As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LEFT HAND SIDE OF THE AFT PASSENGER DOOR SKIN IN THE FORWARD LOWER CORNER BELOW AN EXISTING REPAIR AT FUSELAGE STATION 1640 LONGERON 22L. REPAIR ACCOMPLISHED, REMOVAL OF EXISTING DOUBLER, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLERS DOUBLERS AND TRIPLERS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING AUTHORITY 28276-5248-02-110.