What was found
DURING C1 CHECK, CRACK FOUND ON NR 3 SLAT COVE PANEL AT APPROX 5 INCHES INBD FROM OTBD PANEL EDGE & 2 INCHES UP FROM BOTTOM EDGE. REPLACED LT WING NR 3 SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4004.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C1 CHECK, CRACK FOUND ON NR 3 SLAT COVE PANEL AT APPROX 5 INCHES INBD FROM OTBD PANEL EDGE & 2 INCHES UP FROM BOTTOM EDGE. REPLACED LT WING NR 3 SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4004.