What was found
NR 1 ENG FAN BLADES NR 24, 19, 10, 9, 5, AND 4 HAS CU-NI-IN DAMAGE OUT OF LIMITS. AND THE NR 1 BLADE ROOT DAMAGED FROM SHIM CONTACT OUT OF LIMITS. ACFT GROUNDED. REPLACED THE BLADE PAIRS IAW TC 78472002 ON THE NR 1 ENGINE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENG FAN BLADES NR 24, 19, 10, 9, 5, AND 4 HAS CU-NI-IN DAMAGE OUT OF LIMITS. AND THE NR 1 BLADE ROOT DAMAGED FROM SHIM CONTACT OUT OF LIMITS. ACFT GROUNDED. REPLACED THE BLADE PAIRS IAW TC 78472002 ON THE NR 1 ENGINE.