As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE AT VERTICAL STAB STA 1016 L/H CLOSURE ANGLE BELOW PANEL 323AL IS WORN ON INBD SURFACE / REMOVED AND REPLACED UPPER FUSELAGE AT VERTICAL STA 1016 L/H CLOSURE ANGLE BELOW PNL 323AL IAW SRM 51-40-02-0G-0; DWG 147A0030 ID 0001 REV B USED BMS 5-95 B2 SEALANT MITED AT 10;00AM WITH ALL PERM FASTENERS INSTALLED BEFORE SQUEEZE OUT AT 3:00PM A96309