What was found
INSPECTION FOUND A 1/2" CRACK IN R/H WING #4 SLAT SKIN LOWER AREA, BELOW ACTUATOR ATTACHMENT TO SLAT. THE CRACKED AREA WAS CUTOUT. REPAIR FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1/2" CRACK IN R/H WING #4 SLAT SKIN LOWER AREA, BELOW ACTUATOR ATTACHMENT TO SLAT. THE CRACKED AREA WAS CUTOUT. REPAIR FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.