As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING ROUTINE SCHEDULED MX SEVERAL CHAFES WERE FOUND AT A PREVIOUS REPAIR ON THE LT SIDE OF THE FUSELAGE AT FRAME 30 AREA BETWEEN STRINGERS 17L & 18L. AREA IS LOCATED NEAR THE HEAT EXCHANGER. 6" LONG BY .750" WIDTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-120-53-002. RII INSPECTIONS COMPLIED WITH IAW EO 10-120-53-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.