hindsight2020
Final Approach
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- Apr 3, 2010
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hindsight2020
The power of conversation. I was able to clarify the mechanic's position today. It appears a case of a simple misunderstanding of "required vs desired".
Where we got off the rail a bit initially was in the hesitancy to pull the cylinder, which puzzled me without context. After further consultation it does appear there's nothing to gain regarding the items of interest I was actually concerned about (any rotating internals being bent/broken tweaked). Compression checked, continuity on all moving pieces checked, and TDC verification was accomplished, the engine appears straight.
The hydrolock theory was talked about briefly and quickly ruled out based on the aforementioned evidence and what he observed when he pulled the plugs. There was no river of fluid when he pulled them, nor was the top plug oil fouled.
So now we wait for the engine shop quotes before proceeding. Based on my educated presumption of big item integrity, I'm going the IRAN route, and try to keep the airplane flying. Replacement of all studs and thrus, NDI/recertification (and repair if needed) of the case, inspection of the affected cylinder and repair as necessary, freshening up of the internal bottom end wear items, and bolt it back together. I'll try to keep the thread updated.
Where we got off the rail a bit initially was in the hesitancy to pull the cylinder, which puzzled me without context. After further consultation it does appear there's nothing to gain regarding the items of interest I was actually concerned about (any rotating internals being bent/broken tweaked). Compression checked, continuity on all moving pieces checked, and TDC verification was accomplished, the engine appears straight.
The hydrolock theory was talked about briefly and quickly ruled out based on the aforementioned evidence and what he observed when he pulled the plugs. There was no river of fluid when he pulled them, nor was the top plug oil fouled.
So now we wait for the engine shop quotes before proceeding. Based on my educated presumption of big item integrity, I'm going the IRAN route, and try to keep the airplane flying. Replacement of all studs and thrus, NDI/recertification (and repair if needed) of the case, inspection of the affected cylinder and repair as necessary, freshening up of the internal bottom end wear items, and bolt it back together. I'll try to keep the thread updated.
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