As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AIRCRAFT WAS IN FOR A 100HR INSPECTION. ON INSPECTION AS PER MANUAL FOUND A SMALL AMOUNT OF DEBONDING ON THE LEADING EDGE. NO IMPACT MARKS WHERE FOUND ON EITHER BLADE. MANUFACTURER REPORT FOUND THE BLADES SCRAP DUE TO DIMENSIONAL DIMENSIONS ON ONE BLADE BEYOND LIMITS. ONE BLADE HAS MOVED ON ITS SPAR.