What was found
MULTIPLE DAMAGE ON LOWER FUSELAGE SKIN PANEL LOCATED BETWEEN BS 1031 - 1051, STRINGERS 21R AND 26R. DAMAGE CAUSED BY AIR CONDITIONING EXTERNAL CONNECTION COVER AND LANYARD STRIKING FUSELAGE
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MULTIPLE DAMAGE ON LOWER FUSELAGE SKIN PANEL LOCATED BETWEEN BS 1031 - 1051, STRINGERS 21R AND 26R. DAMAGE CAUSED BY AIR CONDITIONING EXTERNAL CONNECTION COVER AND LANYARD STRIKING FUSELAGE