What was found
INSPECTION FOUND A 2.5 INCH CRACK IN FORWARD RIB OF LT HORIZONTAL STABILIZER TIP. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-00-01, FIGURE 2 AND SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.5 INCH CRACK IN FORWARD RIB OF LT HORIZONTAL STABILIZER TIP. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-00-01, FIGURE 2 AND SRM 51-31-01.