What was found
TUL - 2 INCH CRACK ON RIGHT VERTICAL STABILIZER-TO-FUSELAGE ATTACH ANGLE, HORIZONTAL SIDE. VERIFIED ENDS OF CRACK. CUT OUT DAMAGED SECTION. INSTALLED FILLER AND REPAIR ANGLE PER AARD 53-10-00-2 AND FIGURE 1 DATED 1-5-94. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - 2 INCH CRACK ON RIGHT VERTICAL STABILIZER-TO-FUSELAGE ATTACH ANGLE, HORIZONTAL SIDE. VERIFIED ENDS OF CRACK. CUT OUT DAMAGED SECTION. INSTALLED FILLER AND REPAIR ANGLE PER AARD 53-10-00-2 AND FIGURE 1 DATED 1-5-94. (X)