As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE TAILCONE HAS A DELAMINATION ON INNER SURFACE AT BS 1156+32'; AT 11 O'CLOCK POSITION. <[01] 04 - REPAIRED PER [SRM 51-70-05-2R-1-A00732 (REPAIR 1 - REPAIR OF DAMAGE TO ONE SKIN OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT)]; [02] TASK CARD COMPLETED.