Sometimes it helps to look at the assumptions behind different sides in a debate. The primary assumption here seems to be that leaning a plane correctly prior to takeoff at altitude will increase safety by improving engine performance.
Here's a link to a graph from the the Lycoming O-360 operations manual. By increasing from peak EGT, the percent power at any given altitude varies from 96% power at peak EGT up to 100% at the sweet spot and then down again to 95% at full rich. The sweet spot is about 13 degrees C (55 degrees F) below peak. Assuming the pilot is
not going to do a formal, slow max power runup using an engine monitor and full power (sucking rocks into the prop and throwing them at the horizontal stabilizer all the while,) his finger width approach is probably going to get an approximate level somewhere between 96% and 100%. Let's say an average of 98% power, or 2% less than perfect. Is a couple of percent enough to warrant taking the risk of a leaning error and an engine stumbling halfway down the runway? Food for thought.
Anyway, if a 2% power improvement would make a safety difference, maybe you need to wait and take off in the morning. Your margins are too thin.
The engine power available for a go-around is far more important that the engine power taking off from the end of a runway. I'm just not going to assume that the mixture settings I did with my engine monitor 30 minutes before at a different altitude will apply to the landing conditions. Especially then, I would rather trust the security of full rich than an arbitrary guess about the right mixture settings.

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