As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LWR FUSELAGE STA Y79 TO STA Y589 BETWEEN LONGERON 21L AND 22L EXTERNAL SKIN WITH TOOL MARKS. REMOVED DAMAGE, NDT NO DAMAGE NOTED. FABRICATED REPAIR PARTS PER SRM 53-04 FIG 38 PG 218L. TREATED AND PRIMED PARTS PER SRM 51-10-3 PARA 14 AND 21. INSTALLED ALL REPAIR PARTS PER SRM 53-04 FIG 38 PG 218L.