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Old November 14th, 2007, 17:25   #1
aviatorrbt
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Default CHT and melting.

Hey everyone. I was flying with an older gentleman today that said if the CHT gets above 400 degrees in a small plane (we were flying a Cirrus) that the cylinder heads would melt... anyone know if this is true or remotely true? Thanks
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Old November 14th, 2007, 17:28   #2
Berkut
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Default Re: CHT and melting.

400 degrees isn't even close.
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Old November 14th, 2007, 17:34   #3
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Default Re: CHT and melting.

According to the type certificate data sheet for the IO-360-ES, the max CHT as measured by a bayonet-type thermocouple is 460 degrees. What does the operating handbook say?
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Old November 14th, 2007, 22:12   #4
USMCmech
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Default Re: CHT and melting.

Quote:
Originally Posted by aviatorrbt View Post
Hey everyone. I was flying with an older gentleman today that said if the CHT gets above 400 degrees in a small plane (we were flying a Cirrus) that the cylinder heads would melt... anyone know if this is true or remotely true? Thanks

Not even remotely true.


However, keeping CHTs bellow 400 is a good idea and will lead to the longest life for the engine.

Most engines have a max CHT of about 450, but this should be regarded as a momentary "yellow arc" for short durration only. Cruising around at 450 CHT all day every day will lead to problems.
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Old November 17th, 2007, 08:42   #5
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Default Re: CHT and melting.

Most of the aircraft that I have flown have a caution range that starts at 450F.
500 on the CHT would change the crystalline structure of the metal alloy the cylinder head is made of. It will therefore permanently change it's properties, one of them being strength.
After that it is a matter of time.
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