As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT THE UPPER FUSELAGE WAS DENTED AT STA 427 BETWEEN LONGERON 17L AND 18L. LENGTH 2 INCHES BY WIDTH 0.025 AND DEPTH 0.040 (GOUGE). BLENDED GOUGES AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 PAGE 207 VIEW G. NDT INSPECTED FOR CRACKS AND NO CRACKS FOUND.