What was found
INSPECTION FOUND TWO 2.5 INCH CRACKS AT RIVET HEADS FORWARD OF OUTBOARD SEQUENCE CARRIAGE ATTACH POINT OF RT INBOARD FOREFLAP. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO 2.5 INCH CRACKS AT RIVET HEADS FORWARD OF OUTBOARD SEQUENCE CARRIAGE ATTACH POINT OF RT INBOARD FOREFLAP. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30.