As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION CHECK FOUND A CRACK ON FUSELAGE SKIN AFT PASSENGER DOOR UPPER AFT CORNER STA 1660 LT, LONGERON 9 TO 12 LT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-047 & SRM 53-2-0 FIGURE 18.