As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CIRCUMFERENTIAL FRAME FWD WEB CORRODED AT STA 380 BETWEEN STRINGERS 27R AND 28R. CUT OUT DAMAGED AREA PER SRM 53-10-1. DID HFEC INSPECTION PER NDT M/M 51-00-00. FABRICATED AND INSTALLED ANGLE PER SRM 51-40-04. ALODINED AND PRIMED PER SRM 51-10-2.