As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR, FAULT - CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 LBL 33 (REPAIR) THE CENTER WING FRONT SPAR IS CLASSIFIED AS PRIMARY STRUCTURE PER SRM 51-00-04-0G. THIS REPAIR IS AS REINFORCING REPAIR AND CLASSIFIED AS MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 LBL 33 (REPAIR) REVIEW COMPLETE