What was found
INSPECTION FOUND A 1.5 INCH CRACK AND BEND IN LT HORIZONTAL STABILIZER TIP O/B LOWER AFT CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-11-0, 51-30-2, AND 51-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK AND BEND IN LT HORIZONTAL STABILIZER TIP O/B LOWER AFT CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-11-0, 51-30-2, AND 51-30-3.