What was found
DURING C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL NR 9502, INNER AFT EDGE CRACKED. REMOVED INNER SKIN PER SRM 51-30-2 PAGE 1, FABRICATED NEW INNER SKIN PER SRM 55-10-2. INSTALLED PER SRM 55-10-2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL NR 9502, INNER AFT EDGE CRACKED. REMOVED INNER SKIN PER SRM 51-30-2 PAGE 1, FABRICATED NEW INNER SKIN PER SRM 55-10-2. INSTALLED PER SRM 55-10-2. (M)