As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON EXTERNAL FUSELAGE SKIN AT FASTENER HOLE OF R-2 DOOR CUTOUT AT FORWARD LOWER CORNER. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED AN INNER PLATE, OUTER PLATE, AND A FILLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-3, PG. 200-227, FIG. 46.