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, N/R 54096 FUSELAGE HAS (2) DENTS BETWEEN STA 1070-1090 BETWEEN STR 17L-18L. CUT-OUT 1 EACH DENT AREA DIM 1.0 X 1.0 IAW B-727 SRM 53-30-3 FIG 3. EVALUATION OF SECOND DENT IS WITHIN LIMITS BY A/Y RATIO A .039 DIVIDED BY Y 1.54 = 38.46 IAW B-727 SRM 53-30-1. FAB DOUBLER FORM 2024-T3 .071 PO 9912441 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 3.