As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN, DOUBLER, ANT TRIPLER ARE CRACKED IN THE UPPER FORWARD CORNER OF THE R-1 DOOR CUTOUT. THE CRACK IS 0.5 LONG AND RAN FROM THE EDGE OF THE CUTOUT TO A LOCAL RIVET HOLE. THE SKIN IN THE AREA IS 0.040 THICK, THE DOUBLER IS 0.025 THICK AND THE TRIPLER IS 0.020 THICK ALL THREE LAYERS ARE MANUFACTURED FROM CLAD 2024-T3 SHEET.