As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MISS DRILLED ONE EACH FASTENER HOLE IN FWD FUSELAGE SKIN DURING THE REMOVAL OF EXISTING REPAIR DOUBLER AT FR 2+0.750" S11R+8.250. CUTOUT DAMAGE IN FWD FUSELAGE SKIN AT FR 2+.0750" AND STGR 11R + 8.250". REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED.