As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE DAMAGE AREA OF STA 500, 520 STR 17L,18L ON LEFT SIDE OF FUSELAGE APPROX 10 FT FROM DOOR 1L AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED: INTERIM RPR DONE PER BOEING MSG REQUIRED PERM RPR BY GSO. FUSELAGE SKIN REPAIRED WITH DOUBLER-FILLER REPAIR PER REO G138 42, REV D ON NON ROUTINE 20001. CREATED CF9079 PER EVA 81204 FOR 24 MONTH DTA.