As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER CLIP AT FRAME 80 TO STRINGER 8R HAS A 3/4 INCH CRACK. R & R STRINGER CLIP AT FRAME 80 TO STRINGER 8R IAW SRM 51-40-02. RESTORED SURFACE FINISH TO AFFECTED AREA OF EXTERNAL FUSELAGE IAW CPM 51-21-07, ETN -EM-51-91 & ETN-EM-51-120.