What was found
DAMAGE WAS DISCOVERED IN THE FUSELAGE SKIN AT FS 654 +22 TO +66 AND STR 3R - 4R THAT RESULTED IN TWO SRM REPAIRS 4.875" APART. A DTA WAS ACCOMPLISHED AND THE INSPECTION REQUIREMENTS WERE IMPLEMENTED PER ERA 459157-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGE WAS DISCOVERED IN THE FUSELAGE SKIN AT FS 654 +22 TO +66 AND STR 3R - 4R THAT RESULTED IN TWO SRM REPAIRS 4.875" APART. A DTA WAS ACCOMPLISHED AND THE INSPECTION REQUIREMENTS WERE IMPLEMENTED PER ERA 459157-14.