Jump to content

Recommended Posts

Posted

If they have been run on a test stand, very little...

See if you can get the break-in instructions from your engine rebuilder...

They usually state how many flights should be done early on... what the purpose is... and what to look for...

 

Then there is the usual statement that says break in will occur over time that may last 100 hours...

If you have an engine monitor... you will be watching CHTs that stay elevated until the rings work in...

 

My factory reman IO550 was run on a test stand for a couple of hours... when installed it had two flights circling the airport... a couple more hours...

Then the Long, low, high MP, sweeping rpm flights began...

All in... probably 10hours of break-in related flying... never saw a shift in CHTs...

I was hoping to see an obvious sign that everything was done correctly...

Follow the steps, claim success!  :)

Best regards,

-a-

Posted

My  experience with the factory reman was much the same as Anthony‘s, above. Didn’t see much indication of change on engine monitoring. Lycoming runs their remans on a test stand, so I would imagine that the break in  process was well underway way by the time the engine was installed on my plane. The proof is in the pudding though, because I have excellent oil consumption and compressions have stayed at 78/80 or better for the almost 600 hour since it was installed.

  • Like 1
  • Thanks 1
Posted

I followed the Lycoming instruction for running in except for oil changes, which I did at +4 and +13 hours before going to the regular 25 hour intervals. There wasn't a magic number when it was suddenly "broken in",  just as I got more hours on the engine I would be a little less conservative on limits and expectations. By 40 hours I was back to using the limits I used on the old engine. (which are pretty much book, except for CHT and TIT where my limits are lower))

However, what are you expecting with "broken in" - at 1000 hours some parts/fits will still be getting sweeter and some other parts will be wearing out!

  • Like 2
Posted (edited)

And don’t use Camguard during the break in process. I didn’t resume using it until about the 50 hour mark just to be on the safe side. Also for Lycoming turbo engines use ashless dispersant oil vs mineral oil for break in as per the Lycoming directive.

Edited by Bravoman
  • Thanks 1

Join the conversation

You can post now and register later. If you have an account, sign in now to post with your account.

Guest
Reply to this topic...

×   Pasted as rich text.   Paste as plain text instead

  Only 75 emoji are allowed.

×   Your link has been automatically embedded.   Display as a link instead

×   Your previous content has been restored.   Clear editor

×   You cannot paste images directly. Upload or insert images from URL.

×
×
  • Create New...

Important Information

We have placed cookies on your device to help make this website better. You can adjust your cookie settings, otherwise we'll assume you're okay to continue.