What was found
VERTICAL STAB MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN STA 110.4, STR 9 LT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1 & EA 7-5530-59892.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN STA 110.4, STR 9 LT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1 & EA 7-5530-59892.