As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** ON THE EXTERIOR FUSELAGE SKIN AT STA 1016 BETWEEN STR'S 27L AND 26R / REMOVED FASTENERS ON EXTERIOR FUSELAGE SKIN AT STA. 1016; BETWEEN STR'S 27L AND 26R; I.A.W. - S.R.M. 51-40-02-06-0. REMOVED CORROSION; I.A.W. S.R.M. 51-10-02-0G-0. REMAINING MATERIAL DETERMINED TO BE .060' BY NDI; UT. AREA REPAIRED; I.A.W. E.R. #19-02777; REV. IR AND EA 1-753-34659 REV IR