What was found
INSPECTION FOUND A .25 INCH CRACK IN INTERNAL SKIN OF RT WING LEADING EDGE SLAT NR 4. A REPAIR WAS PERFORMED IAW SRM 57-00-01, PAGE 12, FIGURE 4, SHEET 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN INTERNAL SKIN OF RT WING LEADING EDGE SLAT NR 4. A REPAIR WAS PERFORMED IAW SRM 57-00-01, PAGE 12, FIGURE 4, SHEET 2.