As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT D-CHECK, CORROSION AT LT MOUNTING FLANGE FOR LOWER FUSELAGE ACCESS PANEL 1104 INTERIOR AND EXTERIOR. CUT OUT DAMAGED TIE ANGLE SKIN ATTACHMENT. INSTALLED NEW CHORD ANGLE PER SRM 51-10-4. REPLACED TIE ANGLES AT FRAMES BS 330, 320 AND 300 PER SRM 53-10-4, 4 BY 1 BY 5. N/R 3444.