What was found
LEFT WING T/E STRUCTURE VERTICAL WEB IS CRACKED AT THE INBOARD FWD CORNER OF THE INBOARD FLAP. REMOVED & REPLACED THE CRACKED WEB (ANGLE) IN REF TO DC/MD-10 SRM 51-35-01; VOL II & IN REF TO DAC DWG AUB 7203; REV "BA".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING T/E STRUCTURE VERTICAL WEB IS CRACKED AT THE INBOARD FWD CORNER OF THE INBOARD FLAP. REMOVED & REPLACED THE CRACKED WEB (ANGLE) IN REF TO DC/MD-10 SRM 51-35-01; VOL II & IN REF TO DAC DWG AUB 7203; REV "BA".