What was found
CRACKS DISCOVERED IN THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE WING CENTER SECTION FRONT SPAR. THE DAMAGE IS IN THE WEB OF EACH OF THE STIFFENERS AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. ER/A 397596-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS DISCOVERED IN THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE WING CENTER SECTION FRONT SPAR. THE DAMAGE IS IN THE WEB OF EACH OF THE STIFFENERS AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. ER/A 397596-14.