What was found
INSPECTION FOUND A 2" CRACK IN #3 SLAT LOWER BULLNOSE SKIN AT TWO RIVETS BELOW STOP O/B OF THE ACTUATOR. THE CRACKED AREA WAS CUT OUT AND FILLER AND 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 2" CRACK IN #3 SLAT LOWER BULLNOSE SKIN AT TWO RIVETS BELOW STOP O/B OF THE ACTUATOR. THE CRACKED AREA WAS CUT OUT AND FILLER AND SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.