As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) INDICATION WAS A 1/2 INCH CRACK IN THE EDGE OF THE DOOR SKIN WHICH HAD PREVIOUSLY BEEN STOP DRILLED. INSPECTION FOUND PART TO HAVE A 3 INCH CRACK ACROSS FOUR RIVET HOLES. A CRACK WAS ALSO FOUND AT TWO OF THE FOUR RIVET HOLES WHICH PICK UP THE HINGE IN THE BULKHEAD P/N 46550-04.