As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PILOT'S BULKHEAD AFT SIDE JUST ABOVE WL 72.50 WEB CORRODED AT FS 280.00. BLENDED CORROSION IAW SRM 53-11-10-201-003-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW NDT INSPECTION PROCEDURE UT-3. MININUM MATERIAL REMAINING IS .038". ORIGINAL MATERIAL THICKNESS IS .040" MATERIAL REMOVED IS .002", WITHIN LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-598.