As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION ON FRAME AT STA 1680 BETWEEN STR 29 RT AND STR 30. MAJOR REPAIR ACCOMPLISHED: PERFORMED A GVI OF FUSELAGE STRUCTURE BETWEEN BS 1664-1700 AND STR 26L-26R. FOUND CORROSION ON FRAME, BS 1681 AND SHEAR TIE BETWEEN ST R-27L-28L. REMOVED FRAME AND FABRICATED A NEW FRAME PER BAC DWG 146N1032-3, REV B AND INSTALLED PER BAC DWG 146N1025, REV C AND SRM 51-40-2.