As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C/W ERA 485640-14 REV A PEREMANENT REPAIR OF FUSELAGE SKIN AT STA 1697 JUST BELOW STR 19L REF NRC 2. DENT CUTOUT DIMENSIONS ARE 3.15 FWD/AFT 2.85 UP/DWN DID HFEC SURFACE SCAN AND BOLT HOLE COMMON TO REPAIR. .040 INSURANCE CUT. INSTALLED .050 FILLER, 2 EA STRUCTURAL FILLERS ONE .040 AND .032 AND DBL .063 ALL MADE FROM 2024 T3 CLAD.