What was found
THE LT DORSAL ATTACH ANGLE HAD A .25 INCH CRACK IN VERTICAL LEG. REPLACED LT DORSAL FIN ANGLE PER MO72R22.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE LT DORSAL ATTACH ANGLE HAD A .25 INCH CRACK IN VERTICAL LEG. REPLACED LT DORSAL FIN ANGLE PER MO72R22.