As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES STA 727E-747 ; / [01] C; [02] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [03] PROCURED NEW ANGLE; PART WILL BE INSTALLED ON 5360-E-16462-NG IAW SRM 51-10-02.