As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION ON FRAME 16 RT SIDE AT THE DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP FITTING 7 ON HOLE NUMBER 6 ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME 16 RT SIDE AT THE DOUBLE JOGGLE UPPER FUSELAGE, AS PER ER/A 588153-14AD REV PRI 1 AND PRI 0 AND ER/A 588153-14AD REV ORIGINAL.