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 1072; STR 2LT TO 3' BELOW / REMOVED CORROSION ON FUSELAGE SKIN UNDER VERTICAL STAB BS1040-1072 STR 2L/H TO 3' BELOW W/L308 REPAIRED PER ATS ER 21-01081 REV IR AND SWA EA 21-153-00179 REV IR