What was found
THE FUSELAGE SKIN WAS DENTED AT STA 540, STRINGER 16L. A FLUSH REPAIR AND STRINGER SECTION SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03, 53-30-05, AND ECRA 5331-01039.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN WAS DENTED AT STA 540, STRINGER 16L. A FLUSH REPAIR AND STRINGER SECTION SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03, 53-30-05, AND ECRA 5331-01039.