As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE SKIN AT FR 38 AND STR 42R HAS 1 EA TOOL MARK SURROUNDING FASTENER 1 IN LENGTH X 1 IN WIDTH X 0.007 IN DEPTH. TOOL MARK BLENDED, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. DAMAGE CUTOUT AND WAS NDT INSPECTED IAW NTM 51-10-08 AND NO CRACKS FOUND. DOUBLER AND FILLER FABRICATED AND INSTALLED IAW SRM 53-10-12, FIG 224.