As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A DISASSEMBLY INSPECTION OF PROPELLER LINK, THE BLADE ACTUATING ON THE NR 2 BLADE WAS BROKEN AT THE .4375 INCH BLADE BUTT ATTACH POINT AND THE CHROME PLATING ON THE BLADE PITCH FITTING WAS DETERIORATED AND SHOWED EXTENSIVE PITTING. SUSPECT POSSIBLE FAILURE TO REPLACE OR REWORK COMPONENTS DURING OVERHAUL. PHOTOS AVAILABLE UPON REQUEST.