As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT VERTICAL FIN SKIN HAS 2 POSSIBLE CRACKS EMANATING FROM FASTENERS AT BS 1214 COMMON TO SPAR ** SD ** DAMAGE TO RT VERTICAL FIN SKIN AT BS 1214 COMMON TO FRONT SPAR FORGING JUST ABOVE FUSELAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-01, REPAIRED DAMAGE IAW 55-30-3.