As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION CHECK WAS FOUND A CRACK ON FUSELAGE SKIN AFT PASSENGER DOOR LOWER FWD CORNER STA 1660 LT LONGERON 21 TO 23 LT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-045 & SRM 53-2-0 FIGURE 18.