As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AN EVIDENT DENT DAMAGE WAS FOUND DURING THE INITIAL INSPECTION ON FUSELAGE SKIN STA 1197+88 / STA 119+110, AND BETWEEN STRINGER S-22L / S-24L.(<P >THE DAMAGE WAS REPAIRED IN / ACCORDANCE WITH B767-300 SRM 53-00-01-2R-1 REPAIR 1. SEE RAM FORM / N662GT-20-01.</P>)