What was found
NR 10 SLAT T/E WEDGE DENTED. REMOVED DAMAGE IS .950 DIA 33" FROM OTBD EDGE AND 6" FWD OF AFT EDGE IN UPPER SKIN. REPAIRED IAW EO:B757-5750-50873-A COMPOSITE REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 10 SLAT T/E WEDGE DENTED. REMOVED DAMAGE IS .950 DIA 33" FROM OTBD EDGE AND 6" FWD OF AFT EDGE IN UPPER SKIN. REPAIRED IAW EO:B757-5750-50873-A COMPOSITE REPAIR.