As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CHAFING ON PREVIOUS REPAIR DOUBLER, TRIPLER AND TAPER SHIMS IN FS=968 TO FS=985 AT FUSELAGE SKIN.(FUS)(SM)(TCI 53-20-252). REPAIR DOUBLER, TRIPLER AND TAPER SHIMS IN FS=968 TO FS=985 AT FUSELAGE SKIN WERE REPLACED PER REO 670-53-00-290 REV. E AND SRM 51-25-01-001-001-A01.