As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C1 FUSELAGE NOSE EXTERIOR SKIN IS OIL CANNING AND DENTED AT STA -3 TO -12 L21L TO L22L. CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER AT STA -32 TO -12 L21L TO L22L IAW SRM 53-2-01 FIG 7.