As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURAL INSPECTION AT THE UPPER FUSELAGE MAIN CARGO CABIN, IT WAS FOUND AT BS 927 STR 17RH, THE FRAME ATTACH FITTING WITH FASTENER HOLE WITH BROKEN SCREW. THE AFFECTED FRAME ATTACH FITTING WAS REPAIRED AS PER AEI E.O.5332 AND APPROVED UNDER FAA 8110-3 FORM PROVIDED BY AEI.