As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INTERNAL SKIN AT BS 1065 TO 1087 BETWEEN STRINGERS 39L TO 39R, FOUND CORROSION. REF TO CPCP TASK 53-544-00. THE CORROSION ON FUSELAGE INTERNAL SKIN AT BS 1065 TO 1087 BETWEEN STRINGERS 39L TO 39R WAS REPAIRED IAW PRI 583419-14, REV 0 . THE PRI 583419-14 REV 0 COMPAIRED AND COMPLETED WITH ERA583419 -14 REV ORIGINAL ASSOCIATED ER/A 14-583419.