As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN FOUND BULGING AT STA 2360 STR 34L - 42L. REMOVED BOLTS AND NUTS (TOTAL 8 EACH) AT STA 2360 BULKHEAD STR 34L TO STR 42L PER AMM 20-51-01 REV 90. HFEC INSPECTION CARRIED OUT IAW NDTPM D6-7170 REV 134 PART 6 51-00-00 FIG 23 ON BULGING SKIN. NO CRACKED EVIDENT. BOLTS AND NUTS AT STA 2360 BULKHEAD STR 34L TO STR 42L REINSTALLED PER PER AMM 20-51-01 REV 90.