What was found
DAMAGE ON FUSELAGE SKIN. THE PUNCTURE IS LOCATED BELOW THE S20L LAP JOINT AT APPROX BS 1581, 37 INCHES FWD OF SKIN PANEL EDGE AND 26 INCHES BELOW WL-0. REPAIR IAW ERA 496950-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGE ON FUSELAGE SKIN. THE PUNCTURE IS LOCATED BELOW THE S20L LAP JOINT AT APPROX BS 1581, 37 INCHES FWD OF SKIN PANEL EDGE AND 26 INCHES BELOW WL-0. REPAIR IAW ERA 496950-14.