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 1040 TO 1045; STR 2 RT TO 3' ABOVE / REMOVED CORROSION ON FUSELAGE UPPER SKIN UNDER VERTICAL STAB BS 1040 TO 1045 STR 2 R/H TO 3' ABOVE. REPAIRED PER EA 21-153-00179 REV IR AND ER 21-01081 REV IR