What was found
1" LONG CRACK AT FWD INBD CORNER OF STRESS PANEL 522AT LADDER PLATE. REPAIRED CRACK AT FWD INBD CORNER OF LADDER PLATE AT STRESS PANEL 522AT IAW EO8-57-13-0394A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1" LONG CRACK AT FWD INBD CORNER OF STRESS PANEL 522AT LADDER PLATE. REPAIRED CRACK AT FWD INBD CORNER OF LADDER PLATE AT STRESS PANEL 522AT IAW EO8-57-13-0394A.