As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE EXTERIOR NOSE SECTION AT BS 310 THROUGH 330 BETWEEN STRINGERS 21R TO STRINGER 22R SKIN WAS DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER TREATED AND PRIMED AREA IAW SRM 53-30-3 FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)