As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A ROUTINE 100 HR INSPECTION AME WAS PERFORMING MAIN ROTOR BLADE INSPECTION AND NOTED A HAIR LINE CRACK WERE TRIM TAB IS BONDED TO BLADE. AFTER CONSULTING TEC SUPPORT THEY SAID THE BLADE IS NOT REPAIRABLE AND IS SCRAP. DATE OF INSTALL OF THE BLADE AT 0.0 WAS JULY 20/2004, BLADE HAS 12 YEAR LIFE.