What was found
INSPECTION FOUND A 2 INCH CRACK IN LT WING ANGLE AT OUTBOARD SIDE OF LEADING EDGE NOSE RIB, SLAT STA 0. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN LT WING ANGLE AT OUTBOARD SIDE OF LEADING EDGE NOSE RIB, SLAT STA 0. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-3.