As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE AT STA 1000 BETWEEN STRINGERS 41L - 43L FOUND SKIN CORROSION. SKIN TRIMMED-OUT, REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED PER SRM 53-30-03 REV 117 FIGURE 48. REPAIR REPETITIVE INSPECTION THRESHOLD AT 15, 000FC WITH INTERVALS OF 6000FC (INT HFEC) AND 1500FC (EXT LEFC).