What was found
RIGHT WING, NR 8 SLAT, INNER SURFACE SKIN HAS A CRACK. REMOVED, FABRICATED, REINSTALL NEW COVE SKIN O/T NO. 8 SLAT IAW DWG 114N4077 AND SRM 51-40-02-0G MATERIAL 7075 T6.056 THICK, NO DEVIATION IAW OPS CHECK AMM 27-81-02-424-021.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING, NR 8 SLAT, INNER SURFACE SKIN HAS A CRACK. REMOVED, FABRICATED, REINSTALL NEW COVE SKIN O/T NO. 8 SLAT IAW DWG 114N4077 AND SRM 51-40-02-0G MATERIAL 7075 T6.056 THICK, NO DEVIATION IAW OPS CHECK AMM 27-81-02-424-021.