As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK AT STATON 332.10 LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED DOUBLER PER EA, GENERATED OM-7 NR 13021 FOR FINAL REPAIR DUE IN 18 MONTHS OR 4500 CYCLES. REPAIRED PER EA 59266 AND SRM 53-30-3 FIG 26. (M)