What was found
FUSELAGE SKIN PANEL DAMAGED BETWEEN BS 136.80 - 151.60, STRINGERS 31S - 32S. REPAIRED IAW RD8-53-15610, AND ECO 008.53-18.11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN PANEL DAMAGED BETWEEN BS 136.80 - 151.60, STRINGERS 31S - 32S. REPAIRED IAW RD8-53-15610, AND ECO 008.53-18.11.