I have a 1966 7GCAA with a O-320-A2B. The engine was overhauled by MAttituck and we have about 30 hours SMOH. We also installed a JPI-700 after the overhaul. Since the JPI is new in the aircraft, I don't have any numbers to compare what the engine was doing before the overhaul.
At full power approximately 2650-2700 RPM level flight at about 3000ft MSL, I see 350-360 degrees F on #1, and #2, and 420-430 on #3, and #4.
At about 70% power, the temps drop to 340-350F on #1, and #2, and 390-400F on #3, and #4.
At about 60% power, the temps drop to 330-340F on #1, and #2, and 380 to 385 on #3, and #4.
I am curious if anyone else has a JPI with the O-320 that can compare CHT numbers.
We replaced all of the baffle seal material, with red silicone rubber and have sealed up all of the holes that we can find.
Is this just the nature of the beast due to poor cowl airflow design and/or poor fuel/air distribution of the O-320?
We are still running mineral oil, and the mixture was full rich for all measurements.
At full power approximately 2650-2700 RPM level flight at about 3000ft MSL, I see 350-360 degrees F on #1, and #2, and 420-430 on #3, and #4.
At about 70% power, the temps drop to 340-350F on #1, and #2, and 390-400F on #3, and #4.
At about 60% power, the temps drop to 330-340F on #1, and #2, and 380 to 385 on #3, and #4.
I am curious if anyone else has a JPI with the O-320 that can compare CHT numbers.
We replaced all of the baffle seal material, with red silicone rubber and have sealed up all of the holes that we can find.
Is this just the nature of the beast due to poor cowl airflow design and/or poor fuel/air distribution of the O-320?
We are still running mineral oil, and the mixture was full rich for all measurements.