As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PIT 1460 FRAME, NUMEROUS AREAS ON FRAME CORRODED, TOTAL OF NINE AREAS. REMOVED CORROSION IAW SRM SRM 53-00-07 FIG 101 ORIGINAL THICKNESS .067" AFTER CORROSION REMOVED .055" FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL V. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. MAJOR REPAIR.