As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND FUSELAGE SKIN ON INNER SIDE HAD CORROSION BLEND BEYOND SRM LIMITS. BLEND OUT CORROSION PER ATTACHED SKETCH. DYE CHECK TO ENSURE CRACK FREE. ROTO PEEN BLENDED AREA. REFINISH THE BLENDED AREA PER SRM. FILL BLENDED AREA WITH BMS 5-95. SHIM AS REQUIRED TO REINSTALL THE DRAIN BRACKETS TO THEIR PREVIOUS LOCATIONS PER MRB 767-2528. (M)