What was found
INSPECTION FOUND RT DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND RT DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED. THE ATTACH ANGLE WAS REPLACED IAW EA 5340-01012.