What was found
CRACK - STIFFENER OF PANEL 616ET RT WING L/E UPPER SURFACE, 1 PLACE AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK - STIFFENER OF PANEL 616ET RT WING L/E UPPER SURFACE, 1 PLACE AT XW 297. REPAIRED CRACK AREA IAW MD11 SRM 57-40-02 FIG 201 REV 41.