What was found
INSPECTION FOUND A 5 INCH CRACK IN CUSP WEB AT FS 886, LBL 50. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-4, AND 51-20-0.
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 886, LBL 50. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-4, AND 51-20-0.