As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT CV2 IN TPA, THE FUSELAGE SKIN AT STA 540 BETWEEN S-26R AND S-27R, JUST BELOW THE LAP SPLICE HAS BEEN TRIMMED TO REMOVE CORROSION. THE CUT OUT MEASURES 5 INCH BY 11 INCH. THIS ER/A REPAIRS THE AREA BY ADDING A .090 2024-T3 CLAD FILLER, .050 2024-T3 CLAD DOUBLER AND A .063 2024-T3 CLAD TRIPLER. ACCOMPLISHED REPAIRS PER DL ERA 302359-14.