What was found
INSPECTION FOUND A .5 INCH CRACK IN CUSP WEB AT FS 112, RBL 47. THE CRACK WAS STOP DRILLED IAW 53-01, FIGURE 2 AND A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-03, AND 53-01 FIGURE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN CUSP WEB AT FS 112, RBL 47. THE CRACK WAS STOP DRILLED IAW 53-01, FIGURE 2 AND A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-03, AND 53-01 FIGURE 4.