What was found
DURING AN INSPECTION OF THE MAIN ROTOR BLADES, FOUND A CRACK IN THE T/E OF THE BLADE WHERE THE NON BENDABLE TRIM TAB RIVETS TO THE BLADE. SENDING BLADE FOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING AN INSPECTION OF THE MAIN ROTOR BLADES, FOUND A CRACK IN THE T/E OF THE BLADE WHERE THE NON BENDABLE TRIM TAB RIVETS TO THE BLADE. SENDING BLADE FOR REPAIR.