What was found
INSPECTION FOUND A 1 INCH CRACK IN INBOARD AND OUTBOARD ACTUATOR ROD END ATTACH RIBS OF NR 5 SLAT. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A DOUBLER AND ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN INBOARD AND OUTBOARD ACTUATOR ROD END ATTACH RIBS OF NR 5 SLAT. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A DOUBLER AND ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-1.