What was found
CRACK ON LT DORSAL FIN ATTACH FITTING. FITTING WAS INSTALLED IAW SRM 51-30-5 BOLTS WERE TIGHTEN IAW AMM 20 30 01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT DORSAL FIN ATTACH FITTING. FITTING WAS INSTALLED IAW SRM 51-30-5 BOLTS WERE TIGHTEN IAW AMM 20 30 01.