As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE SKIN PANEL IS DEBONDED AT STA X182.00, STR 29P TO 30P. UNRIVETED, DISBONDED AREA FOR FURTHER EVALUATION. CUT OUT DEBONDED SKIN AND WAFFLE DOUBLER. PERFORMED HFEC AND BOND TEST INSPECTION. NO DISCREPANCIES FOUND. REPAIRED IAW EO8-53-13-0248.