As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE SKIN: WAVY PREVIOUS REPAIR FROM STA Y=181 TO Y=228 BTW LONG 22R TO 26R. DAMAGE PREVIOUS REPAIR WAS REMOVED AND REPLACED FOR NEW ONE CORRECT REPAIR PER SRM 53-04 FIGURE 12C. PERFORM EXTERNAL VISUAL INSPECTION THRESHOLD 8000 LANDINGS AND REPETITIVE INTERVAL 8000 LANDINGS PER SRM 53-04 FIG.12C SHEET 12 GENERAL NOTE 31.