What was found
TUL - FOUND CRACK BETWEEN RIVETS ON VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE 8 INCHE FORWARD OF VERTICAL REAR SPAR ATTACH POINT. CUT OUT DAMAGED AREA. INSTALLED DOUBLER ANGLE PER AARD 53-10-00-2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - FOUND CRACK BETWEEN RIVETS ON VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE 8 INCHE FORWARD OF VERTICAL REAR SPAR ATTACH POINT. CUT OUT DAMAGED AREA. INSTALLED DOUBLER ANGLE PER AARD 53-10-00-2. (M)