As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN BETWEEN STA 680 AND 700 AND BETWEEN STR 26L AND 26R WAS FOUND WITH TWO SPOTS OF CORROSION WHICH REQUIRED CUTOUTS. ADDITIONALLY, TWO EXISTING DOUBLER REPAIRS ARE IN THE AREA WITH LESS THAN 1 SEPARATION. ALL DAMAGE WAS REMOVED BY SPLICING IN A NEW SKIN PANEL FWD OF STA 710.