As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 UPPER FUSELAGE ANGLE AT BASE OF VERTICAL STAB AT STA 1723.076 CANTED FRAME IS CORRODED BEYOND LIMITS CUT OUT CORRODED AREA,NDT CUTOUT,NO CRACKS NOTED FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-2-5 FIG 16A.