As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1/2" CRACK IN FUSELAGE SKIN AT THE R-2 DOOR LOWER HINGE CUTOUT FWD LOWER CORNER, STA 947.5, S13R TO S14R. THE CRACKED AREA OF SKIN WAS CUT OUT AND A REPAIR DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 53-60-01.