What was found
LEFT VERTICAL FIN ATTACH ANGLE HAS LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. REMOVED DAMAGE AND INSTALLED DOUBLER IAW PRI/ERA 533587-14, REV O.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL FIN ATTACH ANGLE HAS LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. REMOVED DAMAGE AND INSTALLED DOUBLER IAW PRI/ERA 533587-14, REV O.