What was found
RED MAIN ROTOR BLADE CRACKED AT UPPER SURFACE BETWEEN BLADE FITTING AND BLADE CUFF. VERIFIED CRACKED AFTER SANDING IAW AMM 62-10-00, 6-1. REMOVED AND REPLACED MAIN ROTOR BLADE IAW AMM 62-10-00, 4-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RED MAIN ROTOR BLADE CRACKED AT UPPER SURFACE BETWEEN BLADE FITTING AND BLADE CUFF. VERIFIED CRACKED AFTER SANDING IAW AMM 62-10-00, 6-1. REMOVED AND REPLACED MAIN ROTOR BLADE IAW AMM 62-10-00, 4-1.