As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME CORRODED AT FS 310 AND ON BOTH SIDES OF STR 27. CORROSION REMOVED IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .047. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. RESTORED SURFACE FINISH IAW SRM 51-42-06-001-001-A01, 51-25-06-001-001-A01, AND 51-25-16-001-001-A01.