As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
B757 53-3-0587 SUPPORT BRACKET CHAFING INTO FUSELAGE SKIN PANEL STA 1795 STR 17R AS VIEWED THRU ACCESS 311AL. RL0105 REF. ST. EN GINEERING N/R 0084140 FOUND FUS SKIN OUT OF LIMITS AT STA 1795 STRINGER 17R IAW B757-3 00 SRM 53-80-70-R4,.50" CRACK. CUT OUT DAMAGE,FABRICATED AND INS TALLED PERMENANT REPAIR IAW B757-300 SRM 53-80-70-R4 WORK ACCOMP LISHED BY MECH