What was found
LEFT TRANSITION PANEL HAD CORROSION AT BS 500C+6 TO 500I, STRINGER 24L. ACCOMPLISHED A SPLICE REPAIR IAW SRM 53-00-53-2R-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT TRANSITION PANEL HAD CORROSION AT BS 500C+6 TO 500I, STRINGER 24L. ACCOMPLISHED A SPLICE REPAIR IAW SRM 53-00-53-2R-5.