What was found
INSPECTION FOUND A 2 INCH CRACK THROUGH TWO FASTENER HOLES OF RIB SUPPORT ANGLE AT WING LEADING EDGE SLAT STA 0. THE RIB SUPPORT ANGLE WAS REMOVED AND 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 A 2 INCH CRACK THROUGH TWO FASTENER HOLES OF RIB SUPPORT ANGLE AT WING LEADING EDGE SLAT STA 0. THE RIB SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.