As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFW - FUSELAGE SKIN HAS CORROSION ON INNER SURFACE AT STATION 412 TO 434 UNDER S37L. BLENDED OUT CORROSION USING A MINIMUM TAPER RATIO OF 20 TO 1. VISUALLY CONFIRMED NO FURTHER CORROSION. PERFORMED HIGH FREQUENCY EDDY CURRENT ON BLENDED AREAS AND HOLES SURROUNDING BLENDS. TREATED BLENDED AREAS WITH ALODINE AND TWO COATS PRIMER AND FILLED WITH BMS595 SEALANT.