As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SEVERAL FATIGUE CRACKS WERE FOUND IN THE FUSELAGE SKIN JUST AFT OF THE FORWARD GALLEY DOOR AND FORWARD OF THE STA 360 PRODUCTION JOINT. *S/U* FASTENER HOLE CRACKED AT STR 15R WAS REPAIRED PER SRM 53-30-3, FIGURE 43. FASTENER HOLES CRACKED AT STR 16R WERE REPAIRED PER SRM 53-30-3, FIGURE 6.