As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BULGE AND SKIN CRACKED AT APPROX FS 1600, JUST AFT OF AFT PRESSURE BULKHEAD APPROX L33L. CUT OUT AREA OF CORROSION, FABRICATED DOUBLER FROM 7075-T6 .071 AND FILLER FROM 7075-T6 .063 IAW SRM 53-2-1 FIG 7. TREATED PRIMED AND INSTALLED IAW SRM 53-2-1 FIG 7.