As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSP, A CRACK WAS DISCOVERED IN A SUPPORT BEAM JUST BELOW FRAME 5 IN THE FUSELAGE TAILCONE. A REPAIR SCHEME REQUEST WAS SUBMITTED AND RECEIVED FROM THE MFG. THE CRACK WAS STOPPED DRILLED AND A REPAIR DOUBLER FROM 0.050" ALUMINUM WAS INSTALLED.