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 FWD SERVICE DOOR UPPER FWD CORNER STA 440 LONGERON 10 TO 12 RT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 53-044 & SRM 53-2-0 FIGURE 14.