As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT FRAME LEG X240.500 BETWEEN STR. 28P AND 27P. REMOVED BRACKET FROM FRAME AT STA.X240.500. REMOVED FRAME SECTION AT STA X240.500, FORMED AND HEAT TREATED FRAME MEMBER IAW DWG 85320497. ALODINED AND PRIMED AS REQUIRED. COMPLIED WITH CONDUCTIVITY TEST.