What was found
VERTICAL STAB, TAIL CONE PANEL 326CT HAS TWO HOLES ON LT SIDE. C-CHECK, REMOVED AND INSTALLED AFT FRAME AND AFT FAIRING, 326CT ASSEMBLY IAW AMM 55. REPAIRED TAIL CONE PANEL 326CT REF STS EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB, TAIL CONE PANEL 326CT HAS TWO HOLES ON LT SIDE. C-CHECK, REMOVED AND INSTALLED AFT FRAME AND AFT FAIRING, 326CT ASSEMBLY IAW AMM 55. REPAIRED TAIL CONE PANEL 326CT REF STS EA.