As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INNER DORSAL FIN JOINT ANGLE RT FOUND CRACKED / DAMAGED ANGLE WAS REPLACED REF SRM 51-10-05, 51-30-02 AND 51-30-05. FUSELAGE SKIN CRACK FOUND AT STA 1475 DAMAGED AREA WAS CUT OUT AND REPAIR INSTALLED PER ERA 487464-14AD REF N/R S/N 499893.