As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS A SHARP DENT AT BS 420 BELOW STR 18L. CUT OUT DAMAGE AREA 1.90 X 1.60 INCH AT BS 420 BELOW STR 18L IAW B-727 SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER 10 X 7.375 INCH 2024 T-3 -.071 PO 9912598 IAW B-727 SRM 53-30-3 FIG 3. TREATED AND PRIMED IAW B-727 SRM 51-10-6. INSTALLED REPAIR DOUBLER IAW B-727 53-30-3 FIG 3.