As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TUL - VERTICAL STIFFENER CORRODED RT WING FRONT SPAR STA 230. (ABOVE NR 5 L/E FLAP ACTUATOR.) REMOVED AND REPLACED CORRODED VERTICAL STIFFENER AT STA 230 ABOVE NR 5 L/E FLAP ACTUATOR. PRIMED, PAINTED, AND SEALED IAW SRM 53-10-01. TST: 49,071 HOURS. CYCLES: 24,653. (X)