As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE R/H UPPER ATTACH POINT SUPPORT FLANGE CRACKED ON THE APU TAIL CONE. MAINTENANCE REMOVED THE DAMAGED AREA FABRICATED A NEW PART AND INSTALLED A DOUBLER IAW ETD2019-145-009415. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.