As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN ROTOR BLADE HAS CRACK IN LEADING EDGE AND FIBERGLASS. INSPECTED, PERFORMED 2500 HOUR INSPECTION, REPAIRED SKIN AT STA 131 TO STA 153 AND STA148 TO STA 152 ON LOWER SURFACE REPLACED OUTBOARD ABRASION STRIP. REPLACED INBOARD AND OUTBOARD SPLICE COVERS REPLACED POLY ROOT TAPE APPLIED HIGH VIS PER CUSTOMER REQUIREMENT; STATIC BALANCED.