As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB; BS 1024 TO 1036; STR 1 TO 2 LT; WL 308 / REMOVED CORROSION ON FUSELAGE SKIN UNDER VERTICAL STAB B/S 1024-1036 STR 1-2 L/H W/L 308. REPAIRED PER ATS ER 21-01081 REV IR AND SWA EA 21-153-00179 REV IR