What was found
INSPECTION FOUND DORSAL FIN LT INNER ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND DORSAL FIN LT INNER ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2.