This is wrong.
Engine should ABSOLUTELY be broken in at high power and low altitude. The best possible place to break in an engine is at sea level where manifold pressure is at its highest. An engine that is broken in at high altitude like you claim to be doing will not seat the rings.
Proper break in is accomplished at various power settings(IAW Lycoming/Continental SB's), up to and including significant time at 100% power. Please explain how you are doing this at an altitude that is limiting your power to approximately 50%, and also how you feel comfortable certifying that you have installed and broken in the engine with your procedure
The reason why the pic was taken was to show the owner and( ultimately ) have a post flight discussion about the inlet as compared to exit area of the cowls and possible opening up the lower cowl for extra cooling. I suspect the inlet / exits were sized more for a 0-360
I used to alternate between 75% and full power for break-ins, Many O/H shops now lean towards 75% only, Who is right?
After that pic was taken, a slow descent back to about 4000 was done. The temps returned to the green. If on the next flights they dont go over 400 degrees Im ok with that, but i would hate to cut the lower cowls only to find after break-in that it was not needed ! Lycoming suggests 400 degrees max, continuous 425 in the climb, but 375 seems the industry norm, 500 is redline and anything above 400 will show less than optimum wear/tear over time.
You are right and I am wrong WRT the high altitude and only 50% ish power. We were over Baldy within gliding distance and out of the valley because of noise concerns but in the end it would have been better to bother the residents than to delay break-in