What was found
DURING C1 CHECK, CRACK FOUND ON NR 2 OTBD SLAT COVE PANEL AT APPROX. 29 INCHES INBD FROM OTD EDGE & 3 INCHES UP FROM LOWER SIDE. REPLACED LT WING 2 OTBD SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4076.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C1 CHECK, CRACK FOUND ON NR 2 OTBD SLAT COVE PANEL AT APPROX. 29 INCHES INBD FROM OTD EDGE & 3 INCHES UP FROM LOWER SIDE. REPLACED LT WING 2 OTBD SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4076.