What was found
INSPECTION FOUND TWO 2 CRACKS IN LT WING RIB TO UPPER SKIN ATTACH ANGLE AT SLAT STA 0 INSIDE LEADING EDGE AREA. THE ANGLE WAS REPLACED IAW SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO 2 CRACKS IN LT WING RIB TO UPPER SKIN ATTACH ANGLE AT SLAT STA 0 INSIDE LEADING EDGE AREA. THE ANGLE WAS REPLACED IAW SRM 51-10-1.