As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERNAL STRINGER BELOW VERT STAB AT LT MIDDLE FIN TO FUSELAGE FITTING IS CORRODED. R & R ON FUSELAGE EXTERNAL STRINGER 3L BELOW VERT STAB IAW 51-40-21. REMOVED CORROSION AT STRINGER 3L, ORIGINAL THICKNESS .155 AFT REWORK MATERIAL LOSS IS .040. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-14. MAJOR REPAIR.