As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L1 DOOR CUTOUT SKIN AT UPPER HINGE HAS A CRACK ON PANEL. REMOVED DAMAGED SKIN AT UPPER HINGE ANGLE IAW SRM 51-10-2. PREFORMED HFEC INSPECTION AROUND SKIN CUTOUT IAW NDTM PART 6 51-00-00 PER 23. CRACK CONFIRMED. FABRICATED A REPAIR IAW DWG 141A8222, AND SRM 51-20-01. INSTALLED IAW SRM 51-40-02 AND DWG 141A8222.