What was found
VERTICAL STAB PANEL AT VSS ZFS-6.562, LT SIDE HAS A CRACK FROM EDGE OF PANEL EXTENDING 5/8 INCH PAST FASTNER. FIRST HOLE BELOW UPPER AFT CORNER OF INLET PANEL. VERIFIED BY NDT. REPAIRED THE SKIN IAW SRM 55-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB PANEL AT VSS ZFS-6.562, LT SIDE HAS A CRACK FROM EDGE OF PANEL EXTENDING 5/8 INCH PAST FASTNER. FIRST HOLE BELOW UPPER AFT CORNER OF INLET PANEL. VERIFIED BY NDT. REPAIRED THE SKIN IAW SRM 55-01.