As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REAR HINGE CASTING FAILED HALFWAY ALONG ARM OF RADIUS, PN 35/815016/7 WHILE APPROACH TO LAND: POSSIBLE CAUSE IS WEAR IN THE FRONT HINGE PIVOT BRACKET BOLT HOLES WHICH COULD CAUSE VIBRATION. INSPECT BOTH FRONT AND REAR BOLT HOLES FOR WEAR ALIGNMENT BY DISCONNECTING THE ACTUATING ROD, REPLACE AS NECESSARY. (X)