What was found
INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN PANEL AT STA 780, STRINGER 15L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN PANEL AT STA 780, STRINGER 15L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01.