What was found
STRINGER CRACKED IN VERTICAL FIN AT FIN STA 180.6 STRINGER 3 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR PARTS PER SRM 55-30-4 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER CRACKED IN VERTICAL FIN AT FIN STA 180.6 STRINGER 3 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR PARTS PER SRM 55-30-4 FIG 1.