I stupidly landed my Twin Comanche I-NASA on its belly last November: virtually no damage to the plane, but the props were scrapped and the engines were opened up and inspected for shock loading. The work was done by a highly reputed Italian workshop, whose owner and boss is a recognised authority on Lycoming engines. Both engines were fully disassembled and thoroughly cleaned before reassembly and bench testing (including the fuel injection system)
During the first test flight, the RH engine momentarily lost power in the climb-out, and remained pegged at 2500 rpm for about 40 seconds, and then recovered. It was inspected and the fuel injection system was found to be too rich and recalibrated. After about 5 flying hours, I took off in a very hot day, and it happened again: but I had forgotten to switch on the electric pumps, so I attributed it to a vapour lock. It happened again in Poland, and my copilot quickly leaned the engine, which immediately recovered. So I decided to have the system inspected at the first oil change (50 hours), and flew with great caution, running the engines at FT for 30 seconds before releasing the brakes.
Then it happened again, and this time the engine never recovered. I took off from Reggio Emilia, and the RH engine ran down to 2500 rpm. I leaned it, switched the electric pump on and off, tried everything, but it went on vibrating until landing in Milan after 45 minutes. Curiously, the CHT dropped to about 250°F and EGT remained fairly low irrespective of the leaning. I flew back at 23.5" MP and 2300 rpm, at 130 KIAS instead of the normal 140-142. MP was normal, and therefore there should be no influence of the alternate air door.
So I stopped flying and asked the engine guys in. They did a very careful test and recalibrated again the fuel injection system, which was again too rich. Now the engines tick over at idle at 700 rpm without problems. All the parameters were OK, so we went for a test flight. And sure enough, during engine runup it did it again.
The engine guys suspected a sticking valve, and performed an SB388 inspection: as I was sure, everything was OK. So they tried again to reproduce the phenomenon, and at the end they concluded that it is a vapour lock due to excessive engine temperatures on the ground (as indeed it was, after such prolonged tests). They claim that everything is OK and that this should not happen again if I avoid to run the engine too long at high setting on the ground (as I was doing for prudence with my 30 seconds FT runup before brake release).
I don't feel too happy about this response, and certainly for a while I will avoid short fields. But has anybody any comment to offer?
Thank you all in advance and best regards