As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORRODED AREAS ON FUSELAGE STRINGER OUTER FLANGE BETWEEN FRAME 76-77, STRG 56 RT AND 56 LT. REPAIR PERFORMED BY REWORK CORROSION FOLLOWING ROTO- AND HFEC INSPECTION OF AREAS AND ADJACENT HOLES WITH NIL FINDINGS IAW EA 6-5318-95920 AND RAS/DATLS/0003029/2006 ISSUE A.