As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND EXTENSIVE DAMAGE TO STATION 500 FUSELAGE CIRCUMFERENTIAL FRAME INNER CHORD BETWEEN STRINGER 28 TO 31 LEFT DUE IMPACT DAMAGE FROM CARGO PALLETS. PERFORMED HIGH FREQUENCY EDDY CURRENT SURFACE SCAN TRIMMED EDGES OF REMAINING CHORD, REMOVED ALL NICKS, SCRATCHES, GOUGES, BURRS AND SHARP EDGES. ACCOMPLISHED SPLICE REPAIR PER EA B767-53-013524.