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 HAD SKIN BULGE AT FS 1150 AT STR 23R. REMOVED STRINGER AND FASTENER AS PER SRM 53-10-3. REMOVED SURFACE CORROSION ON SKIN IN SECTION AS PER SRM 51-10-6 LESS THAN .003. ALODINE AND PRIMED AS PER SRM 51-10-2. INSTALLED STR 23R BETWEEN STA 1130 TO 1170 AS PER SRM 53-10-3. TOTAL CYCLES 29577.