As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK ON EXTERNAL FUSELAGE SKIN AT FORWARD RT SERVICE DOOR LOWER HINGE CUTOUT FORWARD EDGE SKIN. REMOVED SECTION OF SKIN AND INSTALLED REPAIR DOUBLER. REPAIRED PER SB 737-53-1074 FIG 3 AND SRM 53-30-3 FIG 32. (M)