What was found
INSPECTION FOUND A 1 INCH CRACK IN NR 8 SLAT INNER SKIN AFT OF ACTUATOR CUTOUT. THE SLAT PANEL WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN NR 8 SLAT INNER SKIN AFT OF ACTUATOR CUTOUT. THE SLAT PANEL WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2.