As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING INBOARD OF 32 PYLON, LEADING EDGE INTERIOR, UNDER PANEL 611GB, PNEUMATIC DUCT MOUNT GOUGED SPAR VERTICAL STIFFENER (STREAMER ATTACHED). REMOVED AND REPLACED VERTICAL STIFFENER PER BAC DWG 112N2038 AND 112N2002 REVISION D AND SRM 51-40-02.