What was found
INSPECTION FOUND A 1 CRACK IN ANGLE AT BASE OF LT LOWER AFT SIDE VERTICAL STABILIZER. FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-05, FIGURE 23A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 CRACK IN ANGLE AT BASE OF LT LOWER AFT SIDE VERTICAL STABILIZER. FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-05, FIGURE 23A.