As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) UPON VISUAL INSPECTION LT NR 1 PROPELLER BLADE FOUND A CRACK RUNNING PERPENDICULAR ALONG THE NICKEL SHEATH THAT HAS STARTED TO RUN VERITCAL AND INTO THE COMPOSITE OF THE BLADE ITSELF. PROPELLER BLADE WAS COMING DUE FOR O/H AND REMOVED EARLY DUE TO CRACK. PROPELLER BLADE REPLACED AND ACFT RETURNED TO SERVICE.