As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, CREASE ANGLE IS CRACKED UNDER TRIANGULAR RIB, UPPER IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360 THE CREASE CHORD WAS REPAIRED REF EO NR 7-5530-7-2303 PRT 5, REV Q. JPF STEPS 20-30 AND SRM 51-40-03 FIG, THIS IS CLASSIFIED AS A MINOR REPAIR.