What was found
(AUS) MAIN ROTOR BLADE PENDULUM VIBRATION ABSORBER ASSEMBLIES (4OFF) LOWER PLATE BRACKETS CRACKED IN AREA OF INBOARD FLANGE DUE TOEXFOLIATION CORROSION
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) MAIN ROTOR BLADE PENDULUM VIBRATION ABSORBER ASSEMBLIES (4OFF) LOWER PLATE BRACKETS CRACKED IN AREA OF INBOARD FLANGE DUE TOEXFOLIATION CORROSION