I have a Lycoming AEIO-320-E2B installed in a 1976 7KCAB Citabria. The engine has 300hrs since major overhaul which included new camshaft and lifters. The case halves, crankshaft and connecting rods were inspected and yellow tagged by ECI. Penn Yan (.10 over) cylinders with new pistons, rings etc. (Total time on the engine at time of O/H was 1595hrs) This maintenance accomplished 4 years ago by a now defunct shop in NY.
The engine has run very smoothly with no problems for the last 2 years during my ownership, and has only been used for light aerobatics and has mostly been flown locally but has been used for a few 3-5 hour cross country flights during the last year.
Recently the engine was difficult to start, which is unusual, and when started ran extremely roughly. It was immediately shut down. On inspection the propeller turned easily( almost too easily). After removing the top plug from each cylinder, the #4 cylinder could not generate any compression. There was no air escaping the exhaust system. The left side valve covers were removed and the intake valve on the #4 cylinder was found to be stuck open with no movement of the pushrod on turning the prop by hand. The other pushrods worked appropriately.
The pushrods on the #4 cylinder were removed which allowed the intake valve to ‘snap' shut. The hydraulic lifters were removed and resisted compression in a normal fashion. The tappet ‘lifter body' on the exhaust side moved freely within the crankcase but the intake tappet was stuck and could not be moved even with moderate tapping with a brass drift. I have not received oil sample results yet.
I think I understand the implications of the above findings and that I am going to have to get the case split to get the final diagnosis, but does anyone have any insight as to what I should expect to find. Am I looking at another overhaul or even new engine? There will be no warranty consideration.
Best regards
Crispin
The engine has run very smoothly with no problems for the last 2 years during my ownership, and has only been used for light aerobatics and has mostly been flown locally but has been used for a few 3-5 hour cross country flights during the last year.
Recently the engine was difficult to start, which is unusual, and when started ran extremely roughly. It was immediately shut down. On inspection the propeller turned easily( almost too easily). After removing the top plug from each cylinder, the #4 cylinder could not generate any compression. There was no air escaping the exhaust system. The left side valve covers were removed and the intake valve on the #4 cylinder was found to be stuck open with no movement of the pushrod on turning the prop by hand. The other pushrods worked appropriately.
The pushrods on the #4 cylinder were removed which allowed the intake valve to ‘snap' shut. The hydraulic lifters were removed and resisted compression in a normal fashion. The tappet ‘lifter body' on the exhaust side moved freely within the crankcase but the intake tappet was stuck and could not be moved even with moderate tapping with a brass drift. I have not received oil sample results yet.
I think I understand the implications of the above findings and that I am going to have to get the case split to get the final diagnosis, but does anyone have any insight as to what I should expect to find. Am I looking at another overhaul or even new engine? There will be no warranty consideration.
Best regards
Crispin