Anybody know why cylinder #2 seems to be the most problematic on the Rockets? I've just test flown a Rocket where cylinder #2 overheated (above 460) on a climb to 14k. Looking at logs from others, it seems cylinder work always includes #2.
According to a mechanic working on the test flown plane, the cylinder is located on the pilots side closest to the firewall, but in front of the oil cooler. It does look like it would be the most challenging to cool. Baffling looked OK and sealing looked OK to the cowling.
According to the logs, the owner had pulled and honed the #2 cylinder about 25 hrs earlier, and owner was saying it may just need more break in. I'm not sure that really sounds right. Shouldn't it have settled down in 25 hours?
Now, looking at another plane, cylinder #2 has been replaced due to low compression while all the others have passable compressions (66, 68 and in the 70's). Will this engine (800 hrs TSREMAN) be OK if treated well (CHT below 380)?.