As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE ON FUSELAGE SKIN 1" X 1" HOLE. FUSELAGE PUNCTURED BOTTOM LEFT APROX STA 640 WL 144. HOLE IS APPROX 1 INCH BY 1 INCH. HOLE LOCATION IS AT BS STA 668 & ABV STR 26L RCV'D AVO1269 REV 2, REF ECRA 5300-01414. ACCMP'D PERMANENT REPAIR IAW EG DOCUMENT. CUT OUT DAMAGE STA 668 STR 26L PER AVO1269.