As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FRAME AND BULKHEAD AT Y= 680 TO 683 BETWEEN LONGERONS L35L TO L35R. REMOVED FRAME SECTION, SPLICE AND DOUBLERS. FABRICATED AND INSTALLED REPAIR ANGLES TO FRAME AND REPAIR DOUBLER TO BULKHEAD IAW COTNEY ENGINEERING ORDER SKA 95148-3 AND SRM 51-1-8.