As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME 1088.20 AFT SIDE CORRODED BTW STGR 25L-26R. REMOVED CORROSION FROM 1088.20 AFT SIDE IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSP IAW BSC NDT INSP PROCEDURE 4.3. MIN REMAINING MATERIAL IS 060". NO DAMAGE ALLOWED ON FRAME. COMPLIED WITH EC/TC EA 32-2017-043 PERFORMED PERMANENT REPAIR IAW EA 32-2017-043.