As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, FUS EXTERIOR SKIN BULGE AT FWD SIDE OF FUS FWD JACK PAD AT FS 348.2 AT STR 21R. CUT OUT DAMAGED SECTION OF SKIN AND REMOVED CORROSION FROM UNDERLYING SURFACES PER SRM 51-10-6. INSTALLED DOUBLER REPAIR 12 INCHES BY 20 INCHES .050 2024-T3 PER SRM 53-30-3 FIG 1. TOTAL CYCLES 29577.