What was found
DORSAL FIN FUSELAGE RT SIDE ANGLE IS CRACKED AT CENTER (1). REMOVED AND REPLACED ANGLE PER SRM 51-30-02, 51-10-04, 51-10-03,AND 51-30-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DORSAL FIN FUSELAGE RT SIDE ANGLE IS CRACKED AT CENTER (1). REMOVED AND REPLACED ANGLE PER SRM 51-30-02, 51-10-04, 51-10-03,AND 51-30-04.