As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AROUND NUTPLATES ON TRANSITION PANEL FS 727F-727E S26L. ACFT GROUNDED. REMOVED CORROSION AROUND NUTPLATES ON TRANSITIONAL FROM STA 727 TO STA 727E, S26K. ORIGINAL THICKNESS IS .040, REMAINING THICKNESS IS .022. REMOVED .018. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REPAIRED DAMAGED TRANSITION PANEL IAW SRM 53-00-53 ALODINED & PRIMED IAW SRM 51-20-01. DISPLACED AND REINSTALLED FLOOR PANEL 140EF IAW AMM 25-52-10.