As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CIRCUMFERENTIAL FRAME REINFORCING ANGLE CORRODED AT STA 380 BETWEEN STRINGERS 27R AND 28R. CUT OUT DAMAGED AREA PER SRM 53-10-1. HFEC INSPECTED CUTOUT PER NDT M/M 51-00-00. NO CRACKS IND. INSTALLED ANGLE REPAIR PER SRM 51-40-04. TREATED AND PRIMED PER SRM 51-10-2.