What was found
INSPECTION FOUND A .5 INCH CRACK IN THE LT WING NR 1 SLAT LOWER SKIN AT FASTENER AREA O/B OF I/B AUX TRACK. THE CRACKED AREA WAS REMOVED AND FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN THE LT WING NR 1 SLAT LOWER SKIN AT FASTENER AREA O/B OF I/B AUX TRACK. THE CRACKED AREA WAS REMOVED AND FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 201.