As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FS 275 FRAME CORRODED AT S29R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. RESTORED SURFACE FINISH IAW SRM 51-25-06-001-001-A01, 51-25-16-001-001-A01, AND 51-42-06-001-001-A01.