The instructions I have call for leaning very slowly to max RPM, then continuing to lean until the first sign of loss of RPM, then enrichening back to the point of max RPM. (My own technique is to push the mixture very slightly further rich from that point.)
There is a term called "Best Power" that is generally accepted as somewhat rich of peak EGT. While that may not give the absolute greatest range, it will give the best speed/shortest flight time all other things being equal. It is a bit richer (according to the texts I've read, anywhere from 50-100 degrees richer than peak EGT) than I personally enjoy. But it is where I prefer to be as opposed to the absolute leanest possible (within the capabilities of still having a smooth engine.)
I don't subscribe (or perhaps I just don't fully understand) to all the logic of Mr. Deakin...(aviation author) ... but he makes a good argument that an engine can be in a range of increasing RPM while leaning... yet have one or more cylinders that have become lean beyond peak. I can see the validity of that. (If 6 cylinders have 2 very rich, 2 almost at peak, and 2 right at peak EGT... then further leaning will take the 2 at peak beyond peak and down the lean-of-peak side of operations. Yet the 2 almost at peak cylinders have improved their horsepower output as have the 2 very rich cylinders. In other words, of the 6 available cyls, 4 have increased power output as they approached closer to peak EGT, while only 2 have begun the downhill slide on the other side of peak EGT. Therefore the engine may actually exhibit a slight increase in RPM despite the fact that two cylinders are lean of peak (LOP), 2 cyls are at peak, and 2 are rich of peak (ROP).
Also, it's been postulated that an engine running at peak, or even slightly rich of peak, can suffer damage as conditions change and one or more cylinders have cause to lean still further. (A change of density altitude, for example.) In the above example of the 6 cylinders.... any further leaning OR richening, regardless of cause....might place 2 cylinders at risk of excessive EGT. If the power setting of the engine is above 65%, it's possible to damage those cylinders that become leaner...because they are running hotter. Capt. Deakin makes a persuasive case for running lean of peak because further leaning will only result in a cooler EGT. Of course that can only be accomplished in properly instrumented, fuel injected engines. (And it ignores the possibility that an engine might have an equal chance of an inflight change that makes it run richer....and therefore hotter.)
The problem is, with our engines, we're back to measuring things with a micrometer when we use digital EGT gauges. We then mark it with a grease pencil when we are running a variable-length induction engine like this one. (Or when we're "listening" for roughness.) And we're then cutting it with a hatchet with this carburetor and mixture control. (Does it sound as if I have very low regard for digital gauges in these fairly crude engine installations we have?)
I am quite happy with using the tachometer, and my fuel burns average 7.8 gph and speeds run right at 104 kts/120 mph like the factory claims.
What is an EGT gauge going to tell me that I don't already know?
'53 B-model N146YS SN:25713
50th Anniversary of Flight Model. Winner-Best Original 170B, 100th Anniversary of Flight Convention.
An originality nut (mostly) for the right reasons.
50th Anniversary of Flight Model. Winner-Best Original 170B, 100th Anniversary of Flight Convention.
An originality nut (mostly) for the right reasons.

- jrenwick
- Posts: 2045
- Joined: Thu Apr 01, 2004 8:34 pm
Oh, I certainly wouldn't get rid of it. As I said before, it's very nice to have a picture of what's going on with the engine, and I really like the alarms, especially on oil pressure and temperature if you can add those sensors. A six-way EGT is also really nice for debugging problems, like finding a bad spark plug.Haydon wrote:Thank You John and "Blu-elder"I have a lot of respect for my"elders and my betters." From now on I will lean by engine sound. Guess I will have to "duck tape" over the EGT gauge.... I would be inclined to remove it....but, the hole in the exhaust would probably whistle...warning George that I was about to pass him.......
![]()
Richard......
Best Regards,
John
John Renwick
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
Minneapolis, MN
Former owner, '55 C-170B, N4401B
'42 J-3 Cub, N62088
'50 Swift GC-1B, N2431B, Oshkosh 2009 Outstanding Swift Award, 2016 Best Continuously Maintained Swift
- GAHorn
- Posts: 21295
- Joined: Fri Apr 12, 2002 8:45 pm
Yes, you are right, John. My question was a rhetorical one ("What is an EGT gauge going to tell me that I don't already know.") that is not applicable to a multi-cylinder, multi-function gauge.
You are certainly correct, that a good quality, multi-cylinder, multi-function gauge can be very useful in trouble-shooting and in early detection of changes that are occuring in an engine's cylinders.
And my opinion of digital gauges is only that...a personal opinion heavily influenced by personal preference. (I see gee-whiz stuff all day, every day at work and the simple-life is a return to serenity/relaxing pleasure to my personal flying.)
Being an originality nut is also to be taken into consideration by anyone reading my posts. I love original airplanes. (Except, of course, my digital radios, tail-pull handles, tow-adaptors, hatch-latches, 172 door locks, wheels and brakes, strobes.......)
You are certainly correct, that a good quality, multi-cylinder, multi-function gauge can be very useful in trouble-shooting and in early detection of changes that are occuring in an engine's cylinders.
And my opinion of digital gauges is only that...a personal opinion heavily influenced by personal preference. (I see gee-whiz stuff all day, every day at work and the simple-life is a return to serenity/relaxing pleasure to my personal flying.)
Being an originality nut is also to be taken into consideration by anyone reading my posts. I love original airplanes. (Except, of course, my digital radios, tail-pull handles, tow-adaptors, hatch-latches, 172 door locks, wheels and brakes, strobes.......)

'53 B-model N146YS SN:25713
50th Anniversary of Flight Model. Winner-Best Original 170B, 100th Anniversary of Flight Convention.
An originality nut (mostly) for the right reasons.
50th Anniversary of Flight Model. Winner-Best Original 170B, 100th Anniversary of Flight Convention.
An originality nut (mostly) for the right reasons.

- cessna170bdriver
- Posts: 4115
- Joined: Mon Apr 22, 2002 5:13 pm
gahorn wrote:... The problem is, with our engines, we're back to measuring things with a micrometer when we use digital EGT gauges. We then mark it with a grease pencil when we are running a variable-length induction engine like this one. (Or when we're "listening" for roughness.) And we're then cutting it with a hatchet with this carburetor and mixture control. (Does it sound as if I have very low regard for digital gauges in these fairly crude engine installations we have?)...
George is correct in that our engines probably don't need super-accurate digital instrumentation, but then again we probably don't really NEED a gyro panel or GPS, or the airplane itself for that matter; they’re all just toys to make us happy. To each his own. Amen brother on the flying as a means of escape! (In more ways than onegahorn wrote:...(I see gee-whiz stuff all day, every day at work and the simple-life is a return to serenity/relaxing pleasure to my personal flying.)
Being an originality nut is also to be taken into consideration by anyone reading my posts. I love original airplanes. (Except, of course, my digital radios, tail-pull handles, tow-adaptors, hatch-latches, 172 door locks, wheels and brakes, strobes.......)

I put an Electronics International UBG-16 6-cylinder EGT/CHT in my airplane as part of the engine overhaul project last year. (I’m a bit of a gadget geek, so sue me! ) I can’t say that I’m operating any better or more economically, but I do enjoy the insight I get into the operation of the engine. In about 70 hours of operation, I have gotten a pretty good idea of what is “normal†for each cylinder for whatever the situation and conditions happen to be. If someday I have an induction or exhaust leak, or a plug start to foul, hopefully I’ll have some insight on where to start looking for the problem.
Probably the best upgrade, if you can call it that, I did during the overhaul project was to replace the tachometer (my preference is still mechanical analog for this instrument, go figure

George and I have discussed this here before, but IMHO, the hatchet analogy is right up there with the "fire hydrant valve on a water fountain" analogy, i.e. it’s just an exaggeration to make a point. With my vernier mixture control and the digital instrumentation, I can set EGT for any one cylinder within 5 degrees of where I want it, and once set, it rarely varies by more than a degree or two. That doesn’t necessarily accomplish anything especially useful, as there are other cylinders that are 150 degrees different, and there’s nothing that can be done for one that doesn’t affect all in one way or another; I just think it’s interesting. So there.
Miles
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