>> soon as throttle pushed in, cyl's 5 and 6 climb at about 1 degree per second - power always retarded not to exceed 390 and cool down in the 350-360 range before trying to push up power again.<<
Bob,
When I read that statement - - I stopped what I was doing (preparing a presentation for the ASTM in connection with the approval of the G100UL™ avgas ) - -
In order to follow up.
THIS IS IMPORTANT: There are VERY FEW THINGS IN AN AIRCRAFT PISTON ENGINE THAT CAN CAUSE AN OPERATING CYLINDER CHT TO SUDDENLY BEGIN TO INCREASE AT A RATE OF 1 DEGREE / SECOND ( 360 TO 390 IN 30 SECONDS, FOR EXAMPLE ) - - - except:
1) Outright pre-ignition; or,
2) Simulated outright-pre-ignition due to improperly advanced timing.
MERE DETONATION - - EVEN MEDIUM TO HEAVY DETONATION - - will not do that.
Amazingly, if you have caught and limited the CHT rise and managed that at levels under about 420 dF, as you appear to have done - - then you have likely NOT done any harm to the cylinders. But a borescope is in order. And change the spark plugs in those two cylinders. The plugs can be damaged from those kinds of combustion events.
I have a lot of old and a lot of more recent data that documents all of the statements made, above.
If you will forward to me the engine data downloads from those flights I will try to take a look at them and I can tell you what was going on.
Call me if you want to. I might have some suggestions for you to allow you to proceed to get your aircraft flying again comfortably. However - - getting me the engine download data is the most important thing you can do.
Regards, George