As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C CHECK, FUSELAGE FRAME GOUGED AT BS 480 BELOW STRINGER 17L. BLENDED AREA AT BS 480 BELOW STRINGER 17L, ORIGINAL MATERIAL 0.150", MATERIAL REMAINING WAS APPROXIMATE 40% OF THICKNESS LEAVING 60% FOUND TO BE WITHIN LIMITS IAW EO NR OE-N765AT-1-25-08. TREATED AND PRIMED AREA IAW SRM 51-10-2 AND EVA B253-00043.