As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING VISUAL INSPECTION OF FUSELAGE, THE MED NR 1L FORWARD LOWER REVEAL (STA 434) WAS FOUND CRACKED 1 INCH IN LENGTH HORIZONTALLY BELOW STOP NR 1 ON LOWER REVEAL. STOP DRILLED IAW SRM 51-10-01 AND BOEING TELEX AND 81180-3. TO BE REPLACED PRIOR TO 1,500 CYCLE OR 15 MONTHS WHICHEVER DONE FIRST. FORM 8110-3 ISSUED. (X)