What was found
FUSELAGE PUNCTURED BOTTOM LEFT APPROXIMATELY BS 640 AND WL 144. HOLE IS APPROX 1 INCH BY 1 INCH. HOLE LOCATION IS AT BS STA 668 AND ABOVE STRINGER 26L. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EG DOCUMENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE PUNCTURED BOTTOM LEFT APPROXIMATELY BS 640 AND WL 144. HOLE IS APPROX 1 INCH BY 1 INCH. HOLE LOCATION IS AT BS STA 668 AND ABOVE STRINGER 26L. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EG DOCUMENT.