As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FS 280 STRAP CORRODED AT S27. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT, IS .079" ORIGINAL IS .080, MATERIAL REMOVED IS .001. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00-101-001-A01.