As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GOUGE / DENT FOUND DURING PRIMARY INSPECTION AT FUSELAGE STA 755 L-24 & L25 MEASURED 3.00 X .133. ACCOMPLISHED HFEC INSPECTION ON DENT, NO CRACKS FOUND FOLLOWING BLEND-OUT OF THE EFFECTED AREA ACCOMPLISHED UT INSPECTION OF EFFECTED AREA AND FOUND SKIN THICKNESS OUT OF LIMITS. ORIGINAL THICKNESS .071. LOWEST THICKNESS FOLLOWING BLENDING .052. CLASS 1 REPAIR BEING ACCOMPLISHED IAW SRM 53-00-01.