What was found
CRACKS WERE FOUND IN THE LBL 10 VERTICAL STIFFENER OF THE CENTER SECTION FRONT SPAR, IN THE WEB OF THE STIFFENER AT THE OVERWING FLOORBEAM TO STIFFENER JOINT. A SPLICE REPAIR WAS ACCOMPLISHED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS WERE FOUND IN THE LBL 10 VERTICAL STIFFENER OF THE CENTER SECTION FRONT SPAR, IN THE WEB OF THE STIFFENER AT THE OVERWING FLOORBEAM TO STIFFENER JOINT. A SPLICE REPAIR WAS ACCOMPLISHED.