What was found
LEFT WING; TRANSVERSE WEB IS CRACKED ON UPPER LEG O/B END; ABOVE #1 PYLON AFT TIP. REMOVED AND REPLACED LEFT WING TRANSVERSE WEB; P/N 115A2156-7 IAW SRM 51-40-02-0G-0 AND DWG. 115A2512; REV. -.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING; TRANSVERSE WEB IS CRACKED ON UPPER LEG O/B END; ABOVE #1 PYLON AFT TIP. REMOVED AND REPLACED LEFT WING TRANSVERSE WEB; P/N 115A2156-7 IAW SRM 51-40-02-0G-0 AND DWG. 115A2512; REV. -.