What was found
LEVEL 2 CORROSION/BOTTOM OF FUSELAGE FILLET PANEL 194A HAS CORROSION AT ATTACH ANGLE. REMOVED DAMAGE, TREATED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 51-50-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 2 CORROSION/BOTTOM OF FUSELAGE FILLET PANEL 194A HAS CORROSION AT ATTACH ANGLE. REMOVED DAMAGE, TREATED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 51-50-04.