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Home » Topics » Main Forum » PIPER MODELS » PA-28 » High oil temps

High oil temps

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Posted In: PA-28

  • Participant
    wesley ballou on May 5, 2025 at 10:44 pm #23093

    Steve & Charlie

    I have had some success with the ongoing high oil temp issue. We increased the oil pressure. Just put a washer in the oil pump. The oil runs on the high side but is still within limits. This seems to circulate the oil so it gets through the cooler a little faster. I still have trouble in the climb with the oil temp getting to the red line. When I get to altitude it seems to settle into the high normal range. This is when outside air temperatures are in the low to mid 80’s. My concern is that when it gets to be summertime here in Texas and temperatures get in the mid 90’s and above, I will not be able keep it within limits until to altitude. I have had thoughts of putting a higher capacity oil cooler in. Additionally, I was looking into moving the oil cooler to a location that it would get better airflow like some of the newer model PA-28’s. I was also looking into the possibility of increasing the vents on the bottom of the cowling or possibly installing a cowl flap to increase airflow until I can get to altitude and power back to cruse power. Any thoughts on any of these suggestions?

    Thanks for taking the time to read this and any feedback you could provide would be appreciated.

    Thanks, Wesley

    Participant
    STEVE on August 5, 2024 at 10:31 am #22675

    Hi Wesley, and Charlie;

    I have attached a file that contains troubleshooting steps for high oil temperatures.
    It’s pretty self explanatory.
    One of the easier checks is removing the vernatherm (thermostatic bypass valve) and measuring the length–see page 4 of the attachment. Then submerge it in light oil that’s heated to 150 deg F. Measure it again. It should be at least 0.160 longer; if it isn’t you’ll need to get a new one. 
    A vernatherm that doesn’t extend won’t force oil through the oil cooler.

    Another check of the thermal control system is to look at the sealing surface of the vernatherm, and the sealing surface inside the engine case to see if; 1) check for wear on the vernatherm surface and on the vernatherm contact surface on the engine case.

    Lycoming Service Instructions 1316A is attached–it provides information on oil cooler causes, and solutions.

    Let me know what you find

    Steve

     

    Attachments:
    • LYCHiOitTemps.pdf
    • SI1316ACoolerByPassSeatRepair.pdf
    Participant
    CHARLIE MUELLER on August 4, 2024 at 10:28 am #22672

    Steve-

    Not sure if you were wanting me to respond or Wesley who posted more recently on high oil temps. The short answer is my peak oil temp occurs at top of climb.

    I recently flew my Dakota from Naples, Florida to Aurora, Illinois in July. It was a hot day with surface temps in the 90s.

    My first leg the oil temp peaked at 236 and settled down to 208, but most of the flight was 215

    The second leg Montgomery Alabama to Owensboro KY (the hottest part of the day the oil peaked at 242 and settled to a low of 208 with most of the time in cruise at 218.

    The last. leg was Owensboro, KY to Aurora, Illinois and the oil peaked at 227 and dropped to 210 and it was 210 for most of the time in cruise.

    I have a half dozen other flights that I need to download engine data for but I think the temps were more like the last flight-peaks around 227.

    Participant
    STEVE on August 3, 2024 at 12:00 pm #22670

    Hi Charlie;
    As I read this, it seems to say that you were getting high oil temperatures when you’re running the engine on the ground.

    That prompts me to ask; “Are you also getting high oil temperatures in flight?”

    Pls let me know.

    Thanks 
    Steve

    Participant
    wesley ballou on July 29, 2024 at 9:33 pm #22668

    I have a 1967 Chrokee 235B.  It flew fine for the past year.  Now I am experiencing high oil temperatures. Oil and filter have been changed withing the last 2 hours.  Oil pressure is fine.  Within 15 – 20 minutes of start up the oil temp is very near the red line.  Engine runs were done on the ramp with outside temperatures of 80 degrees F.  We have checked the baffles, changed the oil temp gage, the oil temp sensor, and the oil cooler.  None of these remedies seems to have an effect on lowering the oil temp.  Has anyone had a similar experience or have any suggestions on how to remedy the situation?

    Participant
    CHARLIE MUELLER on September 22, 2022 at 9:22 am #21572

    Steve-

    I will try increasing the oil pressure as you suggest and also begin using lean to peak EGT after reviewing my pilot guide . The engine runs the same after the new cylinder. I’ll also review cowl exhaust fairing and report back in October.

    Thanks again-

    Charlie

    Participant
    STEVE on September 18, 2022 at 12:53 pm #21566

    Hi Charlie;
    The adjustment to increase the cruise oil pressure is above and behind the upper surface on the copilots side of the engine. The old kind (like I have) does not have an adjustment screw and washer on the outside of the large nut/cover.
    If yours has the screw/jam nut on the outside of the large nut/cover, then all that’s required it to loosen the jam nut and turn the screw in. I would start with a half turn, then test.
    If your large nut/cover does not have a jam nut and screw projecting out of the top, the procedure to increase the OP is to remove the assembly, which consists of the large nut/cap, a spring and a steel ball. All it takes to increase the pressure is to put a simple aircraft quality washer between the outer end of the spring and the large nut/cap.

    The JPI 830 Pilots Handbook (https://www.jpinstruments.com/wp-content/uploads/2012/07/PG-EDM-730_830_851_740-Rev-F-TB2.pdf) has information on how to use the “lean find” feature in your monitor. I believe there is a horsepower read out on the 830. Any time you’re below 75 % power you can lean to peak. The Lean Find feature should identify the first one to peak. Check out that Pilots Handbook for the details.

    As far as modifying the lower cowl, you shouldn’t closed down the exit holes for the exhaust stacks because the engine does move compared to the cowling during operation. The pipes need room to move in the opening.

    If you were good with fiberglass, you could make a fairing that would redirect the air that might come in the holes for the exhaust. But even if you made one, you’d have to legally install it.
    I’ve seen those type of exhaust pipe fairings for Cessna Cardinals and Cessna 182s, but can’t recall seeing one for a Piper. You can take a look here: https://aircraftspeedmods.ca/products/exhaust-fairing-stc-sta-2/. Maybe the company can give you some guidance on its fairings.

    I don’t think you’re in too much trouble with your CHTs. That said, please inspect to see that the inner cylinder baffles (the metal parts that fill the gaps between cylinder barrels and heads) are installed correctly.

    Does the engine feel any different than it did before you installed the new cylinder??

    Let me know if you find anything else.

    Steve
    Let me

    Participant
    CHARLIE MUELLER on September 16, 2022 at 9:57 am #21563

    Steve here are a few more pieces of information

    I never fly above 70% power except on takeoff. I sometimes fly 55-60 but usually 65% and occasionally 70% so I’m not sure what Savvy report you refer to but I’ll take a closer look.

    How do I increase OP in cruise- is there a setting on the oil pump?

    Yes my CG flights are in Florida and it seems that the high OATS are a big contributing factor to the high temps that I’m experiencing also occasional CHTS 400-420 and once in awhile 433 in initial climb but they always cool down in cruise.

    My leaning has been all over the map as I’ve read more, talked with Lycoming service reps-I’ve gotten myself all mixed up. Lean to 12 gph, lean to 160 ROP, Lean to engine roughness then enrich to smooth power.

    I do have an EDM 830 and it has both ROP and LOP Modes.

    I would be comfortable leaning to peak EGT as long as I can easily determine the 1st cylinder to peak.

    See attached oil analysis

    One other suggestion that’s been given to me and that is to modify the lower cowl to reduce the size of the opening around the exhaust riser to prevent ram air from coming into the lower compartment and diminishing the negative pressure in the lower cowl engine compartment.

    Thank you for all of your suggestions and input.

    Charlie

    Attachments:
    • N8382Z-220616.pdf
    • 7FDEF12B-C256-4634-9392-AE1AC630FC6E.jpeg
    • B02D632B-BB13-440F-B5ED-14426DE00FAF.jpeg
    Participant
    STEVE on September 12, 2022 at 11:10 am #21547

    Hi Charlie;
    Thanks for all the data you’ve sent; very helpful.
    One of your cylinders has a chrome lining. That’s shown by all the “worm tracks” in the photo. I can’t really tell what the other cylinder photo signifies.
    As you may know the compression rings in a chrome cylinder wall don’t always seal the combustion gas pressures as well as the rings in a steel cylinder wall. I’m suggesting that another factor for the high oil temps is the increased amount of hot combustion gasses leaking past the rings in the glazed cylinder and the chrome cylinder.
    And if I’m reading the Savvy report correctly, it appears as though you’re power settings in cruise are above the high side of normal. I’m gratified to see that your oil temps hover right around 200 when you fly at 65% power settings.
    Your idle OP is very good. You could try increasing your cruise OP; that would push more oil through your cooler. My OP reads 77 psi in cruise.
    Your oil consumption numbers are good, esp considering the chrome cyl and the glazed cyl. I have 4 chrome cyl on the Lyc 180 in my Comanche and I get about 4.5 hours per quart.
    If I understand you correctly, you fly US CG Aux flights at 1000′. I’m guessing these flights are in Florida; am I correct? When you say the temps are trending higher, could that rise coincide with the increase in OATs as summer comes on??
    Are you also flying the US CG flights at 65% power and leaned to best power.
    FWIW, Best power leaning, which is around 80 deg R of peak is a pretty hot spot in the leaning curve. You should be able to lessen the CHTs by leaning more. Lycoming publications allow leaning to peak EGT below 75 % power.
    Is there an engine monitor in your airplane? Does it have a “lean find” feature? Would you be comfortable leaning your engine to peak EGT. If you are going to try this, the key is to lean to peak on the first cylinder to achieve peak EGT; not the hottest cylinder.
    Have you sent in oil samples for oil analyses? If so, did the reports reveal any anomalies?
    Thanks for the information. Please get back to me with your replies.
    I’ve attached a chart showing how leaning affects EGT, CHT, HP and Internal Combustion Pressures, As you can see every value goes down when you lean to peak vs. 80 deg rich of peak.
    Best,
    Steve enginemgmtchart.jpg enginemgmtchart.jpg

    Attachments:
    • enginemgmtchart.jpg
    Participant
    CHARLIE MUELLER on September 12, 2022 at 9:22 am #21544

    Steve-

    My cruise oil temps have always been elevated but seem to be slowly trending higher (see attached trend report)but they could be in part to my increasing USCG Aux flying 1,000′ . It does appear that OAT makes a difference. I am based in Florida in the fall through June and Michigan over the summer. I just flew a trip to upper MI, and was able to get my cruise oil temp 198-204 due to 65% power, 100 degrees ROP and lower OAT.

    Oil pressure at idle appears to be 55psi +/-

    Cylinders #1 and 3 are glazed as determined by borescope(see photos).

    I run 8-10 quarts and try to keep it at 9. I burn a quart every 7-8 hours.
    The engine does not stutter at all upon start up. It does occasionally stumble when I have reduced power in the pattern and then need to come back in with. power but after a very brief hesitation it responds.

    I have attached reports of my engine data as well as photos of the #1 and #3 cylinders.

    Charlie

    Attachments:
    • ReportCardN8382Z32022.pdf
    • TrendAnalysisReportN8382Z22022.pdf
    • N8382Z1glazedwall.jpg
    • N8382Z3glazedwall.jpg
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