What was found
INSPECTION FOUND A .75 INCH CRACK AND LOOSE RIVETS IN RT WING SLAT NR 3 AT AFT SIDE. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3 AND 51-10-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK AND LOOSE RIVETS IN RT WING SLAT NR 3 AT AFT SIDE. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3 AND 51-10-04.