SUMMARY: The FAA is adopting a new airworthiness directive (AD) that supersedes an existing
AD, for Lycoming Engines (formerly Textron Lycoming), direct-drive reciprocating engines (except
O-145, O-320H, O-360E, LO-360E, LTO-360E, O-435, and TIO-541 series engines). That AD
currently requires inspection of the crankshaft gear installation and rework or replacement of the
gears where necessary after a propeller strike, sudden stoppage, at overhaul, or whenever gear train
repair is required. This AD requires the same actions but makes the correction that the existing gear
retaining bolt and lockplate be removed from service and new hardware installed, and revises the
definitions for sudden stoppage and propeller strike. This AD results from a change to the definition
of a propeller strike or sudden stoppage. We are issuing this AD to prevent loosening or failure of the
crankshaft gear retaining bolt, which may cause sudden engine failure.
To summarize from what I can tell this ad calls for only inspection of camshaft gears and replacment of retaining bolts on the back of the engine. This is also what the mechanic who signed it back into service interprets the ad to read. They dailed the crank and it was very straight and it was flown 2 hours post . I got a new prop to put on the plane and am going to have it ferried here this week (it's in annual and seems very airworthy)
So my question is can i trust this engine ? From myresearch most seem to point to overhaul. However if there was dangers wouldn't the ad require further inspection of the crank or am i completely mislead. Engine has 1400 smoh.
I know i haven't said what my new plane is.....and it's a mooney (don't laught) thought it would compliment a stinson nicely. I figure if anyone else is going to tell me to slap a prop on it and fly the s*** out of it till tbo they might reside here.
Mike


, feels bad to have to buy a new crank !!