As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE R/H TRANSITION ANGLE FROM STA 500+8 TO 500A HAS CORROSION AROUND THE FASTENER HOLES / [01] REMOVED CORROSION PER SRM 51-10-02 ; FOUND TO BE OUT OF LIMITS ( 0.011 ) PER SRM 53-00-53-1A-2 .;[02] REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02 AND SRM 51-10-02;[03] INSPECTED WORK PERFORMED